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Garmin T-30D CAT III NAV Ramp Test Set 产品说明书

Garmin T-30D CAT III NAV Ramp Test Set 产品说明书

T-30D•Permits ICAO Annex 10 CAT III ILS ramp check certification• Checks VOR, GS, LOC, MB, Flight Director, andAutopilot• Dual VOR/LOC/GS frequencies • Separate and simultaneous MB/ILS • Dual extended-range variable ILS• Quick, easy one-man operation from the cockpit • Lightweight and portable – weighs only 18 lbs. • Built-in NICAD battery and charger• Two year limited warranty; five & ten year available • Rugged, reliable, affordable• Backed by 40 years manufacturing experience • CE Compliant• Available non standard VOR/ILS frequencies with local agency approvalThe T-30D Ramp Test Set is designed for one-man operation of the VOR, MB, GS, LOC, flight director, and autopilot from the cockpit or flight deck. Built into a rugged and durable case, the T-30D will permit compliance with CAT III periodic ramp check certification in all weather conditions.DescriptionSpecifications Subject to Change Copyright © Tel-Instruments Electronics Corp.1VOR• Allows selection of VOR bearing in 45º steps from 0 -315°• Manual slewing provides capability for checking full-scale deflection for “sticky” analog meter movement (+10º)• Permits deletion of the REF 0, VAR 0, 30 and 9960 Hz modulation to check flag operation • 1020 Hz tone enable switch • Manual slewing of VOR bearing ± 10° left and right of courseLOC and G/S• Allows selection of preset DDM deflections of: On Course, one and 2 dots off center• Full-scale deflection can be tested using manual slewing• Allows 90 and 150 Hz tones to be deleted • Simultaneous LOC/GS/MB Mode • 1020 Hz tone enable switch• Variable attenuator calibrated in 1 dB steps • Two preset paired frequencies availableMarker Beacon and ILS • User selection of inner, middle, and outer marker • Simultaneous MB and ILS output signals •Variable and Preset DDM settings • Variable attenuator to control output Additional Features• Rugged Mil-Spec case • Built in battery and charger• 100/220 volt operation 40 – 400 Hz• Simple to understand front panel and controls that requires minimal training • Built-In diagnostic Self Test/TIC-Tel-Instruments-T-30D-NAV-Ramp-Test-Set.aspxTo buy, sell, rent or trade-in this product please click on the link below:VOR Operation LOC Operation108.15 MHz ± 0.025%Frequency108.10 MHz ± 0.025%Power +17 ±2 dBAttenuation 110 dB in 1 dB stepsModulationAudio Frequency 90/150 HzAudio Frequency Accuracy ±0.01%AM Depth 20 ± 2%Distortion < 5%Phase Accuracy 90 to 1150 Hz ±10ºIndicator DeflectionOn Course0.0 ± 0.01DDM/0.155 ± .02DDMVariable -0.155 to +0.155 DDMStep Left and Right; 1 & 2 DotsTone 1020 Hz ± 2%108.05 MHz ± 0.025%Frequency108.00 MHz ± 0.025%Power +17/ ± 2 dBAttenuation 110 dB in 1 dB stepsModulationAudio Frequency 30/9960 HzAudio Frequency Accuracy ± 0.01%AM Depth 30 ± 2%FM Deviation 480 ± 30 HzDistortion < 5%Indicator Deflection/Bearing 0-315° /± 0.1º in 45°Steps/Variable ±10 º- 15°Tone 1020 Hz ± 2%Frequency 75.0 MHZ ± 0.005%Power +18 ± 2dBAttenuation 110 dB in 1 dB stepsModulationAudio Frequency 400/1300/3000 HzAudio Frequency Accuracy ± 2%AM Depth 95 ± 4%Distortion < 10%334.70 MHz ± 0.0025%Frequency334.55 MHz ± 0.0025%Power +11 ±2 dBAttenuation 110 dB in 1 dB stepsModulationAudio Frequency 90/150 HzAudio Frequency Accuracy ± 0.01%AM Depth 40 ± 3%Distortion < 5%Phase Accuracy 90 to 150 Hz ± 10ºIndicator DeflectionOn Course0.0 ± 0.01DDM/0.175 ± .025DDMVariable -0.175 to + 0.175 DDMStep Up and Down; 1 & 2 DotsDelete 90 and/or 150 HzSize 14.5 x 9.4 x 6.5 in.Weight 18lbs.PowerInternal Battery or external120/220 VAC 50-400 HzEnvironmentalStorage- -51° to + 71° COperating -30° to +55ºCT-30D Specifications Subject to Change Copyright © Tel-Instruments Electronics Corp. 2Tel-Instrument Electronics Corp.728 Garden StreetCarlstadt, NJ 07072(201) 933-1600MB OperationGS OperationPhysical CharacteristicsLeading the Avionics Test Industry into the 21st Century!。

Teledyne Test Tools T3AFG30 和 T3AFG60 功能 随机生成器说明书

Teledyne Test Tools T3AFG30 和 T3AFG60 功能 随机生成器说明书

Debug with Confidence30MHz–60MHzTeledyne Test Tools T3AFG30and T3AFG60range of function/arbitrary generators are a series ofdual-channel waveform generators with specificationsof up to60MHz maximum bandwidth,150M Sa/smaximum sampling rate and14-bit vertical resolution.The proprietary Arbitrary&Pulse techniques used in theT3AFG30/T3AFG60models helps to solve theweaknesses inherent in traditional DDS generators whengenerating arbitrary,square and pulse waveforms.Withthe above advantages the T3AFG30and T3AFG60generators can provide users with a variety of high fidelityand low jitter signals,which can meet the growingrequirements of a wide range of complex applications.Tools for Improved Debugging●●Deep Memory–16kpts/Ch.Generatecomplex arbitrary waveforms.Quickly set up modulated waveforms.●●Wide Range of Modulation Types–AM,DSB-AM,FM,PM,FSK,ASK,PWM,Sweep,Burst,and PSK.●●High Resolution–14bit resolution.Generatewaveforms with low noise,low spurioussignal content and high dynamic range.●●Bandwidth Models of30MHz and60MHz.Wide choice of bandwidths.Other modelsavailable up to500MHz.●●Built In Arbitrary Waveforms.Load and replay built in Arbitrary Waveforms.●●User Defined Waveforms.Store and recall user defined waveforms.Enquire about the T3AFG5and T3AFG10.●●Lower cost5MHz and10MHz single channel modelsare also available.Key SpecificationsOrderingInformationFunctionT3AFG30,T3AFG60Display Size4.3”Color TFTExcellent Performance●●Modelbandwidths from 30MHz to 60MHz●●All Models have 2Channels ●●16kpts/Channel memory Great Connectivity●●USBhostport for mass storage●●USB device port (USBTMC)●●LAN portThe rise/fall times can be set independentlyto a minimum of 16.8ns at any frequency and to a maximum of 22.4s.The T3AFG range of Function/Arbitrary Waveform Generators support a wide range of modulation types including AM,FM,PM,FSK,ASK,PSKandDSB-AM.Burstmode supports ‘N Cycle’and ‘Gated’modes with the Burst source being configured as ‘Internal’,‘External’or ‘Manual’.Output amplitude into a high impedance load can be as high 20Vpp at frequencies up to 10MHz,and 10Vpp for frequencies greater than 20MHz.Smart Capabilities●●Sweepoutput carrier can be Sine,Square,Rampand Arbitrary waveforms●●Burstoutput under internal or external signal control●●Waveforms types include DC●●FrequencyResolution 1µHz●●DSB-AM:Double Sideband AM modulation Function ●●HarmonicFunction generating up to 16harmonics●●Multi-LanguageUser InterfaceSweep mode supports ‘Linear’and ‘Log’sweep,with ‘Up’and ‘Down’direction,and Sweep source can be configured as ‘Internal’,‘External’or ‘Manual’.The counter functionality,accessed via the rear panel BNC,gives a DCor ACcoupled counter capability from 100mHz to 200MHz.The Teledyne Test Tools T3AFG30and T3AFG60,with its low jitter design,can generate waveforms with exceptional edge stability.With better jitter performance comes better edge stability,and higher confidence inyour circuit design.Sine wave output exhibits almost no spurious artefacts at 60MHz and 0dBm.Low JitterI/O Connectivity●●LAN and USB connection●●10MHz Reference Input/Output●●Aux Input/Output ●●External modulationinput ●●External burst/sweep trigger input●●External gate input●●TheAux Input/Output will output a trigger pulse when an internal source is used●●ExternalCounterinputFrequencySpecificationDC CharacteristicsModulation Characteristics–PWMSync OutputOrderinginformation©2018Teledyne Test Tools is a brand and trademark of Teledyne LeCroyInc.All rights reserved.Specifications,prices,availability and deliverysubject to change without notice.Product brand or brand names are trademarks or requested trademarks of their respective Company ProfileT eledyne LeCroyis a leading provider of oscilloscopes,protocol analyzers and related test and measurement solutions that enable companies across a wide range of industries to design and test electronic devices of all types.Since our founding in 1964,we have focused on creating products that improve productivity by helping engineers resolve design issues faster and more effectively.Oscilloscopes are tools used by designers and engineers to measure and analyze complex electronic signals in order to develop high-performancesystems and to validate electronic designs in order to improve time to market.The Teledyne Test Tools brand extends the Teledyne LeCroy product portfolio with a comprehensiverange of testequipment solutions.This new range of products delivers a broad range of quality test solutions that enable engineers to rapidly validate product and design and reduce time-to-market.Designers,engineers and educators rely on Teledyne Test Tools solutions to meet their most challenging needs for testing,education and electronics validation.Location and FacilitiesHeadquartered in Chestnut Ridge,New York,T eledyne Test Tools and Teledyne LeCroy has sales,service and development subsidiaries in the US and throughoutEurope and Asia.T eledyne T est T ools and T eledyne LeCroy products are employed across a wide variety of industries,including semiconductor,computer,consumer electronics,education,military/aerospace,automotive/industrial,and telecommunications.Teledyne LeCroy (US Headquarters)700Chestnut Ridge RoadChestnut Ridge,NY .USA10977-6499Phone:800-553-2769or 845-425-2000Fax Sales:845-578-5985Phone Support:1-800-553-2769Email Sales:*******************************Email Support:**************************Web Site:/Teledyne LeCroy(European Headquarters)T eledyne LeCroy GmbH Im Breitspiel 11cD-69126Heidelberg,Germany Phone:+49622182700Fax:+496221834655Phone Service:+496221827085Phone Support:+496221827028Email Sales:*******************************Email Service:*******************************Email Support:*********************************Web Site:/germanyDistributed by:。

