内饰豪华高品质 安全配置尤为丰富 2011款英菲尼迪FX35海外原型车评测

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30-40万suv车型推荐

30-40万suv车型推荐

30-40万suv车型推荐近年来,SUV市场火爆,那30-40万suv哪款车好呢?下面跟着店铺一起来看看30-40万suv车型推荐。

30-40万suv车型推荐推荐车型一:东风英菲尼迪QX50价格区间:34.98-44.98万元作为英菲尼迪国产后的首款SUV车型,东风英菲尼迪QX50凭借着较高的性价比深入人心。

而尺寸加大的它对于消费者来说,还是很受青睐的。

而四年或10万公里的免费保养政策更是它俘获人心的杀手锏。

下面,我们为您介绍豪华紧凑型SUV东风英菲尼迪QX50(以下简称为英菲尼迪QX50)。

外观方面,国产QX50保持进口版本的设计,但细节之处的变化使它更受消费者喜爱。

它采用上下分离式水波纹的中网设计,在保险杠下方,它装配了银色边框装饰和银色下护板,这使得它更加运动。

而两侧的大灯更是将优雅氛围点准的恰到好处。

车身侧面,修长的车头、下压的车尾,带来一些跨界的韵味。

车身尺寸方面,它的长宽高分别为4744mm/1803mm/1614mm,轴距长达2880mm。

车尾部分,横制水滴式的设计脱颖而出,圆润饱满的尾部让它依旧动感。

另外,尾部的东风英菲尼迪标识亮明国产身份。

内饰方面,国产英菲尼迪QX50极富诚意,它原汁原味的保留了进口版本的设计。

该车方向盘采用三幅多功能方向盘,该方向盘握感十足,并显露出一丝运动气息。

仪表盘采用传统机械式仪表盘,黑底白字配合蓝色背光显得十分优雅。

中控台布局合理,虽然按键非常多,但熟悉过后,上手非常容易。

另外,中控台上的钟表凸显科技氛围。

配置方面,英菲尼迪QX50也极富诚意,它拥有智能巡航系统、盲点警示系统、车道偏离预警系统、胎压监测系统、一键式启动、自动大灯、驾驶席员个性记忆系统、前排座椅加热、全景影像、Bose音响、导航系统等配置。

