slides3_05

合集下载

蓝绿科技欧美风ppt模板

蓝绿科技欧美风ppt模板
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IMAGE WITH DESCRIPTION
PLACEHOLDER
• Placeholder • Placeholder
1. The text demonstrates how your own text will look when you replace the placeholder with your own text.
when you replace the placeholder with your own text. This is a placeholder text. This is a placeholder text.
DOUGHNUT CHART WITH SECTIONS
Example 1 Example 2 Example 3 Example 4 Example 5 Example 6
For replacing the placeholder text you need to click on the placeholder text and insert your own text.
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T
Threats
The text demonstrates how your own text will look when you replace the placeholder with your own text.
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CHARTPOOL
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AGENDA
01 Title slides 02 Text slides 03 Image slides 04 Diagrams 05 Tables and Timetables
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06 Prozessgrafiken 07 Organisationsgrafiken 08 Projektfolien 09 Maps 10 Icons & Mobile Devices

工作汇报用什么软件

工作汇报用什么软件

工作汇报用什么软件在现代工作中,工作汇报已成为企业管理中不可或缺的一部分。

通过工作汇报,可以使领导和下属都能够清楚地了解到工作进展情况和达成的成果。

因此,选择一款合适的工作汇报软件非常重要。

下面详细介绍几款主流的工作汇报软件。

1. Microsoft PowerPoint (PowerPoint)PowerPoint是一款广泛使用的演示文稿软件,也在工作汇报中得到了广泛的应用。

Power Point的主要特点是操作简单,不需要过多的设计技巧,且支持多种不同的文件格式导入,例如视频、音频、图片等,用于幻灯片演示非常方便。

除此以外,还支持制作动态图表、动画效果、并具有多种幻灯片设计模板可供选择。

另外,还具有云端存储功能,支持多人协作,方便分享和修改。

因此,PowerPoint是一款非常多功能的软件,非常适合用于工作汇报。

2. Microsoft Excel(Excel)Excel是一款电子表格软件,具有强大的计算能力、数据处理和统计分析功能。

Excel可以制作各种表格、图表、公式等,支持多种数据格式导入和导出。

在工作汇报中,Excel可以用于数据分析、预算报表、进度计划表等方面。

利用Excel分析数据可以帮助更好地了解工作进展情况,并为下一步的工作做出更好的决策。

因此,Excel也可以作为一款重要的工作汇报软件。

3. Google SlidesGoogle Slides是一个免费在线演示文稿软件,特点是简单易用、数据协作方便,适合私人、学校和企业用户使用。

GoogleSlides支持多种语言和操作系统,兼容Smartphone、PC等各种终端,方便用户随时随地进行幻灯片制作和编辑。

Google Slides还具有实时协作功能,多人协作可实现同时编辑幻灯片、添加注释、修改数据等,方便各部门之间的跨职能协作。

另外,Google Slides 提供了多种演示文稿模板,可供用户根据需求进行选择,快速制作出精致的幻灯片。

老师ppt课件常用软件

老师ppt课件常用软件
提高演示的质量和效果。
导出为PDF
用户可以将PPT导出为PDF格 式,方便分享和阅读。
使用技巧
1 2
快速制作幻灯片
用户可以使用模板中的占位符,快速添加文本、 图片等内容,提高制作效率。
自定义动画效果
用户可以自定义动画效果的速度、方向、出场方 式等,制作出更加个性化的PPT。
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批量替换字体和字号
用户可以使用“批量替换”功能,快速替换所有 幻灯片中的字体和字号。
通过自定义动画效果,可以让演示文稿更加生动有趣。
幻灯片的布局和结构
合理安排幻灯片的布局和结构,可以让演示文稿更加清晰易懂。
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金山WPS演示
软件特点
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兼容性强
金山WPS演示可以兼容多 种文件格式,如.docx、 .pptx等,能很好地满足用 户的多种需求。
轻量级软件
金山WPS演示相较于其他 同类软件,安装包体积更 小,运行更快,更流畅。
跨平台支持
除了Windows和Mac OS X平台, PowerPoint还支持在移动设备上使 用,方便用户随时随地进行编辑和 展示。
功能介绍
模板和主题
PowerPoint提供了大量的模板 和主题,可以帮助用户快速创 建出具有专业水准的演示文稿

图表和图形
PowerPoint支持插入各种图表 和图形,如柱状图、折线图、 饼图等,以及自定义图形和符 号。
界面简洁
金山WPS演示的界面设计 简洁直观,操作便捷,容 易上手。
功能介绍
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02
03
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多种模板
金山WPS演示提供了多种模 板,用户可以根据自己的需求 选择合适的模板持添加多种 动画效果,让PPT更加生动、

