2014款Huracan LP 610

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兰博基尼

兰博基尼

Miura
1966年3月日内瓦车展,达拉瑞和甘迪尼的大作P400 Miura登台,Miura 通常被翻译为“缪拉”或“穆拉”。Miura的车身分为三段,车身前罩、 座舱、后发动机罩,前后两部分可以掀开,内部机械完全暴露于外。整 体看来,Miura车型具有强烈的攻击型,在现在看来依然不觉过时Miura 在造型上和90年代流行过的美国克莱斯勒蝰蛇超级跑车神似。Miura车身 很低,全高只有1050毫米,双座双门,车长却有4370毫米。Miura座舱全 部玻璃包围,很有轰炸机味道。侧面看去,前后通过音波线连接,侧窗 底部正是音波线的波谷。后发动机罩通过斜面与顶棚相接。前后罩面与 座舱接连方式的不同再度把“生猛”二字强加于前车身。Miura还有不完 善的地方,意大利发动机噪声是世界闻名的。有人美其名“性感的吼 声”,虽然赛车手不会介意这些小节,但是那些肯花巨资购买跑车的人必 然是有地位的人,他们是决不会忍受隆隆作响的发动机噪声。华莱士成 立专门小组来解决这一问题,发动机与座舱之间布臵了特殊玻璃材料的 隔绝层,为了冷却发动机,Miura发动机用塑胶物质包裹,后发动机罩黑 色的水平隔栅对于排热也起到很好的作用。
Countach
LM002
1980年,兰博基尼汽车公司破产。来自瑞士的Mimran兄弟公司收购了兰博基 尼。1985年兰博基尼推出了一款越野车LM200,这是兰博基尼历史上推出的唯 一一款量产越野车,为了能够获得来自美国军方的合同,兰博基尼完全按照 高战略机动性、高战术机动性、高防护性、高隐蔽性、组件结构的军用标准 设计,拥有非常完美的机械性能及越野能力。兰博基尼提供的样车在美国加 利福尼亚沙漠的军方测试中撞毁,它的残骸也被遗弃在那里。而美国军方因 为这次测试的失败将目光转向了本土公司,但是兰博基尼并未放弃开发越野 车的计划。1981年,以Cheetah为蓝本的LM001车型问世,它搭载一部4.7L排气 量的V12汽油发动机,最高功率为382马力。在1986年推出最终量产车型之前, 兰博基尼推出了多款测试车型,最终LM002正式定型,量产版LM002搭载经过 兰博基尼工程师悉心调校的5.2L V12发动机,并配备来自ZF公司的变速箱。而 为了保证这款车能够应付恶劣环境,LM002被设计成可以使用低标号汽油, 并提供了多重燃油过滤装臵来确保进入化油器的每一滴汽油都是干净的。同 时,它还使用了一个体积巨大的散热器,确保LM002有足够的散热能力,再 加上高效的空气滤清器,LM002完全能够适应撒哈拉沙漠的恶劣气候。自重 将近3吨的LM002的百公里加速仅需7.7秒,最高时速可以达到208km/h,这样 的性能表现,在当时的越野车中独一无二。而在拥有极好的公路性能的同时, LM002也拥有极为强悍的越野能力。这款超级越野车的制造成本非常高昂, 在1993年停产时仅仅生产了328辆车。

2014年豪华版Accord跑车LX-S说明书

2014年豪华版Accord跑车LX-S说明书
EX-L adds to or replaces EX features
• Continuously variable transmission (CVT) with Sport Mode and paddle shifters
• Forward Collision Warning (FCW) 8 • Lane Departure Warning (LDW)9 • Honda LaneWatchTM10 • Driver’s seat with 10-way power adjustment, including power
EX-L with Navigation adds to or replaces EX-L features
• Honda Satellite-Linked Navigation SystemTM12 with voice recognition, FM Traffic and interface dial
EX adds to or replaces LX-S features
• One-touch power moonroof with tilt feature • Smart Entry • Fog lights • Heated power side mirrors with integrated turn indicators • Multi-angle rearview camera with guidelines • Push button start • HondaLinkTM featuring AhaTM7 compatibility • Audio touch-screen • Compass
GENUINE ACCESSORIES
Manufactured to the same strict standards as Honda vehicles, Honda Genuine Accessories are the perfect way to personalize and protect your vehicle. Please see your Honda dealer for details.

2014年款 揽胜极光性能参数及官方报价

2014年款 揽胜极光性能参数及官方报价

耀真版
发动机智能启停系统四轮驱动系统扭矩矢量分配制动系统 全地形反馈适应系统®定速巡航
陡坡缓降控制 (HDC)
动态稳定控制系统 (DSC)车速感受式电子助力转向系统 (EPAS)
侧倾稳定系统 (RSC)牵引力控制系统 (TCS)电子驻车辅助系统 (EPB)发动机阻力矩控制系统 (EDC)电子制动力分配系统 (EBD)
紧急制动辅助系统 (EBA)
一键式按钮启动
免钥匙进入5英寸TFT 虚拟组合仪表滑盖中央储物槽
前排遮阳板带照明化妆镜全自动空调 (含空气滤清器和 AQS 自动空气循环)前排点烟器与烟灰缸
自动防眩目后视镜真皮多功能方向盘 - 集成音响控制,巡航控制以及蓝牙电话连接自定义车内氛围照明足部空间、手套箱及行李箱照明丝缎银铝合金饰面
镶边地毯纹理真皮座椅,驾驶座椅 6 向电动可调并含记忆功能,副驾驶座 4 向电动可调前排座椅电动腰托
前排加热座椅
后排座椅中央扶手带 2 个杯托
标准配置的官方指导价:RMB 528,000
耀真版
耀享版
耀享版
耀动版
耀动版。