动力方面,英菲尼迪QX50沿用了进口车型上的那台VQ25HR 2.5L V6自然吸气发动机,最大功率235马力,最大扭矩253牛·米。

与发动机匹配的是英菲迪尼7速手自一体变速器。

黑翼飞行模拟器用户手册说明书

黑翼飞行模拟器用户手册说明书

IntroductionThe Blackwing BW 635RG is an ultralight two-seater aeroplane designed for recreational flying and training purposes. It features a sleek and modern design, with a composite airframe and a low-wing configuration. The Blackwing has a cruising speed of up to 120 knots and a range of approximately 700 nautical miles, making it suitable for both short and long-distance flights. The cockpit is equipped with state-of-the-art avionics, including a glass cockpit display and an autopilot system. The Blackwing is also known for its superior handling and stability, making it a popular choice among flying enthusiasts and flight schools. The BW 635RG is powered by the venerable Rotax 915 iS engine.Development Credits:Mal Cartwright Product LeadRuss White3D Modelling, Interior and Exterior TexturingJack Lavigne IntegrationHarry Stringer AnimationPropAir Flight Model and SystemsJordan Gough ManualWith special thanks to our Beta Testers:Rob Abernathy John BurgessNick Cooper John DowMatt McGee Darryl WightmanTable of ContentsIntroduction (2)Development Credits: (2)With special thanks to our Beta Testers: (2)Table of Contents (3)Notes on Hardware (4)Overview (5)Aircraft Limitations (6)Airspeed Limitations (6)Engine Limitations (6)Operating Conditions (6)Fuel (7)Other Limitations (7)Emergency Procedures (8)Engine Failure on the Take-off Roll (8)Engine Failure after Take-off (8)Glide Performance (8)Emergency Landing (9)Spin Recovery (9)Normal Procedures (10)Before Starting Engine (10)Starting Engine (10)Before Taxiing (11)Taxiing (11)Engine Runup (11)Before Take-off (11)Take-Off (12)Initial Climb (12)Cruise Climb (12)Cruise (12)Landing (13)Balked Landing (13)After Landing (13)Securing Aircraft (14)Basic Performance (15)Stall Speeds (15)Take-Off Performance (15)Landing Performance (16)Systems Description (17)Instrument Panel Layout (17)Switch Logic and Electrical System (18)Master Switch (18)Fuel Pump Switch (19)LAND/TAXI Switch (19)Strobe/Nav Switch (19)Electrical System Diagram (20)Engine (21)Propeller (21)Fuel (21)Notes on HardwareDue to the unusual 3-position switches in this aircraft, conventional hardware 2position toggle switches (eg. strobe or nav light switches) cannot be translated tothe single 3-position switch which combine these.Additionally, as this aircraft utilises a single level power control (throttle), conventional throttle/prop/mixture hardware may interfere with the function of this system, and not work as intended. It is recommended to place your propeller and mixture levers in the IDLE position, and not move them while the engine is running.OverviewThe Orbx BW 635RG has been developed using official documentation and Computer Aided Design (CAD) resources from Blackwing Sweden. As a result, the aeroplane has been created through masterful modelling, texturing, systems integration, and flight model development.Figure 1 – Aircraft 3-viewAircraft DimensionsLength 6.6m Height 2.2m Wingspan8.4mWeightsBasic Empty Weight 375kg Maximum Take-off Weight 600kg Maximum Fuel Capacity (Litres)130LThe content in this manual and the operation of the BW 635RG in Microsoft Flight Simulator strictly must not be used as reference material in any form for operating the real aircraft.Aircraft LimitationsAirspeed LimitationsAirspeed Description Airspeed (KIAS) RemarksVne Never Exceed Speed 157 Must not exceed this speed in any operation.Va Manoeuvring Speed 109 If full or abrupt control deflection is made, the airframe may be overstressed.Vfe1 Max flap extended speed20 degrees90 Maximum speed for flaps 20°Vfe2 Max flap extended speed35-45 degrees 70 Maximum speed for flaps 35-45°Vlo Maximum landing gearoperating speed 70Do not extended or retract the landing gearabove this speed.Vle Maximum landing gear extended speed 90 Do not exceed this speed with the landing gearalready down.Vs0 Stall speed flaps/gearextended 38 Stall speed with gear down/flaps >0° and in level flight at MTOWVs1 Stall speed clean 49 Stall speed flaps retracted, gear up and in level flight at MTOWEngine LimitationsEngineEngine Manufacturer Rotax Engine Model Rotax 915 iSMaximum Power Take-off (Max 5 min.) 141 hp Continuous 135 hpMaximum RPM Take-off (Max 5 min.) 5800 Continuous 5500Critical Altitude 15000ft AMSL Maximum OperatingAltitude23000ft AMSL Operating ConditionsAerobatic manoeuvres, flight in IFR conditionsand flights in icing conditions are prohibited inthis aircraft.FuelFuel TanksLeft Right Litres US Gal Litres US GalTotal Fuel in Tank 67.5 17.8 62.5 16.5Unusable Fuel 2.5 0.7 2.5 0.7 Total Useable Fuel in Tanks 66.5 17.6 61.5 16.2Other LimitationsMaximum demonstrated crosswind for the BW 635RG is 20 knots.Emergency ProceduresNote: The following procedures have been modified to be suitable for simulation. It does not cover emergencies that are a) not simulated and b) not reasonable. Checklist items from the real procedures have been omitted and these procedures must not under any circumstances be used for training purposes.Engine Failure on the Take-off RollThrottle: IDLEIgnition: OFFFuel Pump: MAIN (DOWN POS)Brakes: APPLYWhen stopped: SECURE AIRCRAFTEngine Failure after Take-offNose: IMMEDIATELY LOWERAirspeed: 65 KNOTSLanding Area: DETERMINE WITHIN 30° OF NOSEFlaps: USE AS REQUIREDLanding Gear: USE DESCRETIONFuel Selector: OFFIgnition: OFFMaster Switch: OFFGlide PerformanceThe BW 635RG, the approximate performance for a glide is 65 KIAS which willgive approximately a 545ft/min rate of descent in the clean configuration.Glide performance will degrade significantly on extension of flaps and landinggear.Emergency LandingAirspeed: 65 KIASField: PICK BEST OPTIONLanding Gear: USE DISCRETION DEPENDING ON FIELD TYPEFlaps: AS REQUIREDFuel