FAA AD issuance - AD 2012-14-05- Slide release cable- ATA 52

FAA AD issuance - AD 2012-14-05-  Slide release cable- ATA 52

FAAAviation Safety AIRWORTHINESS DIRECTIVE /aircraft/safety/alerts//fr/advanced.html2012-14-05 Airbus: Amendment 39-17119. Docket No. FAA-2012-0266; Directorate Identifier 2011-NM-061-AD.(a) Effective DateThis airworthiness directive (AD) becomes effective August 21, 2012.(b) Affected ADsNone.(c) ApplicabilityThis AD applies to all Airbus Model A318-111, -112, -121, and -122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; and Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes; certificated in any category; all serial numbers.(d) SubjectAir Transport Association (ATA) of America Code 28: Fuel tanks; 53: Fuselage.(e) ReasonThis AD was prompted by reports of unsuccessful slide deployments during scheduled deployment tests, and failed functional tests of the release travel of the slide release mechanism. We are issuing this AD to prevent non-availability of left- or right-hand off-wing exit slides that could impair emergency evacuation of the passengers and flightcrew, and could result in personal injuries.(f) ComplianceYou are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done.(g) Inspection and ModificationExcept as provided by paragraph (k) of this AD, within 36 months after the effective date of this AD, inspect the off-wing slide release cables on the left- and right-hand sides to determine whether part number (P/N) L32A319-160-001 is installed. A review of airplane maintenance records is acceptable in lieu of this inspection if the part number of the off-wing slide release cables can be conclusively determined from that review. If any off-wing slide release cable has P/N L32A319-160-001, before further flight, replace with a new off-wing slide release cable having P/N L32A320-180, in accordance with the Accomplishment Instructions of Airbus Mandatory Service Bulletin A320-53-1227, Revision 05, dated March 27, 2012.(h) Optional ModificationInstallation of a shorter off-wing slide release cable having P/N L32A319-160-002 with relocated inflation bottle during installation of the additional center tank, in accordance with the Accomplishment Instructions of the applicable service bulletin identified in paragraphs (h)(1) through(h)(4) of this AD, is acceptable for compliance with the requirements of paragraph (g) of this AD.(1) Airbus Service Bulletin A320-28-1118, Revision 03, including Appendix 1, dated May 12, 2009.(2) Airbus Service Bulletin A320-28-1132, Revision 04, including Appendices 1 and 2, dated February 1, 2010.(3) Airbus Service Bulletin A320-28-1145, Revision 01, including Appendix 01, dated April 27, 2007.(4) Airbus Service Bulletin A320-28-1154, Revision 01, dated April 7, 2008.(i) Parts Installation ProhibitionAs of the effective date of this AD, no person may install an off-wing slide release cable having P/N L32A319-160-001 on any airplane.(j) Credit for Previous Actions(1) This paragraph provides credit for the actions required by paragraph (g) of this AD, if installation of off-wing slide release cables having P/N L32A320-180 was done before the effective date of this AD using the service bulletin identified in paragraphs (j)(1)(i) through (j)(1)(v) of this AD.(i) Airbus Service Bulletin A320-53-1227, dated March 24, 2010.(ii) Airbus Service Bulletin A320-53-1227, Revision 01, dated May 31, 2010.(iii) Airbus Mandatory Service Bulletin A320-53-1227, Revision 02, dated March 10, 2011.(iv) Airbus Mandatory Service Bulletin A320-53-1227, Revision 03, dated July 28, 2011.(v) Airbus Mandatory Service Bulletin A320-53-1227, Revision 04, dated February 14, 2012.(2) This paragraph provides credit for the actions specified in paragraph (h) of this AD, if those actions were performed before the effective date of this AD using the service information specified in paragraphs (j)(2)(i) through (j)(2)(v) of this AD.(i) Airbus Service Bulletin A320-28-1132, dated October 13, 2004.(ii) Airbus Service Bulletin A320-28-1132, Revision 01, dated October 12, 2006.(iii) Airbus Service Bulletin A320-28-1132, Revision 02, dated November 12, 2008.(iv) Airbus Service Bulletin A320-28-1132, Revision 03, dated October 5, 2009.(v) Airbus Service Bulletin A320-28-1145, dated February 28, 2006.(k) ExceptionProvided that off-wing slide release cables have not been replaced with a slide release cable having P/N L32A319-160-001, airplanes having Airbus modification 150811, 26138, 37856, or 39673 installed in production are in compliance with the requirements of paragraph (g) of this AD.(l) Other FAA AD ProvisionsThe following provisions also apply to this AD:(1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sendinginformation directly to the International Branch, send it to ATTN: Sanjay Ralhan, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, Washington 98057-3356; telephone (425) 227-1405; fax (425) 227-1149. Information may be emailed to: 9-ANM-116-AMOC-REQUESTS@. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office. The AMOC approval letter must specifically reference this AD.(2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered FAA-approved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service.(m) Related InformationRefer to MCAI European Aviation Safety Agency Airworthiness Directive 2011-0015, dated January 31, 2011, and the service information specified in paragraphs (m)(1) through (m)(5) of this AD, for related information.(1) Airbus Service Bulletin A320-28-1118, Revision 03, including Appendix 1, dated May 12, 2009.(2) Airbus Service Bulletin A320-28-1132, Revision 04, including Appendices 1 and 2, dated February 1, 2010.(3) Airbus Service Bulletin A320-28-1145, Revision 01, including Appendix 01, dated April 27, 2007.(4) Airbus Service Bulletin A320-28-1154, Revision 01, dated April 7, 2008.(5) Airbus Mandatory Service Bulletin A320-53-1227, Revision 05, dated March 27, 2012. (n) Material Incorporated by Reference(1) The Director of the Federal Register approved the Incorporation by Reference (IBR) of the following service information under 5 U.S.C. 552(a) and 1 CFR part 51.(2) You must use the following service information to do the actions required by this AD, unless the AD specifies otherwise.(i) Airbus Mandatory Service Bulletin A320-53-1227, Revision 05, dated March 27, 2012.Reserved(ii)(3) If you accomplish the optional actions specified by this AD, you must use the following service information to perform those actions, unless the AD specifies otherwise.(i) Airbus Service Bulletin A320-28-1118, Revision 03, including Appendix 1, dated May 12, 2009.(ii) Airbus Service Bulletin A320-28-1132, Revision 04, including Appendices 1 and 2, dated February 1, 2010.(iii) Airbus Service Bulletin A320-28-1145, Revision 01, including Appendix 01, dated April 27, 2007.(iv) Airbus Service Bulletin A320-28-1154, Revision 01, dated April 7, 2008.(4) For service information identified in this AD, contact Airbus, Airworthiness Office–EAS, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61 93 44 51; email account.airworth-eas@; Internet .(5) You may review copies of the service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington. For information on the availability of this material at the FAA, call 425-227-1221.(6) You may also review copies of the service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of thismaterial at an NARA facility, call 202-741-6030, or go to /federal_register/ code_of_federal_regulations/ibr_locations.html.Issued in Renton, Washington, on June 29, 2012.Kalene C. Yanamura,Acting Manager, Transport Airplane Directorate,Aircraft Certification Service.。

slides8_05

slides8_05

User documentation
• This is documentation for the user of your program • It is the "user manual" • Entire books have been written on the subject and I don't intend to cover it here • Feel free to include user documentation for your project if you want (but not too much of it)
How to write good comments
• Does your comment help your reader understand the code? • Are you writing a comment just because you know that "comments are good"? • Is the comment something that the reader could easily work out for themselves? • Don't be afraid to add a reference instead of a comment for tricky things
Some common bad comments
i= i+1; /* Add one to i */
for (i= 0; i < 1000; i++) { /* Tricky bit */ . . Hundreds of lines of obscure uncommented code here . } int x,y,q3,z4; /* Define some variables */ int main() /* Main routine */