JTorX 用于在线模型驱动测试派生和执行的工具说明书

JTorX  用于在线模型驱动测试派生和执行的工具说明书

JTorX:A Tool for On-Line Model-Driven TestDerivation and ExecutionAxel BelinfanteFormal Methods and Tools,University of Twente,The Netherlands**************************.nlAbstract.We introduce JTorX,a tool for model-driven test derivationand execution,based on the ioco theory.This theory,originally presentedin[12],has been refined in[13]with test-cases that are input-enabled.For models with underspecified traces[3]introduced uioco.JTorX improves over its predecessor TorX[14]by using uioco and this newer ioco theory.By being much easier to deploy,due to improvedinstallation,configuration and usage.And by integrating additional func-tionality,next to testing:checking for(u)ioco between models[6];check-ing for underspecified traces in a model;interactive or guided simulationof a model.This makes JTorX an excellent vehicle for educational pur-poses in courses on model-based testing,as experience has shown–andits usefulness is not limited to education,as experience has shown too.1IntroductionTen years ago we presented TorX,a tool for model-based testing.Its main focus was on on line test derivation and execution,i.e.a test is derived on demand while it is being executed(for offline execution a test case was treated as a special kind of model;only much later TorX was extended with(experimental) offline test derivation).As we wrote in[1],important features of TorX are flexibility and openness.However,it turned out that in our attempt to obtain these features we sacrificed ease of deployment,in particular ease of configura-tion,and,on Windows,ease of installation.For case studies that was not an issue because1)usually one can choose where to run them(on a Unix system), 2)typically they were done by TorX-experts,and3)the configuration overhead was small compared to the overall effort of setting up a case study anyway.How-ever,it was an issue for transfer of the tool to non-TorX-experts,like students who have to install and use the tool to do tool-based exercises,or staffmembers who want to use it to show the idea of model-based testing.JTorX is our answer to this problem.JTorX is a re-implementation of the main functionality of TorX in Java.As a consequence,installation of JTorX is rather simple,also on Windows.Configuration is much simpler than in TorX, because all of it can be done via the JTorX Graphical User Interface(GUI).Not only is JTorX easier to deploy,we also used the opportunity to catch up with theoretical progress,and to add features that are helpful for education and for quick impromptu demonstrations.These are discussed in the next section.JTorX is,under BSD-style license,available for free at[17].J.Esparza and R.Majumdar(Eds.):TACAS2010,LNCS6015,pp.266–270,2010.c Springer-Verlag Berlin Heidelberg2010JTorX:A Tool for On-Line Model-Driven Test Derivation and Execution267 2FeaturesCatching up with theoretical progress led to the following.The initial design of TorX,based on the ioco theory of[12],made use of the fact that in that theory test cases are non input-enabled(once the tester has decided to apply a stimulus it will not look at output that might be produced by the system under test (SUT)until the stimulus has been applied).This was already revised when westarted to experiment with timed testing[5].The design of JTorX is based on the refined ioco theory of[13]in which test cases are input-enabled.In addition, JTorX allows testing for uioco(introduced in[3]),a weaker relation than ioco developed for models that contain underspecified traces.In JTorX the ability to support offline test derivation has been taken into account from the start.The following features were added in JTorX to ease educational use,nextto the functionality for on line test derivation and execution:a checker tofind underspecified traces in a given model;a checker that checks(instead of tests)whether two models are(u)ioco-related[6];a simulator for manual exploration of a model(or suspension automaton,see Section3)or guided simulation of a given trace,e.g.produced by one of the checkers.The test run can be guided,using such trace,or a test purpose.To access models,JTorX has built-in sup-port for:graphml[8](to allow the use of graph editor yEd[15]to draw a model as automaton),the Aldebaran(.aut)file format,the Jararaca[16]file format(toallow a regular expression-style specification of traces to guide a test run),and the TorX Explorer protocol to allow model access via the mcrl2[9],LTSmin[4]and CADP[7]tool environments.To connect to a SUT JTorX has built-in support for:use of a simulated model;use of a real program that communicates using labels of the model,either on its standard input and output,or over asingle TCP connection;use of the TorX Adapter protocol(for backwards com-patibility).Each test run is reported in a(text)log shown in the GUI(and as in TorX visualized in a dynamically updated message sequence chart).Duringa test run(as in TorX),and during simulation,progress through models and suspension automaton is visualized in dynamically updated automaton viewers. 3ArchitectureTheflexibility and openness of TorX were obtained by having a modular tool architecture.JTorX inherits this architecture(but not the deployment issues, by having a different implementation).A typical(J)TorX configuration,de-picted in Fig.1,contains at least the following components.(Components that are only used in guided test runs appear dotted in thisfigure.)An Explorerprovides uniform access to the(labelled transition system)state space of the Model(or Test Purpose,in case of a guided test run).A Primer provides access to the suspension automaton(see[13])of the Model(or Test Purpose)accessedvia its Explorer,i.e.it determinizes and marks quiescent states(in which the SUT is expected to stay silent)withδ-labelled selfloops.It does this on demand. To avoid storing states unnecessarily Primer and Driver tell their resp.Explorer268 A.BelinfanteFig.1.Tool components of a typical(J)TorX configuration.Items TP,Explorer, Primer and Combinator in the dotted boxes are only present in a guided test run. and Primer which states(reached by stimulus or observation not in the test run) to forget.An Adapter provides uniform access to the SUT.The Driver controls a test run,and decides whether to obtain and apply a stimulus,whether to obtain and check an observation,or to stop the test run.Additional components,like the Combinator,are used e.g.to guide a test run using a Test Purpose.Typi-cally,an Explorer is modeling-formalism dependent,but model-independent;an Adapter is model-dependent,and specific for a particular(family of)SUT.Theother tool components are model-,formalism-and SUT-independent.4UsageAt four universities students have used JTorX in courses on testing techniques, to compare models,and to test a real program w.r.t.a model that they developed themselves.Doing these exercises gave the students a deeper understanding of the ioco theory and its test derivation algorithm,and allowed them to experi-ence model-based testing in practice.For the tutors,the use of JTorX greatly reduced the effort needed to set up the exercise class,compared to the use of TorX in previous years.Moreover,it encouraged developing more elaborate exercises–for example,testing of a real program(now facilitated by JTorX built-in standard i/o Adapter)was not done in previous years.For the students, JTorX clearly provided a better user experience–with TorX there typical were complaints,e.g.about the GUI,but with JTorX there were none.As a result,JTorX will continue to be used in these courses.JTorX found a real,unintended error in a Java program developed as SUT for one of the courses.The program occasionally lost inputs,because its input handling was initialized inside(instead of before)its main input-processing loop.In an internship a student used Unit Testing and then JTorX to test the program he developed.JTorX foundfive errors,some of which rather subtle–these might not have been found without JTorX,even when the time invested in model-based testing would have been spent on manual testing instead[11].5Future WorkWe foresee improvements to JTorX in two directions:improvement of the user experience e.g.by professionalization of the user interface,and extension of theJTorX:A Tool for On-Line Model-Driven Test Derivation and Execution269 functionality.Implementation in JTorX of TorX’ability to deal with param-eterized action labels will enable use of its real-time Explorer[5]and its Explorer for Promela models.Also,connection to TorXakis[10]is planned.6Related WorkWe are aware of existing tools for model-based testing like those discussed in[2], but to our knowledge,none of them posseses a similar suitability for education. AcknowledgementsOur gratitude goes to Mark Timmer for helping with the testing techniques practical exercises at University of Twente,to Jan Tretmans for trying JTorX and providing feedback,and to Jaco van de Pol for feedback on this article. References1.Belinfante,A.,et al.:Formal test automation:A simple experiment.In:12th Int.Workshop on Testing of Communicating Systems,pp.179–196.Kluwer,Dordrecht (1999)2.Belinfante,A.F.E.,Frantzen,L.,Schallhart,C.:Tools for test case generation.In:Broy,M.,Jonsson,B.,Katoen,J.-P.,Leucker,M.,Pretschner,A.(eds.)Model-Based Testing of Reactive Systems.LNCS,vol.3472,pp.391–438.Springer, Heidelberg(2005)3.van der Bijl,H.M.,Rensink,A.,Tretmans,J.:Compositional testing with ioco.In:Petrenko,A.,Ulrich,A.(eds.)F ATES2003.LNCS,vol.2931,pp.86–100.Springer, Heidelberg(2004)4.Blom,S.C.C.,van de Pol,J.C.,Weber,M.:Bridging the gap between enumera-tive and symbolic model checkers.Technical Report TR-CTIT-09-30,Centre for Telematics and Information Technology,University of Twente,Enschede(2009) 5.Bohnenkamp,H.C.,Belinfante, A.F.E.:Timed testing with TorX.In:Fitzger-ald,J.S.,Hayes,I.J.,Tarlecki,A.(eds.)FM2005.LNCS,vol.3582,pp.173–188.Springer,Heidelberg(2005)6.Frantzen,L.:iocoChecker(2008),http://www.cs.ru.nl/~lf/tools/iocochecker7.Garavel,H.,et al.:Cadp2006:A toolbox for the construction and analysis ofdistributed processes.In:Damm,W.,Hermanns,H.(eds.)CAV2007.LNCS, vol.4590,pp.158–163.Springer,Heidelberg(2007)8.GraphML work group:GraphMLfile format,9.Groote,J.F.,et al.:The mcrl2toolset.In:Proc.International Workshop on Ad-vanced Software Development Tools and Techniques,WASDeTT2008(2008) 10.Mostowski,W.,Poll, E.,Schmaltz,J.,Tretmans,J.,Schreur,R.W.:Model-based testing of electronic passports.In:Alpuente,M.(ed.)FMICS2009.LNCS, vol.5825,pp.207–209.Springer,Heidelberg(2009)11.Sijtema,M.:Developing XBus2—a software bus,that is maintainable,testableand backwards-compatible.Internship Report,University of Twente(2009)12.Tretmans,J.:Test generation with inputs,outputs,and repetitive quiescence.Soft-ware-Concepts and Tools17(3)(1996)270 A.Belinfante13.Tretmans,J.:Model Based Testing with Labelled Transition Systems.In:Hierons,R.M.,Bowen,J.P.,Harman,M.(eds.)FORTEST.LNCS,vol.4949,pp.1–38.Springer,Heidelberg(2008)14.Tretmans,J.,Brinksma,H.:TorX:Automated model-based testing.In:Hartman,A.,Dussa-Ziegler,K.(eds.)First European Conference on Model-Driven SoftwareEngineering,Nuremberg,Germany,Nuremberg,Germany,December2003,pp.13–43(2003)15.yWorks:yEd,/en/products_yed_about.html16.Jararaca manual,http://fmt.cs.utwente.nl/tools/torx/jararaca.1.html17.JTorX website,http://fmt.cs.utwente.nl/tools/jtorx/。