Selector: OFFIgnition: OFFFuel Pump: MAIN (down)Master Switch: OFF BEFORE LANDINGSpin RecoveryThrottle: IDLEControl Stick: AILERON NEUTRALRudder: FULL OPPOSITE TO DIRECTION OF ROTATIONControl Stick: POSITIVELY FORWARD OF NEUTRALRudder: NEUTRAL WHEN ROTATION STOPSControl Stick: SMOOTHLY PULL OUT OF DIVEWARNING:INTENTIONAL SPINS ARE NOT APPROVED INTHIS AIRCRAFT.Normal ProceduresNote: The pre-flight inspection portion of the normal procedures has been removed due to impracticality in the simulator.Before Starting EngineIgnition: OFFMaster Switch: OFF (down)Backup Battery: OFF/AUTO (down)Landing Gear Lever: DOWNCircuit Breakers: INCanopy CLOSED (CLICKING THE LATCHON THE INSIDE LEFT SIDEWALL.) Starting EngineParking Brake: HOLD TOE BRAKES AND ENGAGE PARKINGBRAKEMaster Switch: ENGINE START (middle position)Fuel Selector: SETFuel Gauge: CHECKFuel Pump: BOTH (up)Ignition: BOTHNav Lights: STROBE (middle position)Throttle: SET ½-1 INCH OPENIgnition: STARTOil Pressure: GREEN WITHIN 10 SECWarnings: NONEBefore TaxiingMaster Switch: NORMAL OPERATION (up)Altimeter: SETAvionics: SETParking Brake: DISENGAGETaxiingInstruments: CHECKED (COMPASS/HSI/BALL/ATT) Engine RunupParking Brake: ENGAGERPM: 2500 RPMFuel Pump: CYCLE, CHECK FUEL PRESSUREIdle: CHECK IDLE 1800 +/- 100 RPM Before Take-offCanopy: CLOSED AND LOCKEDFlaps: 1 STAGE (20°)Elevator Trim: SET FOR TAKE-OFFEngine Instruments: NORMALLanding Light: ON (up)Controls: FULL FREE AND CORRECT MOVEMENTParking Brake: DISENGAGETake-OffThrottle: FULLControls: NEUTRAL45 Knots: ROTATEAccelerate: NOSE ON HORIZON, ACCEL TO 80 KIASPositive Rate of Climb: GEAR UPLanding Light: OFF (down)Flaps: RETRACT ABOVE 500’ AGLInitial ClimbThrottle: MAX CONTINUOUS (5500 RPM)Airspeed: 90 KIASFuel Pump: MAIN (down) ABOVE 500’ AGL Cruise ClimbThrottle: MAX CONTINUOUS (5500 RPM)Airspeed: 130 KIASCruiseThrottle: 55-75% PowerAirspeed: 120-157 KIAS (<130 KIAS IN TURB)LandingFuel: QTY CHECKEDFuel Selector: FULLEST TANKFuel Pump: BOTH (up position)Airspeed: 90 KIASFlaps: EXTEND FLAP 1 <90 KIASDownwind Airspeed: 65 KIASLanding Gear: DOWN @ 65 KIAS; CHECK 3 GREENLanding Light: ON (up position)Base Leg: EXTEND FLAP 2 < 65 KIASFinal Approach Airspeed: 60 KIASBalked LandingThrottle: SMOOTHLY INCREASEAirspeed: 60 KIASTrim: COURSE TRIM TO RELIEVE PRESSUREFlaps: RETRACT TO POSITION 1 (20°)Gear: UPTrim: TRIM FOR CLIMBAfter LandingFlaps: RETRACTExterior Lights: AS REQ’DFuel Pump: MAIN (down)Securing AircraftParking Brake: ENGAGEDThrottle: IDLESwitches: ALL OFF EXCEPT ACL AND MASTERIgnition: OFFNav Lights: OFF (down)Master Switch: OFFBasic PerformanceStall SpeedsMTOW 600kg | CG 32% MAC | Power Idle | Level FlightFlap Position Stall Speed (KIAS) 0° 49 20° 44 35° 39 45°38Take-Off PerformanceMTOW | ISA CONDITIONS | SEA LEVEL | FLAPS 1 (20°) | MTOW (600kg)Cruise PerformanceRunway Surface Ground RollOver 50ft Obstacleft mft mPaved Runway328 100 656 200 Unpaved (Grass) Runway 361110689208Pressure Altitude Power (%) TAS Fuel Flow LPH MAP (inHg) Endurance(hr)Range (nm) 500055 161 19.7 30 5.8 941 65 170 23.3 34.1 4.9 827 7517826.937.44.1738Landing PerformanceMTOW | ISA CONDITIONS | FLAPS 2 (35°) | MTOW (600kg) | Speed 1.3 x VsoRunway Surface Ground Roll Over 50ft Obstacle ft m ft mPaved Runway 525 160 951 290 Unpaved (Grass) Runway 558 170 984 300Systems Description Instrument Panel LayoutSwitch Logic and Electrical SystemThe electrical switches in the BW 635RG are 3-position switches. These are generally known as “DOWN”, “MIDDLE” and “UP”. They are briefly explained below.Master SwitchThe MASTER switch functions in a unique way, with the following switch logic:1.When the MASTER switch is DOWN, all battery power is off. There will beno electrical power provided to the aircraft.•Note: The engine CANNOT be shut down when the master switch isoff. Electrical power must be present for the engine to turn off.2.When the MASTER switch is in the MIDDLE (Engine Start) position, limitedsystem functionality will be present. The backup battery will be activatedand power the following systems:•Primary Flight Display•Compass•AHRS (Attitude Heading Reference System)•Radio3.When the MASTER switch is UP (Normal Operation), full electrical supplywill be provided to the aircraft. The following systems will be powered on: •Note: the engine CANNOT be started with the MASTER switch in theUP position. If the engine won’t start, check the switch is in theMIDDLE position•Multi-Function Display•Transponder•Autopilot•Audio panel•STBY instruments•Pitot Heat•Main battery is disconnected from running engine. Alternatorprovides power.See Section NORMAL PROCEDURES for positioning of the MASTER switch.Fuel Pump SwitchThe Fuel Pump switch also has some advanced logic to it, due to two fuel pumpsbeing present, however, to put it simply, it operates in the following way:1.In the DOWN position, the main fuel pump is in use.2.In the MIDDLE position, the auxiliary fuel pump is in use.3.In the UP position, both fuel pumps will be on.LAND/TAXI SwitchThe LAND/TAXI switch powers the Taxi and Landing lights. It operates in the following logic:1.In the DOWN position, both lights will be OFF.2.In the MIDDLE position, the taxi light will switch on when the landinggear is extended.3.In the UP position, the Landing Light will switch on when the landinggear is extended.Strobe/Nav SwitchThe Strobe/Nav switch powers the Navigation (Red/Green) and Strobe (flashingwhite) lights. It operates in the following logic:1.In the DOWN position, both lights will be OFF.2.In the MIDDLE position, the STROBE light will be on.3.In the UP position, both the strobe and Nav lights will be on.Electrical System DiagramThe BW 635RG’s electrical system is modelled in the following way in Microsoft Flight Simulator.Because the starter system is connected to the BACKUP BUS, this means you cannot start the