希沃ppt 课件

希沃ppt 课件

行间距和段间距
适当调整行间距和段间距 ,使文字排版更加美观和 易读。
图片处理技巧
图片选择
选用与主题相关的图片, 确保图片质量清晰、色彩 鲜艳。
图片裁剪
根据需要裁剪图片,突出 重点,去除不必要的背景 。
图片调整
调整图片的亮度和对比度 ,使图片更加生动和鲜明 。
动画效果应用
动画类型
选择适当的动画效果,如淡入淡 出、飞入飞出等,避免过度使用
在线测试
希沃ppt提供了多种在线测试题型,如选择题、 填空题等,方便教师进行课堂测试和作业布置。
即时反馈
测试结果能够即时反馈给学生和教师,帮助学生 了解自己的掌握情况,教师则可以根据反馈调整 教学策略。
数据统计
测试结果可以进行数据统计和分析,帮助教师全 面了解学生的学习状况,为后续教学提供参考依 据。
学习成果。
教学内容选择
相关性
确保教学内容与教学目标相一致,能够有效地支 持教学目标的实现。
适宜性
根据学生的年龄、认知水平和兴趣选择适宜的教 学内容,以提高学生的学习兴趣。
完整性
确保教学内容的完整性,涵盖所有必要的主题和 知识点。
教学方法选择
多样性
根据不同的教学内容和教学目标,选择多种教学方法,如讲解、 示范、小组讨论、案例分析等。
Articulate Storyline
专业的课件制作软件,提供丰富的交互式组 件和模板,适合制作高质量的课件。
02
希沃ppt制作技巧
文字排版技巧
01
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字体选择
选择清晰易读的字体,如 微软雅黑、宋体等,避免 使用过于花哨的字体。
字号大小
根据演示场合和观众人数 ,合理设置字号大小,确 保观众能够清晰地看到内 容。

05-DEPLOY-Slides

05-DEPLOY-Slides

Basic Deployment-1
© 2007 BEA Systems, Inc.
237
Road Map
1.
Web Servers
– – – Web Servers Defined HTTP Static and Dynamic Content
2. 3. 4. 5.
Web Applications EJB Applications Enterprise Applications Deployment
Basic Deployment-13
© 2007 BEA Systems, Inc.
249
Configuring Web Applications
f Web applications are configured through deployment
descriptors web.xml and weblogic.xml which:
3. 4. 5.
EJB Applications Enterprise Applications Deployment
Basic Deployment-10
© 2007 BEA Systems, Inc.
246
What Is a Web Application?
f A Web application is a group of server-side resources
© 2007 BEA Systems, Inc.
WLS Retrieves Resource 2
3 HTTP Response
Basic Deployment-4
240
MIME Types
f Multipurpose Internet Mail Extensions (MIME) is a