Loadwise Model 502 评定容量指示器系统说明书

Loadwise Model 502 评定容量指示器系统说明书

LOADWISE MODEL 502 RATED502 CAPACITY INDICATOR SYSTEMLOADWISE MODEL 502 RATED CAPACITY INDICATOR SYSTEMCALIBRATION MANUALLOADWISE, INC.18362 GOTHARD STREETHUNTINGTON BEACH, CA 92648TEL: 714/841-5662FAX: 714/841-5372LOADWISE MODEL 502 RATEDCAPACITY INDICATOR SYSTEMTable of ContentsDescription Page Display Operation 3 Operation Modes 4To Enter Cal Mode 5Cal Modes 6 Sequence of Calibration 7Cal Mode 00 8Cal Mode 01 9Cal Mode 02 10Cal Mode 03 11Cal Mode 04 12Cal Mode 05 13Cal Mode 06 14Cal Mode 10 15Cal Mode 11 16Cal Mode 12 17Cal Mode 13 18Cal Mode 14 22Cal Mode 15 24LOADWISE MODEL 502 RATEDCAPACITY INDICATOR SYSTEMDISPLAY CONSOLEThe Display Console is split into two sections. The center section is a four (4) line “alpha-numeric” screen that displays information to the operator, and the right section is a keypad used to enter information into the system and to change the display to the various modes, and is also used in the calibration process.F L/H ALT+ TESTTARE DEDUCT DUTYLOADWISE 500LOADWISE MODEL 502 RATEDCAPACITY INDICATOR SYSTEMF L/H ALTTARE DEDUCT DUTYLOADWISE 500LOADWISE MODEL 502 RATEDCAPACITY INDICATOR SYSTEMTO ENTER THE CALIBRATION MODEThe calibration mode is protected by a sequence code which is only available to trained, authorized personnel, at the discretion of the owner.To enter the calibration mode, press:TEST - TEST - TEST - ALTThe display will show the crane make and model, the increments used in the systemand the load chart (“feet - pounds” or “meters - kilos”), the serial number of thesystem, and the system’s date.While this data is displayed, (approximately 10 seconds,) the entry code must be pushed. If the incorrect entry code is selected, the display will return to its standard, normal mode.Once the calibration mode has been entered, the display will be at calibration mode00, which is the starting point for the calibration process.WARNINGTHE CALIBRATION MODE ENABLES THE BASIC FUNCTION OF THEINDICATOR TO BE CHANGED. UNAUTHORIZED INTERFERENCE WITH THE CALIBRATION OF THE SYSTEM CAN BE VERY DANGEROUS TO THE SAFETYOF THE CRANE.LOADWISE MODEL 502 RATEDCAPACITY INDICATOR SYSTEM The calibration mode contains fifteen (15) sections. Not all sections are used on all typesof cranes.MODE FUNCTION01 TO ENABLE SENSOR ZEROS TO BE SET02 TO ENABLE SENSOR SPANS AND SENSITIVITY TO BE SET03 TO PRESET THE MAIN BOOM WEIGHT IN DIFFERENT CONFIGURATIONS04 TO PRESET THE JIB WEIGHT COMBINED WITH THE MAIN BOOM WEIGHT05 CALIBRATION OF THE LOAD ON THE HOOK06 TO CORRECT FOR DEFLECTION OF THE BOOM AND JIB COMBINATIONSDUE TO THEIR OWN WEIGHT, AND THE HOOK LOAD07 (RESERVED FOR A MODEL OTHER THAN 502)08 (RESERVED FOR A MODEL OTHER THAN 502)09 (RESERVED FOR A MODEL OTHER THAN 502)10 “LAST-LOADS-RECALL” FUNCTION11 TO PRE-SET THE ALARMS AND WARNING LIMITS12 TO PRE-SET THE VARIOUS LOAD LIMITS13 TO ENTER THE CRANE GEOMETRY (SEE DWG # 94536 OR # 94537)14 TO ENTER THE WINCH/BOOM HOIST ROPE GEOMETRY (SEE DWG # 94554)15 MEMORY MOVEMENT SYSTEMLOADWISE MODEL 502 RATEDCAPACITY INDICATOR SYSTEM 1)Go to Mode 15 and carry out “I - A” to ensure that the system is cleared back tothe factory standard.2)Ensure that the loadpins are electrically connected before installation, and thezeros are set (in Mode 01,Section 06 & 07) and the sensitivity of each pin is set (in Mode 02, Section 06 & 07).3)Check the geometry dimensions in Mode 13 and 14, ensuring that all data ispresent and correct.4)Check Mode 11 and 12 for correct settings of alarm percentages, rope limits, etc.5)Complete Mode 01 and 02 for setting the zero and the span of boom angle.6)Initial boom calibrations should be carried out with the shortest boom length withMode 03 (boom weight) and then Mode 05 (load calibration), to be completed and working correctly before moving on to the next section.7)After ensuring that (# 6 above) has been completed and is correct, increase theboom length to approximately half the full length, or to the shortest boom that willcarry a jib. Next, this main boom should be calibrated for boom weight (in Mode03), and the jib fitted and then calibrated for boom weight (in Mode 04). Boomdeflection (in Mode 06) is then carried out at this time and at any other time it isfound to be necessary.8)Additonal boom and boom / jib combinations should then be rigged and calibrated,to cover the maximum possible boom lengths. Typically at least three (3) boomlengths are calibrated, and more (if practical) will ensure maximum accuracy ofcalibration. If midpoint suspension is employed, calibration must be carried out at the suspension point boom length and at the boom length immediately prior tomidpoint suspension.9)Jib calibrations (in Mode 04) must be carried out for all combinations of jibs (forexample, all boom lengths / offsets on the minimum and maximum boom lengths). 10)After all the above is completed and double-checked, go to Mode 15 and backupthe calibration by copying “A” memory to “B” memory. TAKE GREAT CARE TONOT DO AN “I - A” COPY AS THIS WILL WIPE OUT THE CALIBRATION.LOADWISE MODEL 502 RATEDCAPACITY INDICATOR SYSTEMCal Mode 00 is the “index” or starting point, used to access the various Cal Modes. To exit the calibration mode (while in Cal Mode 00) and return to the normal, operating mode, press “F”.NOTE: while in the calibration mode, the alarms / cut-outs are suppressed with the exception of (1) “OUT-OF-LEVEL” and (2) “OVERHOIST” (or “Anti Two Block”). Also while in Cal Mode these two messages will not be available on the display.Notes:1)In Mode 00, the section numbercannot be modified.2)To select a mode, press “ALT”.This will cause the Cal Modenumber to flash. While it isflashing, press “+” or “-” to selectthe mode. When the correct CalMode number has beenselected, press “ALT” to accessthe Section Number.3)If there is not an available modefor the number selected, thesystem will return automaticallyto Cal Mode 00, Section 00.4)While the Cal Mode number isflashing, the “CAL. END=F”message is not available.LOADWISE MODEL 502 RATEDCAPACITY INDICATOR SYSTEM The display will show this whenfirst in Cal Mode 01Within Cal Mode 01, there are eight (8) sections:Mode/SectionNo.Sensor No. Sensor Description01/00 A3 Superstructure Angle Sensor (only on special applications)01/01 A2 Luffing Jib Angle Sensor (when fitted)01/02 L2 (Not Applicable to 502 System)01/03 W3 (Not Applicable to 502 System)01/04 L1 (Not Applicable to 502 System)01/05 A1 Boom Angle Sensor01/06 W2 2nd Load Sensor01/07 W1 1st Load SensorTo change Sections, press “ALT” - this will cause the Section number to flash. While it is flashing, press “+” or “-” until the correct Section number is displayed. To stop the number flashing, press “ALT”.The second display line as shown above has two sets of numbers: the left-hand set are for reference only; and the right-hand set are changed to effect the calibration.To modify the Section, press “F”. This will cause the ‘100’s’ to