engine with the MASTER switch in the UP position, due to the BACKUP BUS being disconnected from the circuit once the MAIN BAT BUS is powered.Page 21 of 21User Guide v1.0 –RevisionEngineThe BW 635RG is powered by the Rotax 915iS. The Rotax 915iS is a four-stroke, four-cylinder, fuel-injected, turbocharged aircraft engine with a maximum power output of141 horsepower. The engine utilizes electronic fuel injection (EFI) technology toprovide precise fuel delivery and improved fuel efficiency. It also features a modernliquid-cooling system and a dual electronic ignition system for reliable performance.The Rotax 915iS engine has a maximum operating RPM of 5,200, with a recommended continuous operation range of 5,000 RPM or less.PropellerThe propeller is a 3-blade wood-composite design, which is hydraulically adjustable for operation at various pitch angles, controlled independently of the pilot. The propeller is linked to the engine through an electronically controlled governor, where RPM isadjusted in accordance with the position of the throttle control. This pitch curve cannot be adjusted in flight, however is designed to ensure maximum performance in allphases of flight.FuelBoth wings have fuel tanks, which are fed to the engine via electric fuel pumps. Fuelsystem information is fed via sensors to the Garmin avionics suite and can be viewedon the displays inside the cockpit.AIRPLANE WEIGHTSBasic Empty Weight……………………….…375 KgMaximum Takeoff Weight…………………..600 KgMaximum Fuel Weight………………………...95 Kg Maximum Landing Weight………………….600 Kg TANK USABLE FUEL LEFT WING TANK67.5 litres 17.8 US Gallons RIGHT WING TANK62.5 litres 16.5 US Gallons TOTAL 130 litres34.3 US GallonsFUEL CAPACITY AIRSPEEDS Never Exceed Speed ……….…………….173 KIAS Max Structural Cruising Speed…………..156 KIAS Maneuvering Speed MTOW……………….109 KIAS Initial Climb………………………………………80 KIASBest Angle Climb……………………………….75 KIASBest Rate of Climb……………………………..90 KIASMax Flap Ext 20°……………………..............90 KIASMax Flap Ext 35-45°……………………………70 KIASMax Landing Gear Operation……………….70 KIASMax Landing Gear Extended………………..90 KIASPlanned Cruise TAS………………………….130 KIASFinal Approach Speed………………………..60 KIAS POWERPLANT LIMITATIONSENGINE LIMITS (RPM)Take-off (5 Minutes)………....5800 RPM Max Continuous……………….5500 RPMALTITUDE LIMITSMaximum Operating Altitude………………23 000ftFor Microsoft Flight Simulator Use Only0-12023 Orbx Simulation Systems Pty. Ltd BW 635RG QUICK REFERENCESHEETIssued: 21 Apr 2023Revised: 21 Apr 20230-2PROCEDURESBEFORE STARTING ENGINEPreflight Inspection………………………….COMPLETECrew Briefing………………………………….COMPLETEIgnition…………………………………………………….OFFMaster Switch…………………………………………..OFFBackup Battery …..…………………………….OFF/AUTOLanding Gear Lever………………………………..DOWNCircuit Breakers…………………………………………..IN Canopy………………………………………………CLOSED STARTING ENGINEArea……………………………………………………..CLEARParking Brake……………….HOLD TOE BRAKES ANDENGAGEMaster Switch …..……………….ENGINE START (MID)Fuel Selector…………………………………………….SETFuel Pump………………………………………BOTH (UP)Ignition………………………………………………….BOTHExternal Lights……………………………………..AS REQThrottle ………………………..………..Τ12-1 INCH OPENIgnition………………………………………………….START AFTER START Oil Pressure.…………………………………………RISING Master Switch ……………………………..NORMAL (UP)Radios………………………………………………………SET Altimeter…………………………………………………..SET ATIS and Clearance…………………………..OBTAINEDBEFORE TAXIBrakes/Park Brake ………………………….DISENGAGEFlight Instruments……………………………..CHECKEDCompass…………………………………………CHECKED BEFORE TAKEOFFCanopy/Harnesses………………………………SECURE Flaps…………………………………….……1 STAGE (20°)Trim ..……………………………………SET FOR TAKEOFF Flight Instruments………………………………………SET Engine Instruments………………CHECKED NORMAL Avionics…………………………………………………….SET External Lights………………………………………AS REQ Flight Controls…………..FULL, FREE AND CORRECT Takeoff Safety Brief………………………….DELIVERED TAKEOFFBrakes/Park Brake………………………….DISENGAGEPower…………SMOOTHLY INCREASE TO MAXIMUM45 knots………………………………………………ROTATEAccelerate……….…NOSE ON HORIZON, TO 80 KTSPositive Rate of Climb………………………….GEAR UPLanding Light.……………………………….OFF (DOWN)Flaps ………………………..RETRACT ABOVE 500’ AGLMEMORY ITEMS 2023 Orbx Simulation Systems Pty. Ltd ENGINE RUN UP Parking Brake ……………………………………..ENGAGE Engine Instruments……………………………CHECKED Engine RPM…………………………………SET 2500 RPM Fuel Pump…………………………………………….CYCLE Idle …………………..…..CHECK IDLE 1800 ±100RPM Navigation Equipment …..…………………………….SETFor Microsoft Flight Simulator Use OnlyIssued: 21 Apr 2023Revised: 21 Apr 2023AFTER TAKEOFF Engine Instruments……………………..WITHIN LIMITS Climb Speed…………………………………………90 KIAS Fuel Pump………….MAIN (DOWN ) ABOVE 500’ AGL0-3CRUISEPower….……………………………………….SET 55-75%Airspeed…..……….120-157KTS (<130KTS IN TURB.)DESCENTAltimeter…………………………………………………..SETFuel Selector………………………………FULLEST TANKPower Lever………………….AS REQUIRED FOR RODApproach Brief………………………………PLETE BEFORE LANDINGBrakes……………………………………………………..OFFFuel ………….………………………………QTY CHECKEDFuel Selector………………………………FULLEST TANK Fuel Pump……….………………………………BOTH (UP)LANDINGDOWNWINDAirspeed….………………………………………….90 KIASFlaps….………………………………………STAGE 1 (20°)Airspeed………….………………………………….65 KIASLanding Gear…..…………………….DOWN @ 65 KIASCHECK 3 GREENLanding Light………………………………………ON (UP)BASEFlaps…………………………… STAGE 2 (35°) < 65 KIASFINALAirspeed………….………………………………….60 KIASTouchdown ……………………….MAIN WHEELS FIRSTStick………………………………………………FULL BACK Brakes…………………………………………………..APPLYAFTER LANDING Flaps………………………………………………..RETRACT Landing Lights…………………………………………..OFFFuel Pump….………………………………MAIN (DOWN)SHUTDOWNParking Brake ……………………………………..ENGAGE Throttle……………………………………………………IDLE Switches….………………………….OFF EXCL. MASTERIgnition..…………………………………………………..OFFLights….……………………………………….OFF (DOWN)Master Switch..……………………………..OFF (DOWN)MEMORY ITEMS 2023 Orbx Simulation Systems Pty. Ltd For Microsoft Flight Simulator Use OnlyPROCEDURESIssued: 21 Apr 2023Revised: 21 Apr 2023。