巴克尔(Parker)小型和标准尺寸球轨滑动轨道说明书

巴克尔(Parker)小型和标准尺寸球轨滑动轨道说明书

Contents14-15Overview21-22 1.75” (44,5 mm) Wide 23-25 2.62” (66,5 mm) Wide 26-27 5.00” (127,0 mm) Wide 28 6.00” (152,4 mm) Wide 31-34Performance CurvesBall Bearing SlidesMiniature and StandardBall BearingSlidesMiniature and Standard Size Ball Bearings SlidesBall Slide Design PrinciplesParker ball slides are mechanically simple linear motion devices comprised of a stationary base member witha mobile carriage riding on top. Two rows of hardened steel balls on both sides of the base provide the smooth, accurate, low friction sliding motion between the stationary base and the top slide. Each row of bearings is contained between four hardened and precision ground steel rods. These bearing assemblies are factory preloaded to eliminate wobble and unwanted play in the system.Ball slides are functionally much more reliable than simple dovetail slides, since there is no direct sliding contact of the top and bottom members. Ball slides eliminate the rapid wear problems, regular lubrication requirements, and “stiction” (skipping and jumping caused by the increased force needed to initiate movement) characteristic of dovetail slides. Parker also offers a high load capacity, long life crossed roller slides for applications requiring maximum load and life performance.Standard FeaturesAll models offer high quality construction features as standard:•Straight line accuracy of 0.00008 inches per inch of travel (0.00025 inches per inch of travel for miniatures)•Precision machined mounting surfaces to assure flatness and parallelism•Factory preloaded to precision specifications to eliminate any side play and provide a uniform coefficient of friction•Factory threaded mounting holes on the top for easy payload mounting•Factory machining services for special holeconfigurations and custom modifications•Locking thread inserts on preloaded screws for maintenance-free life without loss of preload •Hardened and precision machined 440C stainless steel balls and rodsHow to OrderUse the overview chart on the following page to select the appropriate ball slide. Refer to the individual specifications page for complete performance and mechanical specifications. To order ball slides, use the model number corresponding to the specific size and travel length selected.A variety of modifications to standard models are available to meet custom requirements. Contact our application engineering department with your design specifications.B a l l B e a r i n g S l i d esSeriesWidth in (mm)Travel Normal Load MountingPage in (mm)lbs (kg)Imperial Metric0.5(12,7) 4.95.017.0(2,2)(2,3)(7,6)•••161718SelectionB a l l B e a r i n g S l i d es4000/M4000 SeriesSpecifications Imperial Metric Travel: 1.0 in 25,4 mm Size: Width Length Height1.75 in 1.75 in 0.75 in 44,5 mm 44,5 mm 19,0 mm Load:NormalMoment: Yaw, Pitch, Roll 25 lbsSee page 3111 kgSee page 31Straight line accuracy:0.00008 in/in of travel 2 µm/25 mm of travel Weight: 0.2 lbs0,09 kgConstruction:Aluminum top and base/ 440C stainless steel bearings Mounting surface:Precision machined Finish:Black anodizeModelTravel Aperture Imperial 4001 1.0 in 0.50 in 4005 1.0 in —MetricM400125,4 mm 12,7 mm M400525,4 mm—Qty. (4) Mtg. Holes (Top)Imperial Models – #6-32 Thd. on 1.12 Dia. B.C.Metric Models – M4 Thd. on (30,0) Dia. B.C.Metric Models – M4 S.H.C.S.Dimensions in (mm)Ball Bearing SlidesTravel: 1.0 – 3.0 in 25,4 – 76,2 mm Size: Width Length Height1.75 in2.00 – 4.00 in 0.75 in 44,5 mm50,8 – 101,6 mm 19,0 mm Load:NormalMoment: Yaw, Pitch, Roll 28 – 55 lbs See page 3113 – 25 kg See page 31Straight line accuracy:0.00008 in/in of travel 2 µm/25 mm of travel Weight: 0.2 – 0.6 lbs0,09 – 0,27 kgConstruction:Aluminum top and base/ 440C stainless steel bearings Mounting surface:Precision machined Finish:Black anodizeNormal Load Weight DimensionsA B C D E F Imperial41011.0 in 28 lbs 0.2 lbs2.00 in 1.38 in 0.31 in 0.25 in 834201 2.0 in 40 lbs 0.4 lbs3.00 in 2.38 in 0.31 in 0.25 in 1254301 3.0 in 55 lbs 0.6 lbs4.00 in 3.38 in 0.31 in 0.25 in 167MetricM410125,4 mm 13 kg 0,09 kg 50,8 mm 35,0 mm 7,8 mm 12.9 mm 62M420150,8 mm 18 kg 0,18 kg 76,2 mm 60,0 mm 8,1 mm 13,1 mm 104M430176,2 mm25 kg0,27 kg101,6 mm85,0 mm8,3 mm13,3 mm146“E” Mtg. Holes (Top)Imperial Models – #6-32 Thd.Metric Models – M4 Thd.4100/M4100, 4200/M4200, 4300/M4300 SeriesDimensions in (mm)B a l l B e a r i n g S l i d es4500/M4500 SeriesSpecifications Imperial Metric Travel: 1.0 in 25,4 mm Size: Width Length Height2.62 in 2.62 in 1.00 in 66,5 mm 66,5 mm 25,4 mm Load:NormalMoment: Yaw, Pitch, Roll 62 lbsSee page 3128 kgSee page 31Straight line accuracy:0.00008 in/in of travel 2 µm/25 mm of travelWeight: 4501 – 0.6 lbs 4505 – 0.5 lbsM4501 – 0,27 kg M4505 – 0,23 kgConstruction:Aluminum top and base/ 440C stainless steel bearings Mounting surface:Precision machined Finish:Black anodizeModelTravel ApertureImperial 4501 1.0 in —4505 1.0 in 1.00 in MetricM450125,4 mm —M450525,4 mm25,4 mmQty. (8) Mtg. Holes (Top)Imperial Models – #10-32 Thd. on 2.00 Dia. B.C.Metric Models – M5 Thd. on (50,0) Dia. B.C.Metric Models – M6 S.H.C.S.Dimensions in (mm)Ball Bearing SlidesTravel: 2.0 – 4.0 in 50,8 – 101,6 mm Size: Width Length Height2.62 in4.00 – 6.00 in 1.00 in 66,5 mm101,6 – 152,4 mm 25,4 mm Load:NormalMoment: Yaw, Pitch, Roll 88 – 123 lbs See page 3240 – 56 kg See page 32Straight line accuracy:0.00008 in/in of travel2 µm/25 mm of travelWeight: 0.9 – 1.4 lbs 0,41 – 0,64 kgConstruction:Aluminum top and base/ 440C stainless steel bearings Mounting surface:Precision machined Finish:Black anodizeNormal Load Weight DimensionsA B C D E F G Imperial46012.0 in 88 lbs 0.9 lbs 4.00 in 0.5 in —6 2.00 in 0.69 in 0.31 in 47013.0 in 100 lbs 1.1 lbs 5.00 in 1.0 in —6 2.00 in 1.19 in 0.31 in 48014.0 in 123 lbs 1.4 lbs 6.00 in0.5 in1.0 in 102.00 in 1.69 in 0.31 in MetricM460150,8 mm 40 kg 0,41 kg 101,6 mm 12,5 mm —650,0 mm 12,5 mm 13,3 mm M470176,2 mm 48 kg 0,50 kg 127,0 mm 25,0 mm —650,0 mm 25,0 mm 13,5 mm M4801101,6 mm56 kg0,64 kg152,4 mm 12,5 mm25,0 mm1050,0 mm25,0 mm26,2 mmImperial Models – 1/4” S.H.C.S.Metric Models – M6 S.H.C.S.4600/M4600, 4700/M4700, 4800/M4800 SeriesDimensions in (mm)B a l l B e a r i n g S l i d es4600 SeriesSpecifications Travel: 6.0 – 15.0 in Size: Width Length Height2.62 in9.00 –18.00 in 1.00 inLoad:NormalMoment: Yaw, Pitch, Roll154 – 243 lbs See page 32-33Straight line accuracy:0.00008 in/in of travel Weight: 2.3 – 4.7 lbsConstruction:Aluminum top and base/ 440C stainless steel bearings Mounting surface:Precision machined Finish:Black anodizeModel Travel in NormalLoad lbs Weight lbs Dimensions – inA B C D E F G H J I m p e r i a l4606 6.0154 2.39.003 2.00 1.5082 3.50 1.00346099.0192 3.112.005 2.00 1.00122 5.00 1.003461212.0205 3.915.006 2.00 1.50144 3.25 1.005461515.02434.718.0082.001.001844.001.005for 1/4” S.H.C.S.Dimensions in (mm)Ball BearingSlides4400/M4400 SeriesTravel: 3.0 in76,2 mmSize:Width Length Height 5.00 in5.00 in1.00 in127,0 mm127,0 mm25,4 mmLoad:NormalMoment: Yaw, Pitch, Roll 106 lbsSee page 3148 kgSee page 31Straight line accuracy:0.00008 in/inof travel 2 µm/25 mm of travelWeight: 4410 – 2.2 lbs4450 – 1.7 lbs M4410 – 1,00 kg M4450 – 0,77 kgConstruction:Aluminum top and base/440C stainless steel bearings Mounting surface:Precision machined Finish:Black anodizeTravel ApertureImperial 4410 3.0 in—4450 3.0 in 2.00 inMetric M441076,2 mm—M445076,2 mm50,8 mmQty. (8) Mtg. Holes (Top)Imperial Models – 1/4-20 Thd. on 4.00 Dia. B.C.Metric Models – M6 Thd. on (100,0) Dia. B.C.Metric Models – M6 Thd.Metric Models – M6 S.H.C.S.Metric Models – (13,5)Imperial Models – 4.00Metric Models – (100,0)ApertureDimensions in (mm)B a l l B e a r i n g S l i d es4900/M4900 SeriesSpecifications Imperial Metric Travel: 2.0 in 50,8 mm Size: Width Length Height5.00 in 5.00 in 1.75 in 127,0 mm 127,0 mm 44,5 mm Load:NormalMoment: Yaw, Pitch, Roll77 lbsSee page 3435 kgSee page 34Straight line accuracy:0.00008 in/in of travel 2 µm/25 mm of travel Weight: 3.0 lbs1,4 kgConstruction:Aluminum top and base/ 440C stainless steel bearings Mounting surface:Precision machined Finish:Black anodizeModelTravel Imperial 4900-02 2.0 in MetricM4900-0250,8 mmQty. (6) Mtg. Holes (Top)Imperial Models – 1/4-20 Thd.Metric Models – M6 Thd.Imperial Models – 1/4” S.H.C.S.Metric Models – M6 S.H.C.S.0.50Dimensions in (mm)Ball Bearing SlidesParker Hannifin CorporationElectromechanical & Drives Division28/emn4900/M4900 SeriesTravel: 4.0 – 12.0 in 101,6 – 304,8 mm Size: Width Length Height6.00 in6.00 – 18.00 in 2.00 in 152,4 mm152,4 – 457,2 mm 50,8 mm Load:NormalMoment: Yaw, Pitch, Roll 100 – 294 lbs See page 3445 – 133 kg See page 34Straight line accuracy:0.00008 in/in of travel 2 µm/25 mm of travel Weight: 5.0 – 13.0 lbs2,3 – 6,0 kgConstruction:Aluminum top and base/ 440C stainless steel bearings Mounting surface:Precision machined Finish:Black anodizeModelTravel Normal Load Weight DimensionsA B C D E F G Imperial4900-04 4.0 in 100 lbs 5.0 lbs 6.00 in ——6 5.00 in —44900-066.0 in 154 lbs7.0 lbs 9.00 in 1.50 in —10 5.00 in 1.50 in 84900-088.0 in 205 lbs9.0 lbs 12.00 in 2.50 in —10 5.00 in 3.00 in 84900-1010.0 in 243 lbs 11.0 lbs 15.00 in 2.50 in 2.00 in 14 6.00 in 4.00 in 84900-1212.0 in294 lbs 13.0 lbs 18.00 in 5.00 in 1.00 in 147.00 in 5.00 in 8Metric4900-04101,6 mm 45 kg 2,3 kg 152,4 mm——6125,0 mm—44900-06152,4 mm70 kg 3,0 kg 228,6 mm 37,5 mm —10125,0 mm 37,5 mm 84900-08203,2 mm 93 kg 4,0 kg 304,8 mm 62,5 mm —10125,0 mm 75,0 mm 84900-10254,0 mm 110 kg 5,0 kg 381,0 mm 62,5 mm50,0 mm14150,0 mm 100,0 mm 84900-12304,8 mm133 kg6,0 kg457,2 mm 125,0 mm 25,0 mm14175,0 mm 125,0 mm8Metric Models – M6 S.H.C.S.Imperial Models – 5.00Metric Models – (125,0)Dimensions in (mm)Parker Hannifin CorporationElectromechanical & Drives Division31BallBearingSlidesBall Bearing SlidesParker Hannifin CorporationElectromechanical & Drives Division32/emnParker Hannifin CorporationElectromechanical & Drives Division33BallBearingSlidesBall Bearing SlidesParker Hannifin CorporationElectromechanical & Drives Division34/emnContents124-127Z-Axis Brackets 128-129Micrometer Heads 130-132Optical Mounts123and optical cells are also available.Accessoriesfor Linear and Rotary PositionersAccessoriesParker Hannifin CorporationElectromechanical & Drives Division124/emnZ-Axis BracketsDimensions – in (mm)Thd. N Model A B C D E F G H J JK L M I m p e r i a l3909 1.25 1.25 0.25 1.38 0.250.1560.620.190.380.880.440.88#4-403959 1.25 1.250.25 1.380.250.1560.620.190.040.880.440.88#4-404009 1.75 1.690.25 1.88—0.1560.880.310.63 1.12— 1.12#6-324509 2.44 2.620.38 2.75—0.218 1.220.310.93 2.00— 2.00#10-32M e t r i c M3909(31,8)(31,8)(6,4)(35,1)(6,4)(4,0)(15,7)(5,9)(9,7)(20,0)(10,0)(20,0)M3M3959(31,8)(31,8)(6,4)(35,1)(6,4)(4,0)(15,7)(5,9)(1,0)(20,0)(10,0)(20,0)M3M4009(44,5)(42,9)(6,4)(47,8)—(4,8)(22,4)(7,3)(16,0)(30,0)—(30,0)M4M4509(62,0)(66,5)(9,7)(69,9)—(7,3)(31,0)(8,4)(23,6)(50,0)—(50,0)M6Dimensions – in (mm)Model A B C D E F Imperial3910 1.580.880.190.440.380.313960 2.33MetricM3910(40,1)(20,0)(5,9)(12,3)(7,1)(6,4)M3960(59,2)Dimensions – in (mm)Model A B C Imperial4010 1.120.31 1.12MetricM4010(30,0)(7,1)(30,0)3910, 3960 M3910, M3960Parker Hannifin CorporationElectromechanical & Drives Division125/emnA c c e s s o r i e sDimensions – in (mm)Model A B C D Imperial 4059 1.120.680.380.16MetricM4059(30,0)(16,8)(8,8)(4,8)Dimensions – in (mm)Model A B C D Imperial4059A 1.120.680.620.16MetricM4059A(30,0)(16,8)(15,2)(4,8)Dimensions – in (mm)Model A B C Imperial4510 2.00 2.00 