flash; while flashing, this number can be changed up or down (as required) by pressing “+” or “-”. Once the correct number has been selected,press “F” again to change the flashing digit to the ‘10’s’; a third press of “F” will change the flashing digit tothe ‘1’s’ and an additional press of “F” will change the flashing digit to the ‘0.1’s’, etc. While any of theseright-hand numbers has a flashing digit, it can be changed up or down (as required) by pressing “+” or “-”.A final press of the “F” button will stop the flashing and give three choices:l“ALT” will allow a change to a different Section number.l“L/H” will store the calibration just performed. (If “+” or “-” have not been used, the memory will not be updated (since no change has been made), even if the command to store (“L/H”) is used.) If “L/H” is pressed, the display will change after a delay of approximately three seconds.l“TARE” will return to Mode 00/00 without saving the calibration just performed.Note:The Angle “zero” should be donewith a small positive boom angle(for example, +2.0º).In Mode 01/06 and 01/07, theLoad Sensors MUST be “zeroed”before installation to the crane.Cal Mode 01 is used to “zero” the various sensors:LOADWISE MODEL 502 RATEDCAPACITY INDICATOR SYSTEMThe display will show thiswhen first in Cal Mode 02 Within Cal Mode 02, there are eight (8) sections:Mode/Section No.Sensor No. Sensor Description 02/00A3 Superstructure Angle Sensor (only on special applications) 02/01A2 Luffing Jib Angle Sensor (when fitted) 02/02L2 (Not Applicable to 502 System) 02/03W3 (Not Applicable to 502 System) 02/04L1 (Not Applicable to 502 System) 02/05A1 Boom Angle Sensor 02/06W2 2nd Load Sensor (SENSITIVITY - SEE NOTE BELOW ) 02/07 W1 1st Load Sensor (SENSITIVITY - SEE NOTE BELOW )Cal Mode 02 is used to “span ” the various sensors:Notes:•In Mode 02/06 and 02/07, enter the SENSITIVITY of the load sensors. This information is found on each load sensor, and is expressed as a “mV/V” value such as “1.334”. If more than four digitsare shown, only the first four digits are entered, irrespective of where the decimal point is shown on the load sensor.•Calibration will not be successful if the number on the left-hand side of the second display line is either 000.0 or 409.2. If this occurs, the sensor being calibrated is out of range and must be corrected before proceeding further with the calibration process.LOADWISE MODEL 502 RATEDCAPACITY INDICATOR SYSTEMLOADWISE MODEL 502 RATEDCAPACITY INDICATOR SYSTEMLOADWISE MODEL 502 RATEDCAPACITY INDICATOR SYSTEMLOADWISE MODEL 502 RATEDCAPACITY INDICATOR SYSTEMCAPACITY INDICATOR SYSTEMCal Mode 10 is the LAST LOADS RECALL optionThe display will show thiswhen in Cal Mode 10LOADWISE MODEL 502 RATEDCAPACITY INDICATOR SYSTEM Cal Mode 11 is used to adjust the Alarm SettingsWithin Cal Mode 11, there are eight (8) sections:Mode/SectionNo. DescriptionFactory DefaultValuesNotes11/00 APPROACH % 95.0 %11/01 OVERLOAD % 105.0 %11/02 MOTION-CUT % 110.0%11/03 HIGH ANGLE Aº 80.0º11/04 LOW ANGLE Aº 0.0º11/05 BOOM SWITCH 0.0 Not Applicable to 502 System11/06 SHEAVE % 100For setting in the multiple loads per line 11/07 SCALE FACTOR 0.5 Set to 1.0 for cranes above 650 Tons.To change Sections, press “ALT” - this will cause the Section number to flash. While it is flashing, press “+” or “-” until the correct Section number is displayed. To stop the number flashing, press “ALT”.To modify the Section, press “F”. This will cause the ‘100’s’ to flash; while flashing, this number can be changed up or down (as required) by pressing “+” or “-”. Once the correct number has been selected, press “F” again to change the flashing digit to the ‘10’s’; a third press of “F” will change the flashing digit to the ‘1’s’ and an additional press of “F” will change the flashing digit to the ‘0.1’s’, etc. While any of these right-hand numbers has a flashing digit, it can be changed up or down (as required) by pressing “+” or “-”. (This mode will only change the function size in 0.5 steps.)A final press of the “F” button will stop the flashing and give three choices:l“ALT” will allow a change to a different Section number.l“L/H” will store the calibration just performed. (If “+” or “-” have not been used, the memory will not be updated (since no change has been made), even if the command to store (“L/H”) is used.) If “L/H” is pressed, the display will change after a delay of approximately three seconds.l“TARE” will return to Mode 00/00 without saving the calibration just performed.CAPACITY INDICATOR SYSTEMCal Mode 12 is used to adjust the Load Limit SettingsLOADWISE MODEL 502 RATEDCAPACITY INDICATOR SYSTEMLOADWISE MODEL 502 RATEDCAPACITY INDICATOR SYSTEM502 CALIBRATION MODE 13GEOMETRY DATA - “WITHOUT MAST” VERSIONLATTICE BOOM CRANE WITH “FIXED” GANTRY AND “FLYING BRIDLE”“FIXED” GANTRY“FLYING” BRIDLEDim. CM DESCRIPTIONA Upper Pendant Fixing to Center Line of BoomB Upper Pendant Fixing to Head Sheave PinC Boom Pivot Pin to Gantry (Horizontal)D Boom Pivot Pin to Gantry (Vertical)E Head Sheave Pin to C/L of BoomF Boom Pivot Pin to Center of Slew SSheave Radius X Minimum Boom LengthYBoom Pivot Pin to Ground (Vertical)4 SEP 97 # 94536LOADWISE MODEL 502 RATEDCAPACITY INDICATOR SYSTEMLATTICE BOOM CRANE WITH “MAST”MAST502 CALIBRATION MODE 13GEOMETRY DATA - “WITH MAST” VERSIONDim CM DESCRIPTIONA Upper Pendant Fixing to Center Line of BoomB Upper Pendant Fixing to Head Sheave PinC Boom Pivot Pin to Mast Pivot (Horizontal)D Boom Pivot Pin to Mast Pivot (Vertical)E Head Sheave Pin to C/L of BoomF Boom Pivot Pin to Center of SlewG Mast LengthH Pendant Length on Minimum Boom S Sheave Radius X Minimum Boom LengthYBoom Pivot Pin to Ground (Vertical)Cal Mode 13/11 selects a range of questions to which the crane operator must respond before the system will operate in the normal operating mode. Three options are available:Page 21 Edition # 94599Rev 00242LOADWISE MODEL 502 RATEDCAPACITY INDICATOR SYSTEMPage 23LOADWISE MODEL 502 RATEDCAPACITY INDICATOR SYSTEMEdition # 94599Rev 00242WINCH GEOMETRY22 SEP 97 # 94554Dimension CMDESCRIPTIONA MAIN WINCH TO BOOM PIVOT PIN (HORIZONTAL)B MAN WINCH TO BOOM PIVOT PIN (VERTICAL)C MAIN WINCH RADIUSD AUX WINCH TO BOOM PIVOT PIN (HORIZONTAL)E AUX WINCH TO BOOM PIVOT PIN (VERTICAL) FAUX WINCH RADIUSCAPACITY INDICATOR SYSTEMCal Mode 15 is used to move stored calibration informationPage 25LOADWISE MODEL 502 RATEDCAPACITY INDICATOR SYSTEMEdition # 94599Rev 00242The following functions have been added to the 502 program:Mode/SectionNo.Description01/02 This adds load to all main boom duty loads and should be set as a default to zero.02/02This subtracts load from all jib duty loads and should be set as a default to zero.11/05Is named “Correction %” and should be set as a default value to 100%.This % is 100% at high angle and progresses toward the set value as the boom angle is reduced. Therefore the load should be calibrated at high angle and corrected plus or minus at a low boom angle.。