X3(F25)完整

X3(F25)完整

全新BMW X3 产品培训 03/2011 第 13 页
模块3 -多功能与便利性。 尺寸数据。
尺寸数据。
全新BMW X3
323
830
861
2810 4648
320
977
1675
全新BMW X3 产品培训 03/2011 第 14 页
模块3 -多功能与便利性。 尺寸数据。
尺寸数据。
BMW X3(F25)对比BMW X3(E83)
BMW 培训
产品培训。
Sheer Driving Pleasure
全新BMW X3。
您值得信赖的全能伙伴。
全新BMW X3 产品培训 03/2011 第2页
全新BMW X3。 培训内容。
模块 1。 全新BMW X3设计。
模块 2。 BMW高效动力。
模块 3。 多功能与便利性。
模块 4。 舒适驾乘与动感操控。
开口:1100 mm
开口:950 mm
G
G
行李箱内部高度:774毫米 行李箱内部宽度:960毫米 行李箱内部高度:789毫米 行李箱内部宽度:1079毫米
行李箱内部高度:810毫米 行李箱内部宽度:1117毫米
全新BMW X3 产品培训 03/2011 第 21 页
模块3 -多功能与便利性。 灵活的空间。
F25 F25 E83 E83
+/-x +/-x +/-x
F25 F25 具有优势 besser
同等水平 Neutral
1674 V211 550 L** 480 L***
F25 F25 不具优势 schlechter
+3
+5
+22