1.00MetricM4510(50,0)(50,0)(25,8)Dimensions – in (mm)Model A B Imperial 4060 1.13 1.13MetricM4060(30,0)(30,0)AccessoriesParker Hannifin Corporation Electromechanical & Drives Division126/emnDimensions – in (mm)Model A B C D E Imperial 4499 4.00 1.62 2.88 2.000.50MetricM4499(100,0)(40,5)(71,4)(50,0)(13,1)Dimensions – in (mm)Model A B Imperial4560 2.00 2.00MetricM4560(50,0)(50,0)Dimensions – in (mm)Model A B C D Imperial 4559 2.000.810.440.22MetricM4559(50,0)(20,9)(11,5)(5,5)Parker Hannifin CorporationElectromechanical & Drives Division127/emnA c c e s s o r i e sDimensions – in (mm)Model A B C D E F GH J I m p e r i a l4990-02 6.00 1.50– 4.002 5.50 1.00 4.00 1.004990-048.12 2.62– 5.002 6.50 1.00 5.00 1.004990-0612.12 5.12 1.5 5.004 6.50 1.00 5.00 1.004990-0817.128.62 3.0 5.004 6.75 1.25 5.00 1.504990-1020.5010.00 4.0 6.004 6.75 1.25 5.00 1.504990-1224.1211.62 5.07.004 6.50 1.00 5.00 1.00M e t r i c M4990-02(152,4)(38,9)–(100,0)2(139,7)(26,2)(100,0)(25,4)M4990-04(206,2)(67,6)–(125,0)2(165,1)(26,4)(125,0)(25,4)M4990-06(307,8)(131,2)(37,5)(125,0)4(165,1)(26,4)(125,0)(25,4)M4990-08(434,8)(220,0)(75,0)(125,0)4(171,5)(32,8)(125,0)(38,1)M4990-10(520,7)(255,2)(100,0)(150,0)4(171,5)(32,8)(125,0)(38,1)M4990-12(612,6)(296,6)(125,0)(175,0)4(171,5)(32,8)(125,0)(38,1)Accessories9510-9530 Series Micrometer HeadsParker Daedal micrometer heads are recommended for any application requiring micrometer accuracy in settings and adjustment. These units feature a hardened and ground spindle, easy-to-read graduations, and an attractive non-glare satin chrome finish.Model NumberFigure Travel in (mm)Graduations in (mm)Dimensions – in (mm)A B C D I m p e r i a l9511EA 0.500.001 2.030.500.187—9512EB 0.500.001 2.630.500.3750.549524E B 1.000.0014,230.750.6250.739526E B 2.000.001 6.16 1.250.6250.739531EC 1.000.0001 5.180.940.56—9532E C 2.000.00017.18 1.440.56—M e t r i c9511M A (13)(0,01)(51,6)(13,0)(4,7)—9512M B (13)(0,01)(66,8)(13,0)(9,5)(13,7)9524M B (25)(0,01)(107,4)(19,0)(15,9)(18,5)9526M B (50)(0,01)(156,5)(32,0)(15,9)(18,5)9531M C (25)(0,002)(131,6)(23,9)(14,2)—9532MC(50)(0,002)(182,4)(36,6)(14,2)—(mid-travel)9531E, 9532E 9531M, 9532MFigure CLarge Thimble MIcrometer Head 9512E, 9524E, 9526E 9512M, 9524M, 9526MFigure BStandard Thimble MIcrometer Head 9511E 9511MFigure AMini Thimble MIcrometer HeadA c c e s s o r i e s9550 Series Digital Micrometer HeadsModel 9551The 9551 precision electronic digital micrometer head provides an LCD readout to 0.00005 inch resolution. The micrometer features:• Incremental and/or absolute positioning modes• Zero set at any position, inch and millimeter readout (0.001 mm resolution), display hold, and automatic shutdown after two hours to conserve the integral battery• 1.00 inch micrometer travel• Battery powered for 500 hours of useModel 9552The 9552 precision electronic digital micrometer offers a 0 – 2 inch travel range with a 0.00005 inch resolution. Features include:• 2 inch spindle• Display face swivels for easy reading at various angles • Non-rotating spindle• Pre-set, zero, and inch/mm • Carbide tipped measuring face•Battery powered for 5,000 hours of use9560 Series Differential ScrewsModel 9560: 0.75 in RangeThe 9560 differential screw offers two linear adjustment ranges in one unit: a coarse adjustment range of 0.31 in (8 mm) with a 48-pitch thread and a fine adjustment range of 0.078 in (2 mm) with a pitch equal to 336 threads per inch. The 9560 is interchangeable with 9511 – 9532 series micrometer heads.9570 Series Fine Adjsutment ScrewsModel 9570: 0.75 in Range Model 9575: 0.50 in RangeThese steel adjustment screws feature a 64-pitch thread, making them ideal for applications where finer resolution is required, but positional readout is not. These screws are easily interchanged with the 9511 – 9532 seriesmicrometer heads.AccessoriesOptical Cell MountsModel 2350: 6.0” DiameterModel 2355: 7.0” DiameterModel 2360: 8.0” DiameterModel 2365: 9.0” DiameterParker Daedal optical mounts are highly stable, adjustablemounts for optics up to 9” in diameter and 1.25” thick.These mounts feature precise kinematic ball pivotadjustment on two axes, with orthogonal three-pointsuspension.Specifications2350235523602365Optic Size Opening – in (mm) Dimension “A” Dia. max.: Thickness:6.03 (153,1)1.00 (25,4)7.06 (179,3)1.25 (31,75)8.06 (204,7)1.25 (31,7)9.06 (230,1)1.25 (31,7)Optic Retention:Threaded retainer 3 mounting clips 3 mounting clips 3 mounting clips Range:5°5°5°5°Resolution:0.5 arc-sec0.5 arc-sec0.5 arc-sec0.5 arc-sec Adjustment: 2 – 64-pitch screws 3 – 32-pitch screws 3 – 32-pitch screws 3 – 32-pitch screws Weight: 7.5 lb (16,5 kg)20 lb (44 kg)20 lb (44 kg)20 lb (44 kg) Construction:Aluminum/stainless steelFinish:Black anodizeA c c e s s o r i e sOptical Cell MountsModel 2370/2371: 10.0” Diameter Model 2375/2376: 11.0” Diameter Model 2380/2381: 12.0” DiameterParker Daedal optical mounts are highly stable, adjustable mounts for optics up to 12” in diameter and 2.0” thick. These mounts feature precise kinematic ball pivot adjustment on two axes, with orthogonal three-point suspension. Solid back models are designed to support reflective optics.AccessoriesMirror Mounts Array Model 5000/5100: 3.0” Square Mounting SurfaceModel 5300/5700: 4.5” Square Mounting SurfaceModel 5800/5900: 6.0” Square Mounting SurfaceParker Daedal mirror mounts are patterned with 1/4-20holes on 0.5” or 1.0” centers to mount mirrors and otherhardware. All models except the 5800 have two fineresolution 64-pitch adjustment screws to provide precisetilting of the mounting surface in two axes. The 5800 isequipped with three adjustment screws to provide precisetilting in two axes.Dimensions – in (mm)Model A B D D E F G 5000 2.00 (50,8) 3.00 (76,2)0.75 (19,1) 2.00 (50,8) 3.75 (95,3) 2.00 (50,8) 3.50 (88,9) 5300 3.00 (76,2) 4.50 (114,3) 1.25 (31,8) 4.00 (101,6) 4.50 (114,3) 2.88 (73,2) 5.12 (130,1) 51000.69 (17,5) 3.00 (76,2) 1.50 (38,1) 2.25 (57,2) 2.00 (50,8) 3.50 (88,9)0.25(6,4) 57000.69 (17,5) 4.50 (114,3) 3.00 (76,2) 3.75 (95,3) 2.88 (73,2) 5.12 (130,1)0.25(6,4) 59000.88(2,4) 6.00 (152,4) 4.00 (101,6) 5.38 (136,7) 3.25 (82,6) 6.25 (158,8)0.31(7,9)E n g i n e e r i n g R e f e r e n c eTravelThe travel listed is the total travel of the positioner from hard stop to hard stop.Bearing Load CapacityNormal LoadThis is the maximumdownward (compression) load or force which can be applied to the positionerof the load must be located in the center ofthe mounting surface. For loads which are offset from thisInverted Loaddirection.Moment LoadThis refers to forces which are offset (cantilevered) from the bearingproducing uneven loading on themeans that some bearings are supporting more of the load than others. For this reason it is very important to determine if the moment loading for a given positioner is within acceptable limits. These moment forces are categorized by the direction they act in Pitch, Roll or Yaw; see diagram at left. When loading results in moments acting in only one of the moment directions (pitch, roll or yaw) it is called a single direction moment. Examples of this type of loading are shown below. How to calculate the maximum allowable moment load is discussed on the following page.Pitch MomentThrust CapacityThrust capacity is or load which can be applied in thecomponents.T a and T b Fine Screw and Differential Screw DrivesWith these types of drives the mounting surface or stage carriage is pressed against the drive mechanism by means of a spring. Because of this the maximum thrust which the stage assembly can maintain is different when pressing toward the spring or away from it. When pressing toward the spring, the force is taken up by the drive mechanism (i.e. micrometer). While pulling away, the force is being held in place by the spring. Stages with this type of mechanism have two thrust capacity specifications (T a and T b ). Tarefers to the load capacity against the micrometer and Tb is the spring load capacity. Refer to specific product drawings for load direction.Screw Drive Thrust CapacityStages which use screw drive assemblies will only have one thrust capacity rating. This rating is for either direction of travel.Straight Line and Flatness AccuracyThis is the amount of error a linear positioner deviates from an ideal straight line. The straight line accuracy is the error in the horizontal plane while flatness is the error in the vertical are measured at the moving carriage surface center.Engineering ReferenceCalculating Maximum Allowable Moment Loads on Linear Slides and StagesTo determine if a load or force is within acceptable moment load ranges follow the steps below:1.Calculate maximum load and or force which will be applied to the positioner. Include brackets and other axes which are mounted to the positioner.2.Locate the center of gravity of the load.3.Determine if there is a single or compound moment.4.Measure the distance from the center of force or C.G.to the center of the linear stage carriage. This is the moment arm length and is designated A s for single direction moments and A c for compound moments.5.Locate the moment load graph for the positioner you are interested in (located in back of individual product section, esee example below). The X axis of the graph is the Force, the Y axis is the allowable moment arm A s for single direction moments.6.Locate the moment curve(s) which your load is acting in (pitch, roll or yaw).7.Locate your load force on the X axis of the graph.8.Draw a vertical line from the Force location on the X axis parallel with the Y axis.9.Find the moment arm distance on the Y axis. Draw a horizontal line from this point parallel with the X axis until the vertical and horizontal lines intersect.10.If the intersection point is below the moment curve in question then the stage is within acceptable limits. If the intersection point is above the moment curve, a positioner with a larger normal load capacity should be selected and the above steps repeated.Yaw & PitchRollForce (N)Moment Arm(mm)4500 / M45004500-DM / M4500-DM050100150200250300350050100150Offer of SaleWARNINGFAILURE OR IMPROPER SELECTION OR IMPROPER USE OF THE PRODUCTS AND/OR SYSTEMS DESCRIBED HEREIN OR RELATED ITEMS CAN CAUSE DEATH,PERSONAL INJURY AND PROPERTY DAMAGE.This document and other information from Parker Hannifin Corporation, its subsidiaries and authorized distributors provide product and/or system options for further investigation by users having technical expertise. It is important that you analyze all aspects of your application and review the information concerning the product or system in the current product catalog. Due to the variety of operating conditions and applications for these products or systems, the user, through its own analysis and testing, is solely responsible for making the final selection of the products and systems and assuring that all performance, safety and warning requirements of the application are met.The products described herein, including without limitation, product features, specifications, designs, availability and pricing, are subject to change by Parker Hannifin Corporation and its subsidiaries at any time without notice.Offer of SaleThe items described in this document are hereby offered for sale by Parker Hannifin Corporation, its subsidiaries or its authorized distributors. This offer and its acceptance are governed by the provisions stated in the “Offer of Sale” found on /emn.©2019 Parker Hannifin Corporation, All Rights Reserved。