DPST-3500M数字潜力速度静态测试设备说明书

DPST-3500M数字潜力速度静态测试设备说明书

DPST-3500M Digital Pitot Static Test Set “High Accuracy, Exceeds 91.411 FAR Specs, Light Weight for Flight Line Portable Inspections”FAA Certified Repair Station # DZMR112L Cage Code # 3PTA2General InformationThe Model DPST-3500M is a precision, manually controlled, portable, flight line Digital Pitot Static Test Set. This dual channel test set is designed to provide regulated total Pitot (PT) pressure and Static (PS) pressure outputs to simulate Altitude, Airspeed, Vertical Speed, and Mach parameters. The test set can also be used in laboratory environments to calibrate Air Data instruments and various vacuum and pressure gauges. The test set is compact, lightweight and made for harsh Flight Line conditions. Its compact size can fit in the overhead storage compartment of most commercial airliners.• Control valves have a lifetime warranty with a built in protection seat to prevent over tightening of precision valve stems.• Internal pumps produce pressure and vacuum for maintenance free performance.• Performance ranges: Altitude –1500 to 35,000 ft., Vertical Speed +/-20,000 ft./min, Airspeed 0 to 400 knots, and Mach 0 to 1.12.• Sensors automatically perform temperature compensation for extreme flight line conditions. • Smart AC power supply provides a wide range of input voltages: 85 to 264 V AC / 47 to 440 Hz.• Storm Case* is rugged and constructed to meet applicable requirements of MIL-STD-810F and FED-STD-101C and is watertight and pad lockable for theft protection. • Calibration meets or exceeds the published National Institute Standards and Technology (N.I.S.T) specifications. • Test set is shipped with quick disconnect fittings, 2 hoses (15ft /ea) and a power cord (6ft).• Specifications: Exterior dimensions 17”L X 11.70” W X 6.20”H (43.2 x 29.7 x 15.7 cm) Weight 15 lbs. / 6.8 kg*This system is sold as a complete kit ready for use. Includes a current calibration certificate, all connections, and an operation manual.• Certified to perform Pitot Static FAR 91.411 Part 43 Appendix E certifications on General Aviation, Military, Rotary Wing, and Light Sport Aircrafts.• Precision microprocessor based, with Honeywell sensors, accurate to +/- 0.020 % FS.• Display is a sunlight readable TFT 4” inch color, Micro-Graphic Touch panel showing detailed units of measurements including Ft, M, Kts, Km/hr, Mach, Ft/min, m/min, inHg, mbar, and psia.• Main screen displays Altitude, Vertical Speed, Airspeed, and Mach. • Automatic Pitot and Static leak rate modes perform calculations for operator convenience.• Hoses have self- sealing quick disconnect fittings to protect aircraft from pressure loss.Standard Features *Case meets required measurements to fit into overhead compartment in commercial airlines.Weight 15 lbs.DFW Instrument Corporation Tel # 214-217-7600 16445 Addison Road Fax # 214-217-8307 2nd Floor, Hangar 2 Toll Free # 888-500-0075 Addison, TX 75001 To buy, sell, rent or trade-in this product please click on the link below:/DFW-DPST-3500M-Pitot-Static-Test-Set.aspxDigital Manual Pitot Static Test Set DPST-3500M Performance SpecificationsAbsolute Pressure Performance Static Sensor:Range: 0.3 to 40 inHg abs.Accuracy: +/- 0.020 % FS Overpressure: 200 % FS without damagePitot Sensor Range: 0.8 to 80 inHg abs.Accuracy: +/- 0.020 % FS Overpressure: 200 % FS without damageAltitude Performance Range: -1500 ft. to 35,000 ft.Resolution: 1 ft. Accuracy: ±5 ft. @ 0 ft. ±45 ft. @ 35,000 ft.Rate of Climb Performance Range: 100 ft./min. to 20,000 ft./min.Resolution: 25 ft./min.Accuracy: ±10 % of VSI RateAirspeed Performance Range: 10 to 400 Knots Resolution: 1.0 Knots Accuracy: ±2 Knots @ 20 knots ±1 Knots @ 100 knots ±1.5 Knots @ 400 knotsMach Performance Range: 0.0 Mach to 1.12 Mach Resolution: 0.001 Mach Accuracy: 0.020 Mach + 0.1 Mach Pressure Medium Dry AirPressure Connections Quick Disconnects (2 ea.)Safety Seal on SHIP / UUTDisplay Update Rate Once Every 2 Tenths per Second Temperature Compenstion Range 32°F to 122°F 0°C to 50°C Sensors Honeywell Sensors (NIST Traceable)Power Requirement Input Range: 85 - 264 V AC Frequency Range: 47 Thru 440 Hz Environmental Specs Temp. Operating: -20° C to +85° C Temp. Storage: -25° C to +60° C Humidity: 0% to 95% RH Warranty & Calibration Warranty: 2 years (parts & labor ) Calibration: Up to 1 year (yearly calibration suggested ) Certification Calibration / Trace to NIST Accuracy exceeds FAA Regulations FAR 91.411 Specifications Physical Dimensions 17” L x 11.70” W x 6.20” H (43.2 x 29.7 x 15.7 cm)Weight/ Case Specification 15 Lbs / 6.8 Kg MIL-STD-810F • FED-STD-101C • ATA 300Color / Flight Line Yellow Accessories Include: Protection Quick Release Fittings, Hoses, and operation manual. ORDERING INFORMATION/ OPTIONS Mfg. Part Number:DPST-3500M-XXX Option 1: Removable Lid Option 2: 28VDC power- DC Option 3: Altitude EncoderDFW Instrument Corporation 16445 Addison Road 2nd Floor, Hangar 2Addison, TX 75001Tel. # 214-217-7600 Fax # 214-217-8307。

Model 72-8155 操作手册说明书

Model 72-8155  操作手册说明书

1Table of ContentsTitle Page Overview Inspection Safety Information Rules For Safe Operation International Electrical Symbols The Meter Structure Functional Buttons Display Symbols Measurement Operation A. Measuring Resistance B. Diode and Continuity Test C. Capacitance Measurement D. Inductance Measurement E. Transistor hFE Measurement General Specifications Accuracy Specifications A. Resistance Test B. Continuity & Diodes C. Capacitance Test D. Inductance Test E. Transistor Maintenance A. General Service B. Replacing the Battery C. Replacing the Fuse 34457891011111315171819202021212222232324252OverviewThis Operating Manual covers information on safety and cautions. Please read the relevant information carefully and observe all the Warnings and Notes strictly.To avoid electric shock or personal injury, read the ìSafety Informationî and ìRules for Safety Operationîcarefully before using the Meter.Digital Inductance Capacitance Meter Model72-8155 (hereafter referred to as ìthe Meterî) is a 3 1/2 digits with steady operations, fashionable design and highly reliable hand-held measuring instrument.The Model 72-8155 will measure capacitance, inductance, resistance, transistor hFE and test diodes. It will also test continuity with an audible buzzer.34InspectionOpen the package case and take out the Meter. Check the following items carefully to see if any items are missing or damaged.Item Description Qty 123Operating Manual Test Clip 9V Alkaline Battery (NEDA1604, 6F22or 006P) (installed)1 piece 1 pair 1 pieceIn the event you find any items missing or damaged, please contact your dealer immediately.Safety InformationThis Meter complies with the standards EMC e the Meter only as specified in this operating manual,otherwise the protection provided by the Meter may be impaired.In this manual, a Warning identifies conditions and actions that pose hazards to the user, and may damage the Meter or the equipment under test.A Note identifies the information that user should pay attention to.International electrical symbols used on the Meter and in this Operating Manual are explained on page 7.Rules For Safe Operationllllllll5llllll6International Electrical Symbols Lx7The Meter Structure(see figure 1)8Power L-C 9Functional ButtonsThe following table provides information regarding the functional button operation.Button DescriptionPress the Power down to turn the Meter on.Press the Power again to turn the Meter power off.Press L-C down to enter the Capacitance measurement mode.Press L-C up to enter the Inductance measurement mode.10Display Symbols (see figure 2)(figure 2)Meaningll1.2.3.11Measurement OperationA. Measuring Resistance (see figure 3)(figure 3)Notellll12To avoid damage to the Meter or to the devices under test, disconnect circuit power and discharge all the high-voltage capacitors before measuring diodes andcontinuity.Testing DiodesInsert the red test clip into the terminal and the black test clip into the COM terminal.Set the rotary switch to .For forward voltage drop readings on any semiconductor component, place the red test clip on the componentís anode and place the black test clip on the componentís cathode.The display shows the diode forward voltage dropís nearest value.e the diode test to check diodes, transistors, and other semiconductor devices. The diode test sends a current through the semiconductor junction, and then measures the voltage drop across the junction. A good silicon junction drops between 500mV and 800mV.To test a diode out of a circuit, connect the Meter as follows:13ll l1.2.3.4.5.ll14NoteNote1.2.3.4.15C. Capacitance Measurement (72-8155 only, see figure 5)(figure 5)Notellll16llll17D. Inductance Measurement (see figure 6)(figure 6)1.2.3.4.Remarks:l18(figure 7)1. 2. 3. 4. Note:General Specifications lllllllll19Accuracy Specifications A. Resistance TestRemarks:lll20Remarks:llC. Capacitance TestRemarks:lll21D. Inductance TestRemarks:ll22Maintenancellll23(figure 8)To replace the battery:1.2.3.4.5.24To replace the Meterís fuse:1.2.3.4.5.6.7.(figure 9)S C R E W2526。

迈迪工具集3.5版说明书

迈迪工具集3.5版说明书

前 言济南迈迪数码技术有限公司是一家专业从事工业设计与动画制作、软件开发与技术咨询、网站运营与电子商务的综合信息技术公司,公司自06年整合数个公司业务正式成立以来,秉持原先的开发理念,坚持在优秀的三维设计软件上开发有中国特色的设计技术,服务于广大国内设计者和配件制造商,赢得了众多客户的好评。

本工具集的推出,始终坚持不断增加新功能,提高设计效率的目标,广泛征求众多设计者提出的中肯意见,在原FNT(法恩特工具集,用于SW06以前版本,本公司早期产品)基础上,逐步完善更新,以每年修正两个版本的速度,及时向国内广大设计者提供优秀的设计手段,也因此深得用户青睐。

我公司的软件开发者们,积极采纳用户意见,不断研究新技术应用,始终希望为用户能提供更方便、更实用的软件产品,我们也始终坚持对个人用户免费的目标,也希望更多的受益者能为自己的工作带来更高的效率。