英菲尼迪.新M系_试车报告篇

英菲尼迪.新M系_试车报告篇

操控高手海外试驾2011款英菲尼迪M系列2009年12月08日 01:00 来源:汽车之家类型:编译编辑:胡正暘[汽车之家编译] 紧随雷克萨斯新GS和奔驰第八代E级的上市,英菲尼迪已经为旗下2011款M 系列——也是第三代M产品——的发布做好了准备,据称这款轿车将能与前面两位对手媲美,至少也是势均力敌。

和GS一样,新M系列有V6、V8以及V6混合动力版三种动力系统可选择,很精准的对应了奔驰的V6、V8和即将到来的BlueTEC柴油发动机。

新M系列比老款更长更宽,外观更时尚,娇柔线条的钣金配合更大的车轮,整体感觉就像一辆大一号的G级。

在发动机盖下面,M37配备的是一台327马力3.7升V6发动机,峰值扭矩364牛米,而M56搭载的是420马力5.6升V8发动机,峰值扭矩542牛米,当然你也可以选择混合动力版本,它安装了锂离子电池组以及一台3.5升V6发动机。

英菲尼迪表示混合动力版本将在2011年以2012款的名义发布,它将是公司历史上最清洁最省油的产品。

M37和M56都将标配七速自动变速箱,用户还可以选装运动套件,包括四驱系统、20英寸轮毂、双活塞减震、四轮主动转向、四活塞制动卡钳、换挡拨片,以及运动风格的座椅、方向盘、排挡杆。

在高档车之间的竞争中,科学技术是关键,新的M系列不会让你失望。

驾驶模式包含标准、经济、运动、雪地四种选择,全球首创的盲点干预系统能在车辆偏离行驶车道时对转向系统进行干预,将车辆以稳定的姿态拉回车道,有效防止了因为偏离车道而引起的意外情况,另外这套系统还能实现车辆安全间距控制以及高速巡航的智能化。

车内的乘客还能享受到湿度调节功能,而补风系统能最大程度模拟自然风的感觉,空气过滤系统还能自动检测室内空气的灰尘量以及监控空气新鲜程度。

我们最近拿到了M37四驱版和M56 S版的样车,发现上一代的V6机敏迅速,而现款V8的动力似乎下降了,而且少了一些个性。

英菲尼迪表示他们仍然在继续开发燃油直喷系统,并且坚信M56在2010年春天上市时,它的发动机能在隆隆声响下输出至少420马力功率,考虑到2010款M45的4.5升V8发动机“只有”325马力功率,那么2011款95马力的飞跃确实会是非常惊人的表现,我们试目以待。

英菲尼迪汽车-QX60上市产品介绍培训课件_67P

英菲尼迪汽车-QX60上市产品介绍培训课件_67P

东风英菲尼迪经销商网络发展部英菲尼迪QX60产品介绍•QX60产品定位•QX60产品亮点•QX60产品定位•QX60产品亮点QX60目标客户QX60产品定位•追求事业生活完美平衡的现代商业精英人群属性心态&需求人群洞察目标受众•35-45岁,成熟自信的精英人士•已婚有子女,事业成功,家庭美满•拥有自己的事业,并逐渐意识到家庭的重要性•有意识的寻求事业与家庭的平衡•渴望实现家庭与事业完美平衡的全面掌控力目录•QX60产品定位•QX60产品亮点•优雅动感的豪华设计•超大空间豪华享受•性能与燃油经济性完美平衡•全方位安全防护•优雅动感的豪华设计•超大空间豪华享受•性能与燃油经济性完美平衡•全方位安全防护车身尺寸•QX60是一款大型豪华7座SUV,宽大的车身尺寸使外观更有气势也保证了车内宽敞的空间。