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Using fgets to read from the keyboard
Getting numbers from strings
• Once we've got a string with a number in it (either from a file or from the user typing) we can use atoi or atof to convert it to a number • The functions are part of stdlib.h
File handling in C
• In C we use FILE * to represent a pointer to a file. • fopen is used to open a file. It returns the special value NULL to indicate that it couldn't open the file.
FILE *fptr; char readfname[1000]; fgets (readfname,1000,stdin); fptr= fopen (readfname,"w"); /* oopsie - file name also has \n */
Even experienced programmers can make this error
char numberstring[]= "3.14"; int i; double pi; pi= atof (numberstring); i= atoi ("12"); Both of these functions return 0 if they have a problem
Great Muck-Ups in C #11 of 100
Closing a file
• We can close a file simply using fclose and the file pointer. Here's a complete "hello files".
FILE *fptr; char filename[]= "myfile.dat"; fptr= fopen (filename,"w"); if (fptr == NULL) { printf ("Cannot open file to write!\n"); exit(-1); } fprintf (fptr,"Hello World of filing!\n"); fclose (fptr);
C Programming - Lecture 3
• • • • • • File handling in C - opening and closing. Reading from and writing to files. Special file streams stdin, stdout & stderr. How we SHOULD read input from the user. What are STRUCTURES? What is dynamic memory allocation?
Three special streams
• Three special file streams are defined in the stdio.h header • stdin reads input from the keyboard • stdout send output to the screen • stderr prints errors to an error device (usually also the screen) • What might this do:
Writing to a file using fprintf
• fprintf works just like printf and sprintf except that its first argument is a file pointer.
FILE *fptr; fptr= fopen ("file.dat","w"); /* Check it's open */ fprintf (fptr,"Hello World!\n");
Typedef
• Typedef allows us to associate a name with a structure (or other data type). • Put typedef at the start of your program.
typedef struct line { int x1, y1; int x2, y2; } LINE; int main() { LINE line1; }
line1 is now a structure of line type This is what was happening with all that FILE * stuff
Structures in C
• In C, we can create our own data types - FILE is an example of this. • If programmers do a good job of this, the end user doesn't even have to know what is in the data type. • struct is used to describe a new data type. • typedef is used to associate a name with it. • int, double and char are types of variables. With struct you can create your own. It is a new way to extend the C programming language.
FILE *fptr; char line [1000]; /* Open file and check it is open */ while (fgets(line,1000,fptr) != NULL) { printf ("Read line %s\n",line); }
fgets takes 3 arguments, a string, a maximum number of characters to read and a file pointer. It returns NULL if there is an error (such as EOF)
/* define MAXLEN at start using enum */ FILE *fptr; char tline[MAXLEN]; /* A line of text */ fptr= fopen ("sillyfile.txt","r"); /* check it's open */ while (fgets (tline, MAXLEN, fptr) != NULL) { printf ("%s",tline); // Print it } fclose (fptr);
The struct statement
• Here is an example struct statement.
#include <stdio.h> struct line { int x1, y1; /* co-ords of 1 end of line*/ int x2, y2; /* co-ords of other end */ }; main() { struct line line1; . This defines the variable line1 to be . a variable of type line }
The exit() function
• Sometimes error checking means we want an "emergency exit" from a program. We want it to stop dead. • In main we can use "return" to stop. • In functions we can use exit to do this. • Exit is part of the stdlib.h library exit(-1); in a function is exactly the same as return -1; in the main routine
Gre the file pointer to close the file - not the name of the file
FILE *fptr; fptr= fopen ("myfile.dat","r"); /* Read from file */ fclose ("myfile.dat"); /* Ooops - that's wrong */
• fgets includes the '\n' on the end • This can be a problem - for example if in the last example we got input from the user and tried to use it to write a file:
• We could also read numbers from a file using fscanf – but there is a better way.
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