技术的进步是没有止境的,我们得益于用户的资助和不断提出的意见,因此得以快速发展并始终在三维设计技术二次开发领域和产品数据管理领域据有举足轻重的地位,有了广大用户的支持,我们就有动力不断继续开发下去。

该版本的发布,也是经过严格测试和试用的,使用方式略有变化,但是宗旨没有改变,仍然需要注册码(原先购买的注册码始终有效),若没有注册码,使用是正常的,只不过还会弹出一个广告黑屏,并不影响使用效果,郑重声明:本软件测试和试用过程严格,绝无木马和病毒,也不会有任何额外插件,因此,用户没有必要担心任何问题,倘若因为我们的软件而导致出现计算机问题,则一般是误操作或者本身操作系统有问题,请自行修正。

再次感谢大家的支持!一、软 件 安 装1.本软件目前支持Solidworks2007后续各个版本,安装前,请先确保本机上安装有Solidworks2007或更高版本。

如果在Solidworks2006及以下版本中使用,部分功能可能会运行不正常。

2.在安装本软件前要安装运行环境Microsoft .NetFramework2.0。

特斯拉ModelS用户手册说明书

特斯拉ModelS用户手册说明书

Product Data SheetTrigonox 44BAcetyl acetone peroxide, in solvent mixtureTrigonox® 44B is an acetylacetone peroxide formulation for fast curing of unsaturated polyester resins in the presence of a cobalt accelerator at room and elevated temperatures, including a VR system.CAS number37187-22-7 ( for EU:13784-51-5)EINECS/ELINCS No.253-384-9 (for EU: 237-438-9)TSCA statuslisted on inventorySpecificationsAppearance Clear liquidColor50 Pt-Co max.Total active oxygen 4.0-4.2 %CharacteristicsDensity, 20°C 1.055 g/cm³Viscosity, 20°C21 mPa.sApplicationsTrigonox® 44B is an acetyl acetone peroxide formulation for the curing of unsaturated polyester resins in the presence of a cobalt accelerator at room and elevated temperatures. With the curing system Trigonox® 44B/cobalt accelerator a much faster speed of cure may be achieved than with curing systems based on a MEKP plus cobalt accelerator, at room and elevated temperatures. Normally the gel times with Trigonox® 44B are comparable to those with Butanox M-50.Trigonox® 44B is particularly suitable in those applications where a fast mold-turnover is required, e.g. for the cold press molding or resin injection molding techniques. The system Trigonox® 44B/cobalt accelerator will give a higher peak exotherm than a standard MEKP/cobalt accelerator system. Due to this fact, is it recommendable to avoid the production of too thick laminates in one operation. At low temperatures a reasonable speed of cure is still obtained when Trigonox®44B is used in combination with large amounts of cobalt accelerator possibly in combination with N,N Dimethylaniline as promotor.Thermal stabilityOrganic peroxides are thermally unstable substances, which may undergo self-accelerating decomposition. The lowest temperature at which self-accelerating decomposition of a substance in the original packaging may occur is the Self-Accelerating Decomposition Temperature (SADT). The SADT is determined on the basis of the Heat Accumulation Storage Test.SADT60°CMethod The Heat Accumulation Storage Test is a recognized test method for thedetermination of the SADT of organic peroxides (see Recommendations on theTransport of Dangerous Goods, Manual of Tests and Criteria - United Nations, NewYork and Geneva).StorageDue to the relatively unstable nature of organic peroxides a loss of quality can be detected over a period of time. To minimize the loss of quality, Nouryon recommends a maximum storage temperature (Ts max.) for each organic peroxide product. Note: Ts min. -10°C to prevent crystallization.Ts max.25°CTs min.-10°CNote When stored under the recommended storage conditions, Trigonox® 44B willremain within the Nouryon specifications for a period of at least 6 months afterdelivery.Packaging and transportThe standard packaging is a 30-liter HDPE can (Nourytainer®) for 30 kg peroxide solution. Both packaging and transport meet the international regulations. For the availability of other packed quantities contact your Nouryon representative. Trigonox® 44B land and sea transport is classified as Organic peroxide type E; liquid, Division 5.2; UN 3107. Air transport is classified as Organic peroxide type D; liquid, Division 5.2; UN 3105.Safety and handlingKeep containers tightly closed. Store and handle Trigonox® 44B in a dry well-ventilated place away from sources of heat or ignition and direct sunlight. Never weigh out in the storage room. Avoid contact with reducing agents (e.g. amines), acids, alkalis and heavy metal compounds (e.g. accelerators, driers and metal soaps). Please refer to the Safety Data Sheet (SDS) for further information on the safe storage, use and handling of Trigonox® 44B. This information should be thoroughly reviewed prior to acceptance of this product. The SDS is available at /sds-search.Major decomposition productsCarbon dioxide, acetyl acetone, mixture of aliphatic acids, waterAll information concerning this product and/or suggestions for handling and use contained herein are offered in good faith and are believed to be reliable.Nouryon, however, makes no warranty as to accuracy and/or sufficiency of such information and/or suggestions, as to the product's merchantability or fitness for any particular purpose, or that any suggested use will not infringe any patent. Nouryon does not accept any liability whatsoever arising out of the use of or reliance on this information, or out of the use or the performance of the product. Nothing contained herein shall be construed as granting or extending any license under any patent. Customer must determine for himself, by preliminary tests or otherwise, the suitability of this product for his purposes.The information contained herein supersedes all previously issued information on the subject matter covered. The customer may forward, distribute, and/or photocopy this document only if unaltered and complete, including all of its headers and footers, and should refrain from any unauthorized use. Don’t copythis document to a website.Trigonox®, Nourytainer and Butanox are registered trademarks of Nouryon Functional Chemicals B.V. or affiliates in one or more territories.Contact UsPolymer Specialties Americas************************Polymer Specialties Europe, Middle East, India and Africa*************************Polymer Specialties Asia Pacific************************2023-9-11© 2023Thermoset composites Trigonox 44B。