高:1,750mm•双拱形镀铬进气格栅•水波纹进气中网•自动感应氙气大灯和LED日间行车灯•配备大灯自动水平调节、延时关闭、大灯清洗功能•弯月形D柱设计•车侧最显著的INFINITI标识后排私密玻璃,保护重要乘客或家人的隐私波浪形雕塑感腰线,整车光影效果突出标配20寸轮毂,视觉效果动感,提供良好的操控性能车底部空气流动优化车顶部的空气流动优化后轮导流板前扰流板后尾翼•车尾部分通过后尾翼、后侧扰流板及后尾灯组的设计减小后真空区,降低风阻系数•车底、前保险杠和侧面的设计也都是有利于气流快速通过,保证高速行驶稳定性侧后扰流板后灯组扰流设计后真空区空气动力学设计内饰设计•温馨惬意的整体氛围•精致的用料和做工•众多实用的功能配置高级枫木实木饰板高级真皮座椅、内饰QX60产品亮点•优雅动感的豪华设计•超大空间豪华享受•性能与燃油经济性完美平衡•全方位安全防护第二、三排平地板设计,中级无凸起,保证了第三排宽敞的腿部空间第二排座椅前后可调140mm ,同级最大,内部空间布局更加灵活•作为一款大型7座豪华SUV ,优雅大气的造型是一方面,车内宽敞的使用空间也是一个受人关注的重要因素,QX60的车内空间非常充裕,可以说达到了MPV 车的实用性。

手打牛肉丸营销策划案

手打牛肉丸营销策划案

手打牛肉丸营销策划案前言潮汕手打牛肉丸美誉盛传,名声在外。

但是,美味弹牙的手打牛肉丸却总是犹抱琵琶半遮面般羞涩,市场上很少见到其庐山真面目,很多人都只是听说而已,真正尝到的少之又少。

通过调查我们发现,手打牛肉丸包装进入超市,具有很大的市场前景,能够充分满足有需求欲望的这类人群对于产品优质性、便捷性等的需要。

目前手打牛肉丸竞争者较少,这是一个很大的市场空缺,有机会进入。

通用磨坊在广州设厂,旗下品牌知名度高,如湾仔码头等,但其产品线较少,需要扩展。

“潮”工作室自创“好品道”手打牛肉丸这一品牌,为上头公司通用磨坊做营销策划。

本策划案通过市场调查,选择了中国东部一、二级城市目标市场,目标人群锁定在中高端收入的年轻白领和家庭主妇。

并分别根据目标人群赋予产品丰富立体的形象:永不言败、努力拼搏的坚强品格和多姿多彩、营养健康的品位生活,从而唤起目标人群对于产品更深厚的感情并实现购买。

产品设计多种规格、多种口味的牛肉丸产品,满足不同消费者的不同需求,并通过通用磨坊已有的销售渠道,打开市场,创新更丰富的渠道管理策略,进而实现稳定销售。

由于在竞争上处于相对优势,以及目标人群有足够的消费能力,采取快速撇脂和认知价值定价法定价,价格相对高端,能够实现企业优厚利润。

在促销方式上,活动丰富,并向消费者推广牛肉丸更多的烹饪和食用方法,进一步实现顾客满意。

通过本次策划,我们的目标是希望消费者能够随心所欲吃到优质美味有弹性的手打牛肉丸,打响“好品道”这个品牌,继承、推广和创新潮汕美食文化,并实现企业利润最大化。

目录1.公司介绍 (6)2.宏观环境分析 (7)2.1人口环境分析 (7)2.2经济环境分析 (7)2.3政治法律环境分析 (7)2.4社会文化环境分析 (7)2.5技术环境分析 (8)2.6自然环境分析 (8)3.中观环境分析 (8)3.1潜在进入者的威胁 (8)3.2现有竞争对手间竞争的激烈程度 (9)3.3替代品威胁 (9)3.4买方讨价还价能力 (9)4.微观环境分析 (10)4.1企业内部环境 (10)4.2供应商 (11)4.3中间商 (12)4.4顾客 (13)4.5竞争者 (14)4.6社会公众 (15)5.SWOT分析 (16)5.1“好品道”产品的优势: (16)5.2“好品道”产品的劣势: (17)5.3“好品道”产品的机会: (17)5.4“好品道”产品的威胁: (18)6.目标市场定位 (18)6.1市场细分 (18)6.2选择目标市场 (22)6.3市场定位 (29)7.产品策略 (31)7.1品牌名------好品道 (31)7.2品牌建立介绍 (31)7.3品牌生命周期分析与应对方案 (32)7.5品牌产品特点介绍 (35)7.6品牌产品组合介绍 (36)7.7品牌产品产品包装 (37)7.8手打牛肉丸生产工艺和过程 (38)8.手打牛肉丸定价策略 (41)8.1定价目标 (41)8.2成本估算 (42)8.3分析影响产品定价因素 (44)8.4新产品定价策略 (48)9.渠道设计与选取 (50)9.1目标渠道: (50)9.2营销渠道战略 (50)9.3好品道手打牛肉丸营销渠道选择策略 (52)9.4营销渠道管理 (54)10.促销策略 (57)10.1促销的目的 (57)10.2促销结构图 (57)10.3促销策略选择 (57)10.4策略分析 (58)10.5广告预算 (66)附1:调查问卷 (67)附2:感想 ...................................................................... 错误!未定义书签。

国内首台2011款进口X5 xDrive35i 3.0T(N55B30A)升级ECU

国内首台2011款进口X5 xDrive35i 3.0T(N55B30A)升级ECU

国内首台2011款进口X5 xDrive35i 3.0T(N55B30A)升级ECU 初见新BMW X5,一下子看不出有太大的变化,但仔细端详,又有许多更新之处;造型重新设计的头灯组,比起旧款的要圆润修长,远近灯皆以鱼眼投射方式设计,眼神锐利,而加大的臀型水箱护罩以及进气霸,线条看似复杂,却让新款的车头整体气度依旧狂霸不已。

新X5的“Xdrive”中文称之为智能全轮驱动系统,即适时四驱系统,和传统越野车传动系统相比最大的区别是,它的分动箱没有高低挡。

因为它是由电机控制一组离合器来调节前后扭力分配的中央差速器,不是传统意义上的液力耦合中央差速器LSD(限滑差速器)。

新宝马X5 xDrive35i的仪表样式还是比较传统,显示清晰,信息量大。

内饰乍一眼看,只有方向盘的造型有些改变。

方向盘多功能区域造型向上挑起,给人以出色的美感。

其余部分,在功能使用上相同。

新宝马X5 xDrive35i的内饰和之前没有过多变化,还是那么漂亮,高级,选材考究,工艺精湛,内饰基调保持经典,功能用起来得心应手。

新宝马X5 xDrive35i车尾保杆的设计却趋於保守,红色夜视反光灯位置发生了变化,并取消了不同色的保险杠。

倒车雷达的位置也降低了一些,使驾驶变得更安全。

排气管造型由原来的方形变为圆形,诸多的细节变化让新X5变得活泼了一些,双出排气管,则是在内敛气息中透出满满的性能昭示。

从下面的厂家铭牌上可以看出,新X5 xDrive35i的全新引擎,3.0L单涡轮双涡流发动机,最大功率225Kw,最大扭矩400Nm。

发动机也和老款不同,换成N55系列的N55B30A 发动。

动力系统是新X5 xDrive35i的最大升级,其中3.0L发动机是最大亮点,不同于N54系列的双涡轮增压,N55系列直列6缸涡轮增压发动机只有一个涡轮,但通过双涡管技术,同样达到了老款N54双涡轮增压发动机的效能,重量减轻但性能不减,着实令人兴奋。

0-100公里加速时间仅为6.8秒。

捷豹XJL_试车报告篇

捷豹XJL_试车报告篇

传承、颠覆、创新法国试驾全新捷豹XJ 2010年03月10日 04:11 爱卡汽车网张漪然前言:时间:2009年7月9日,地点:英国伦敦的萨奇画廊Saatchi Gallery,事件:全新捷豹XJ 旗舰车型正式发布。

伴随着新款XF和XK的大获成功,全新的XJ似乎承载着更多使命,尤其是对于中国市场而言,中国的富豪们似乎并不对老款XJ感兴趣,貌似只有ABB才是他们心中豪车的代表,全新一代捷豹XJ的出现正是要打破这种固有格局。

此次赴法国试驾,巴黎的卫星城—凡尔赛成为我们短期落脚之处,入住的酒店就位于著名的凡尔赛宫对面,作为曾经见证法国革命等重大历史时刻的凡尔赛宫,终结了法兰西宫廷的历史。

而作为这篇文章的主角,全新捷豹XJ能不能撼动德国列强们的统治地位呢?我们拭目以待。

我们先从客观的账面数据入手,先期进口到中国的XJ均为加长125mm的XJL,车身长度为5247mm,含后视镜的宽度为2110mm,高1448mm,轴距达到了3157mm,在硬件条件上丝毫不输给德国对手,而全新的设计风格,才是捷豹XJ有可能突出重围的重点。

需要特别说明的是,加长版与标准版是同时研发,并不是为了某些特定区域而后期“拉皮”。

老实讲,老款XJ虽然在国内销量甚微,但浓郁的英式风格给我的印象异常深刻,四只圆形头灯以及货真价实的雪茄式车身,完完全全的继承了1968年第一代XJ6的英式精髓。

而摆在面前的全新XJ 则更多的沿袭自XF和XK,捷豹的新面貌似乎更能符合如今的审美观念,但这绝不等同于毫无特色的与其他品牌“同流合污”,对于这种拥有长远历史的品牌来讲,如何保持以往的风格是至关重要的。

我们注意到,前几代XJ将4只圆形头灯这一经典元素保持的时间非常久,而新款XJ的头灯似乎摒弃了这一风格,当我们将这个问题抛给XJ的设计总监时,他微笑着示意我们仔细观察,他说:我们依旧保留了四只头灯,只不过在新一代XJ上你们需要仔细观察。

新的头灯融合了时下流行的LED元素,在内部用数颗LED组成了日间行车灯,这也算做捷豹迎合潮流的手法之一。

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