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Modeltest 3.5 (May 2004)© David Posadadposada@uvigo.eshttp://darwin.uvigo.es/software/modeltest.htmlDISCLAIMERThis program is free software; you can redistribute it and/or modify it under the terms of the GNU General Public License as published by the Free Software Foundation; either version 2 of the License, or (at your option) any later version. This program is distributed in the hope that it will be useful, but WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License for more details.You should have received a copy of the GNU General Public License along with this program; if not, write to the Free Software Foundation, Inc., 59 Temple Place - Suite 330, Boston, MA 02111-1307, USA.IMPORTANT: Note than only the last versions of Modeltest (3.x) are compatible with the new PAUP* version (4.0). Also consult the PAUP web page (/index.html) for potential bugs that may interfere with ModeltestHISTORYVersion 3.5 (May 04):This is a minor update that does not affect the calculations., AIC weights were sorted by their value, but because these can be almost zero (zero for the computer) for several models, their order would not make sense in the light of the AIC values. Now the program order the AIC weights by the AIC scores.</ul>Version 3.4 (March 04): There was a typo printing the Rd value for K81uf+I. It was printing p-inv instead. (thanks to Michael Sorenson)Version 3.3 (Nov 03):Added options to include branch length estimates as parameters and to calculate AICc. Changed some option letters accordingly.Version 3.2 (March 03): Aesthetic changes. TrN+I had 5 df instead of 6.Version 3.1 (Jan 02): Akaike weights and AIC differences are now calculated. Several minor aesthetic variations.Version 3.07 (May 01): There was a bug that caused that the wrong set of likelihood scores to be printed in the first column when this option was selected.Version 3.06 (Apr 01): Print likelihood scores by default. In the windows version there was a bug by which the file scores.txt was always the standard input (Andy Vierstraete). Using GNU licencese (I should have done this a long time ago) (thanks to Naoki Takebayashi)Version 3.05 (Feb 01): In the windows version, the AIC[55] gave an AIC of 0 to the GTRIG. Now dimension is AIC[56] (Juan Suarez). TIM+G reported invariable sites instead of gamma shape (Cymon Cox)Version 3.04 (July 00): The program outputs now a block of commands to implement the likelihoodsettings in PAUP* for the best-fit model selected. The mixed chi-square distribution is added as default for the I and G tests.Version 3.0 beta 2 (December 99): Because in the new release of PAUP beta3, the likelihood score file includes now base frequencies estimates, the program was modified accordingly. The likelihood ratio tests are now explained with more detail, and the output of Modeltest is more consistent with the likelihood settings option in PAUP*.Version 3.0 beta 1 (December 99): 16 new models are added for a total now of 56 models. These models are variations of two main substitution schemes that I called TIM (transitional model) and TIV (transversional model). They are described in figure 1 below.Version 3.0 (February 99): several cosmetic variations. The output of Modeltest is designed now to specify the model selected accordingly to PAUP* likelihood settings.Version 2.1 (October 99): A bug in the selection of the minimum AIC, which implied that the model GTR+I+G could not be selected is solved. Also, the number of free parameter is redefined. Now JC is considered to have 0 free parameters and GTR+I+G 10. This would affect only a few AIC calculations.Version 2.0 (June 99): 40 models are includedVersion 1-1.06 (June 98): several aesthetic variationsI really appreciate the input from several users and would like to show my appreciation. Thank you very much!MODELTEST Citation:Posada D and Crandall KA 1998. Modeltest: testing the model of DNA substitution. Bioinformatics 14 (9): 817-818.BACKGROUNDAll phylogenetic methods make assumptions, whether explicit or implicit, about the process of DNA substitution (Felsenstein, 1988). For example, an assumption common to many phylogenetic methods is a bifurcating tree to describe the phylogeny of species (Huelsenbeck and Crandall, 1997). Consequently, all the methods of phylogenetic inference depend on their underlying models. To have confidence in inferences it is necessary to have confidence in the models (Goldman, 1993b). Because of this, all the methods based on explicit models of evolution should explore which is the model that fits the data best, justifying then its use.Likelihood ratio tests (LRT)In traditional statistical theory, a widely accepted statistic for testing the goodness of fit of models is the likelihood ratio test statistic! = –2 log ", being"=max LNullModel|Data()[]max L1AlternativeModel|Data() []where L 0 is the likelihood under the null hypothesis (simple model) and L 1 is the likelihood under the alternative hypothesis (more complex, parameter rich, model). The value of this statistic is always equal to or greater than zero, as the likelihood under the more complex model will always be equal or higher than the likelihood under the simpler model. When the models compared are nested (the null hypothesis is a special case of the alternative hypothesis) and the null hypothesis is correct,the ! statistic is asymptotically distributed as #2 with q degrees of freedom, where q is the difference in number of free parameters between the two models; equivalently, q is the number of restrictions on the parameters of the alternative hypothesis required to derive the particular case of the null hypothesis (Goldman, 1993b; Kendall and Stuart, 1979). To preserve the nesting of the models, the likelihood scores are estimated upon the same tree, and then, once the models have been compared,a final tree is estimated using the chosen model of evolution.When the models are not nested, an alternative means of generating the null distribution of the !statistic is through Monte Carlo simulation (parametric bootstrapping) (Goldman, 1993a). The #2approximation used to represent the underlying distribution of the LRT has been problematic.Goldman (1993b) first pointed out the difficulty in counting the number of degrees of freedom and the problem of the sparseness of the DNA data. Later, Yang et al. (1995) suggested that the LRT was well represented by a #2 distribution. However, the #2 distribution may not be reliable when the null model is equivalent to fixing some parameters at the boundary of the parameter space of the alternative model, e.g., rate homogeneity test, where the null hypothesis is a special case of the gamma-distribution model with shape parameter ($) equal to infinity (Yang, 1996). Whelan and Goldman (1999) have also shown that for comparisons of rate variation across sites and nucleotide frequencies estimated as the observed base frequencies, the #2 distribution was significantly different from the true distribution, and the tests were conservative. To account for the boundary problem Ota et al. (1992)and Goldman and Whelan (2000) suggested the use of a mixed !2(or ! 2)distribution consisting of 50% !02 and 50% !12to construct LRT tests for the invariable sites. Thismixed distribution for model fitting is implemented in the Modeltest 3.04 and future versions for the invariable sites and rate heterogeneity among sites LRTs.Akaike Information CriterionThe Akaike information criterion (AIC, (Akaike, 1974) is an asymptotically unbiased estimator of the Kullback-Leibler information quantity (Kullback and Leibler, 1951), which is a measure of the information that is lost when a model is used to approximate full reality. Selecting the model with the minimum AIC is approximately equivalent to minimizing the expected Kullback-Leibler distance between the true model and the estimated sample. The AIC penalizes for the increasing number of parameters in the model, so it is taking into account not only the goodness of fit but also the variance of the parameter estimates. The AIC is computed as:AIC i = -2 ln L i + 2 N i ,where N i is the number of free parameters in the i th model and L i is the maximum-likelihood value of the data under the i th sample.When sample size is small compared to the number of parameters (say, n /K < 40) the use of a second-order AIC, AIC c (Hurvich and Tsai, 1989; Sugiura, 1978), is recommended:AICc =AIC+2K(K+1)n!K!1,where sample size is approximated by the number of variable characters in the alignment (although which number to use is really up to the user).The AIC compares several candidate models simultaneously, it can be used to compare both nested and non-nested models, and model-selection uncertainty can be easily quantified using the AIC differences and Akaike weights. AIC differences (%I or deltas) are rescaled AICs:%i = AIC i – min AICThe AIC differences are easy to interpret and allow a quick comparison and ranking of candidate models. As a rough rule of thumb, models having %i within 1-2 of the best model have substantial support and should receive consideration. Models having %i within 3-7 of the best model have considerably less support, while models with %i > 10 have essentially no support. Akaike weights (w i) are the normalized relative AIC for each candidate model, and they can be interpreted, from a Bayesian perspective, as the probability that a model is the best approximation to the truth given the data:wi =exp(!1/2"i)exp(!1/2"r) r=1R#for R candidate models. Indeed, we could also think of estimating phylogenies under the best models and combine these trees according to their Akaike weights Burnham and Anderson (2003) provide an excellent introduction to the AIC and model selection.Evaluation of model selectionPosada and Crandall (2001a, 2000b) and Posada (2001) have evaluated the performance of different model selection strategies.THE PROGRAMMODELTEST is a simple calculator written in ANSI C and compiled for the Power Macintosh and Windows 95/NT using Metrowerks CodeWarrior. Source code in ANSI C is provided, along with a Makefile for compilation with gcc (or cc) in Unix-like environments. It is designed to compare different nested models of DNA substitution in a hierarchical hypothesis-testing framework (Figure 1). MODELTEST calculates the likelihood ratio test statistic ! = –2 log " and its associated P-value using a #2 distribution with q degrees of freedom in order to reject or fail to reject different null hypothesis about the process of DNA substitution. It also calculates the AIC estimate associated with each likelihood score, the AIC differences and the Akaike weights.UsageThe user communicates with the program using a standard console interface (Figure 2), in Macintosh machines where the input and output files can be specified, By clicking with the mouse in the left File button, the user can select an INPUT FILE. By clicking in the right File button, the user can specify an OUTPUT FILE (the default output is to the Console in the screen). In the Argumentline the user can interact with the program. In Windows (DOS window) (Figure 3) and Unix machines the users interacts with the program through a command or argument line (Figure 4). These are the options:-d : debug level (e.g. -d2)-a : alpha level (e.g. -a0.01)-c : sample size or number of characters (all or just variable). Forces the use of AICc-t : number of taxa. Forces to include branch lengths as parameters-l : likelihood Ratio calculator mode-i : AIC calculator mode-f : input from a file for obtaining AIC values-? : help\nDefault ModeBy default, the program will accept two classes of input files: a file containing ordered raw log likelihood scores and parameter estiamtes corresponding to the tested models (JC, JC+I, JC+G, JC+I+G, K80, K80+I, K80+G, K80+I+G, TrNef, TrNef+I, TrNef+G, TrNef+I+G, K81, K81+I, K81+G, K81+I+G, TVMef, TVMef+I, TVMef+G, TVMef+I+G, TIMef, TIMef+I, TIMef+G, TIMef+I+G, SYM, SYM+I, SYM+G, SYM+I+G, F81, F81+I, F81+G, F81+I+G, HKY, HKY+I, HKY+G, HKY+I&, TrN, TrN+I, TrN+G, TrN+I+G, K81uf, K81uf+I, K81uf+G, K81uf+I+G, TVM, TVM+I, TVM+G, TVM+I+G, TIM, TIM+I, TIM+G, TIM+I+G GTR, GTR+I, GTR+G, GTR+I+G; I: invariable sites; G: gamma distribution; see Figure 1 for abbreviations) and a PAUP* (Swofford, 1998) file containing a matrix of the same log likelihood scores resulting from the execution of a block of PAUP* commands. This block of PAUP (modelblock) commands is included in the package.Debug level (-d)This is a programming feature that does not affect the calculations. This option is for development, and not for usage, of the program.. If you don’t know what is this, don't worry; simply do not use it…Alpha level (-a)The user can set the alpha level of significance (by default this is 0.01) in the command line, inputting –a followed by the desired value. The program will use this level of significance in all its calculations.Sample size (-c)If this option is specified, the corrected AIC (AICc) will be use instead of the standard AIC (AIC). At the same time, the number of characters (e.g., -c500) needs to be specified. This should be actually the sample size, which is not an obvious quantity in phylogenetics. A conservative approach would be to specify here the number of variable characters.Number of taxa (-t)If this option is specified, the number of branches will be included when counting which free parameters have been estimated. This will not change the order of the AIC scores, but possibbly their relative differences.LRT calculator Mode (-l)This is a useful mode when the user wants to calculate likelihood ratio tests and their associate probability for different hypotheses, or only some of the hypothesis tested by default by Modeltest. As the P-value is calculated using a chi-square distribution, the models tested should be nested (the null hypothesis is a special case of the alternative hypothesis). The user is guided by prompts for inputting a pair of likelihood scores and the number of degrees of freedom. Modeltest performs the likelihood ratio test and calculates its associated P-value using a chi-square distribution. In this case the user is responsible for calculating the appropriate number of degrees of freedom and log likelihood scores for testing the intended hypotheses.AIC calculator mode (-i)This mode is aimed to provide the user with a fast calculation of the AIC values corresponding to the likelihood scores. In this case, the models do not need to be nested. The user is guided by prompts for inputting the number of log likelihood scores, the positive log likelihood scores, and the corresponding number of free parameters.Input file for obtaining AIC estimates (-f)If the user is interested in inputting a large number of scores for obtaining the AIC estimates, one can input a file with two columns of data: the positive likelihood scores in one column with the corresponding number of free parameters in the same row constituting the second column.Help (-?)By typing “-?” in the command line, the user can have access to some help. Nevertheless, the lecture of the manual is encouraged…OutputThe output of MODELTEST consists of a description of the likelihood ratio tests performed, and their associated P-values. The null hypotheses tested are described in Figure 1. The program interprets the resulting P-values and chooses the model that fits the data best among those tested following the likelihood ratio test and/or AIC criteria, using a default individual alpha value of 0.01 (for maintaining an overall alpha value of 0.05, the standard Bonferroni correction -alpha/number of tests- results in a individual alpha value of 0.01), or another value specified by the user. The program also calculates the AIC values, indicating the smallest, the AIC differences (deltas) and the Akaike weights. Note that when the equal ti/tv (transition/transversion) rates hypothesis is not rejected, the equal ti and equal tv rates hypotheses are automatically rejected, and then will not be tested.Often, the hLRT and the AIC result in the selection of different models. It is up to the user to decide which model selection criteria is going to use.PACKAGEThe MODELTEST package includes several files in different subdirectories:README.html: quick instructions and comments for the users./batch/modelblockPAUPb10: the batch file with PAUP* commands to obtain likelihood scores for the competing models in the proper format for MODELTEST/bin/Modeltest3.5.mac.app: A Macintosh (OS X) executable/bin/Modeltest3.5.win.exe: A Windows executable/doc/Modeltest3.5.pdf: Documentation in PDF format/license/gpl.html: GNU general public license in HTML format/sample/sample.log: a log file describing the calculations performed by PAUP* to obtain sample.scores/sample/sample.nex: an example data file in NEXUS format/sample/sample.out: the output file of MODELTEST resulting from the analysis of sample.scores. /sample/sample.scores: file with likelihood scores produces by *PAUP after loading sample.nex and executing the modelblockPAUPb10batch file./source/Makefile: Makefile for compilation of MODELTEST in UNIX-like environments/source/Modeltest3.5.c: C source codeExample fileThe example file (sample.nex) included in MODELTEST it is a simulated data set with 10 aligned DNA sequences 1000 bp long. This alignment was simulated on a tree obtained from coalescent process and under the HKY+I model, with the next parameter values:Effective population size = 10000Mutation rate per nucleotide per site = 5e-5Base frequencies (A, C, G, T) = 0.4, 0.2, 0.1, 0.3Transition/transversion rate = 4Alpha parameter of the gamma distribution = 0.4Modeltest hierarchyFigure 1. Hierarchical hypothesis testing in MODELTEST. At each level the null hypothesis (upper model) is either accepted (A) or rejected (R). The models of DNA substitution are: JC (Jukes and Cantor, 1969), K80 (Kimura, 1980), TrNef (TrN equal base frequencies; see below), K81 (Kimura, 1981), TIMef (TIM with equal base frequencies), TIV (TIV with equal base frequencies), SYM (Zharkikh, 1994), F81 (Felsenstein, 1981), HKY (Hasegawa et al., 1985), TrN (Tamura and Nei, 1993), K81uf (K81 unequal base frequencies; see above), TIM, TIV, and GTR (Tavaré, 1986). G: shape parameter of the gamma distribution; I: proportion of invariable sites. Df: degrees of freedom.Table 1. Model names. Some models have no reference (TNef, K81uf, TIMef, TIM, TVMef, TVM), they are just some variations of some existing models, and they were no developed but just named by me.Model NameJC Jukes and Cantor (Jukes and Cantor, 1969)F81Felsenstein 81 (Felsenstein, 1981)K80Kimura 80 (=K2P) (Kimura, 1980)HKY Hasegawa, Kishino, Yano 85 (Hasegawa, Kishino and Yano, 1985)TNef Tamura-Nei equal frequenciesTN Tamura-Nei (Tamura and Nei, 1993)K81Two transversion-parameters model 1 (=K81=K3P) (Kimura, 1981)K81uf Two transversion-parameters model 1 unequal frecuenciesTIMef Transitional model equal frecuenciesTIM Transitional modelTVMef Transversional model equal frecuenciesTVM Transversional modelSYM Symmetrical model (Zharkihk, 1994)GTR General time reversible (=REV) (Tavaré, 1986)Table 2. Model parameters.The substitution codes are just two ways of indicating the substitution scheme. Any of these models can ignore rate variation or include invariable sites (+I), rate variation among sites (+G), or both (+I+G).ModelFreeparametersBasefrequenciesSubstitutionratesSubstitutioncode 1Substitutioncode 2JC0equal a=b=c=d=e=f000000aaaaaa F813unequal a=b=c=d=e=f000000aaaaaa K801equal a=c=d=f, b=e010010abaaba HKY4unequal a=c=d=f, b=e010010abaaba TNef2equal a=c=d=f, b, e010020abaaca TN5unequal a=c=d=f, b, e010020abaaca K812equal a=f, c=d, b=e012210abccba K81uf5unequal a=f, c=d, b=e012210abccba TIMef3equal a=f, c=d, b, e012230abccda TIM6unequal a=f, c=d, b, e012230abccda TVMef4equal a, c, d, f, b=e012314abcdbe TVM7unequal a, c, d, f, b=e012314abcdbe SYM5equal a, c, d, f, b, e012345abcdef GTR8unequal a, c, d, f, b, e012345abcdefSelect input file Select output file Figure 2. Console Interface for MacintoshFigure 3. Macintosh outputFigure 4. Command prompt in WindowsFigure 5. Unix console (Unix, Linux, MacOS X console...)RUNNING THE PAUP COMMANDS BLOCKThe input of Modeltest is likelihood scores corresponding to the specific data set and each one of 40 models. The easiest way of obtaining these scores from an alignment of DNA sequences is using PAUP*. A block of commands for PAUP* is provided below in the commands file ("modelblock3"). Follow these steps:1) Open your data file and execute it in PAUP2) Open the command file (modelblock) and execute it3) Paup starts to work in the data following the commands. Once is finished you will see a file called "model.scores" in the same directory as the command file4) Run the file "model.scores" through modeltestAlternatively, if you are familiar with PAUP*, you can add the PAUP* commands after your data block directly in your data file and execute it.REFERENCESA KAIKE, H. 1974. A new look at the statistical model identification. IEEE Transactions onAutomatic Control 19:716-723.B URNHAM, K. P., and D. R. A NDERSON. 2003. Model selection and multimodel inference: apractical information-theoretic approach. Springer-Verlag, New York, NY.F ELSENSTEIN, J. 1981. Evolutionary trees from DNA sequences: A maximum likelihood approach.J. Mol. Evol. 17:368-376.F ELSENSTEIN, J. 1988. Phylogenies from molecular sequences: inference and reliability. Annu. Rev.Genet. 22:521-565.G OLDMAN, N. 1993a. Simple diagnostic statistical test of models of DNA substitution. J. Mol. Evol.37:650-661.G OLDMAN, N. 1993b. Statistical tests of models of DNA substitution. J. Mol. Evol. 36:182-198.G OLDMAN, N., and S. W HELAN. 2000. Statistical tests of gamma-distributed rate heterogeneity inmodels of sequence evolution in phylogenetics. Mol. Biol. Evol. 17:975-978.H ASEGAWA, M., K. K ISHINO, and T. Y ANO. 1985. Dating the human-ape splitting by a molecularclock of mitochondrial DNA. J. Mol. Evol. 22:160-174.H UELSENBECK, J. P., and K. A. C RANDALL. 1997. Phylogeny estimation and hypothesis testingusing maximum likelihood. Annu. Rev. Ecol. Syst. 28:437-466.H URVICH, C. M., and C.-L. T SAI. 1989. Regression and time series model selection in smallsamples. Biometrika 76:297-307.J UKES, T. H., and C. R. C ANTOR. 1969. Evolution of protein molecules. Pages 21-132 in Mammalian Protein Metabolism (H. M. Munro, ed.) Academic Press, New York, NY.K ENDALL, M., and A. S TUART. 1979. The Advanced Theory of Statistics, 4th edition. Charles Griffin, London.K IMURA, M. 1980. A simple method for estimating evolutionary rate of base substitutions through comparative studies of nucleotide sequences. J. Mol. Evol. 16:111-120.K IMURA, M. 1981. Estimation of evolutionary distances between homologous nucleotide sequences.Proc. Natl. Acad. Sci. USA 78:454-458.K ULLBACK, S., and R. A. L EIBLER. 1951. On information and sufficiency. Ann. Math. Stat. 22:79-86.O HTA, T. 1992. Theoretical study of near neutrality. II. Effect of subdivided population structure with local extinction and recolonization. Genetics:917-923.S UGIURA, N. 1978. Further analysis of the data by Akaike's information criterion and the finite corrections. Comm. Statist. Theor. Meth. A7:13-26.S WOFFORD, D. L. 1998. PAUP* Phylogenetic analysis using parsimony and other methods, version4.0 beta. Sinauer Associates.T AMURA, K., and M. N EI. 1993. Estimation of the number of nucleotide substitutions in the control region of mitochondrial DNA in humans and chimpanzees. Mol. Biol. Evol. 10:512-526.T AVARÉ, S. 1986. Some probabilistic and statistical problems in the analysis of DNA sequences.Pages 57-86 in Some mathematical questions in biology - DNA sequence analysis (R. M.Miura, ed.) Amer. Math. Soc., Providence, RI.W HELAN, S., and N. G OLDMAN. 1999. Distributions of statistics used for the comparison of models of sequence evolution in phylogenetics. Mol. Biol. Evol. 16:1292-1299.Y ANG, Z. 1996. Maximum-likelihood models for combined analyses of multiple sequence data. J.Mol. Evol. 42:587-596.Y ANG, Z., N. G OLDMAN, and A. F RIDAY. 1995. Maximum likelihood trees from DNA sequences: a peculiar statistical estimation problem. Syst. Biol. 44:384-399.Z HARKIKH, A. 1994. Estimation of evolutionary distances between nucleotide sequences. J. Mol.Evol. 39:315-29.。

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