兰博基尼 Huracán LP610-4 Spyder

兰博基尼 Huracán LP610-4 Spyder

兰博基尼 Huracán LP610-4 Spyder作者:Dan Prosser来源:《汽车与运动》2016年第04期在产品演示中有一张特殊的幻灯片格外引人注目。

这是一张简单的图表,描述了兰博基尼Huracán超级跑车的三个款型,并对每一款加以简单的介绍。

LP610-4 coupe这款跑车被贴上“性能”的标签,后轮驱动的LP580-2 coupe,被描述为具有“驾驶乐趣”的车型。

至于我在佛罗里达州驾驶的这款新车LP610-4 Spyder,则被贴上“生活方式”的标签。

基调在一瞬间就奠定了。

为什么我会被带到像迈阿密这样的大都市去驾驶一辆车速超过300km/h的超级跑车突然变得再清楚不过了。

总的来说,Huracán Spyder将花费时间缓慢行驶在全世界最富裕城市中的炫丽街道上。

兰博基尼公司清楚这一点,而且他们正是希望让汽车媒体在这种情境下测试这款新车。

1 Huracán的敞篷版看起来真的非常美妙,但是它的顶篷侵占了部分车内空间Spyder车型基于LP610-4 coupe,采用了动力更为强劲的5.2L V10发动机,而且保留了四轮驱动。

与法拉利和迈凯伦采用的折叠式硬顶敞篷不同,兰博基尼这款跑车采用纤维材质顶篷,并且驾驶员可以在车速最高50km/h时,通过一个按钮在17s内将其打开或者闭合。

Huracán Spyder的净重为1542kg,因为敞篷装置以及附加的支撑结构,给该车增加了120kg的重量。

它的整备质量要比法拉利488敞篷跑车重122kg,比迈凯伦650S敞篷跑车重172kg。

尽管如此,凭借449kW和560Nm的扭矩,Huracán Spyder仍可以完成3.4s百公里的加速度任务,同时它的最高时速为323km/h。

Huracán具有一个超强度铝合金/碳纤维结构,即使是在顶篷被打开的情况下仍可以保留相当强的抗扭性能。

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。

四大天王

四大天王

四大天王作者:张明来源:《汽车之友》2014年第08期屈指可数的几家超级跑车厂商仍保持着积极的工作状态,它们的新产品足够让富人们一掷千金,且让大多数人的梦想又一次更新。

法拉利California T变得不只是外形,还把涡轮增压器植入了身体;迈凯伦650S迫不及待地推出敞篷版,看来是想接收更多订单大干一场;布加迪威航一直琢磨着怎么能再卖出几辆,甚至不惜把祖辈精华都融入进来彰显收藏价值;兰博基尼十年磨一剑,新的“小牛”完美接班,目前是不愁卖的节奏。

开启涡轮时代—法拉利California T法拉利California T相对于老款进行了多方面改进,不仅外观、内饰有了变化,还采用了涡轮增压V8发动机。

California T进一步诠释了法拉利的运动精神,同时它又是一款精致优雅,适合日常驾驶的奢华座驾。

法拉利赋予California T全新的外观设计,前脸进气格栅采用了面积更大的三横镀铬辐条,进气口分居两侧,体现出更强时尚感。

前大灯的样式进行了调整,形似LaFerrari的大灯,凸显锋利尖锐。

California T侧面造型的灵感源自250 Testa Rossa,浮舟式前翼线条延伸至刚劲有力的车尾,体现出空气动力学的流畅动感。

尾部方面,California T的圆形尾灯变化不大,而下方的后保险杠更加突出,并加入了空气扩散器。

法拉利California T依然装备了可自动折叠硬顶,打开车顶时间仅需14秒。

内饰设计上没有太大的改动,基本保留了老款的风格,只是强调了细节方面的升级。

车内的第一印象仍是运动奢华,大面积的真皮、精细的做工体现高品质。

新加入的涡轮性能控制器位于仪表板正中央两个通风口之间,6.5英寸的显示屏设有触摸感应功能,屏幕上的信息可帮助驾驶者充分了解发动机状态。

动力方面,California T换装了一款3.8升V8双涡轮增压发动机,它的排量更小,但功率却增加了52kW,扭矩提高了250Nm,升级后的最大功率升至412kW,峰值扭矩755Nm。

完美风暴 兰博基尼 Huracán LP610-4

完美风暴 兰博基尼 Huracán LP610-4

Lamborghini Huracán LP610-4 兰博基尼Gallardo的继任者名为Hurac án,中文解释为“风暴”,Hurac án的决斗目标是法拉利458 Italia。

现在我们从兰博基尼得到了这个拥有V10发动机和449kW的宝贝Gathering Storm文/Mike Duff 译/范围@AS-范围-扭头就走完美风暴兰博基尼 Hurac án LP610-4117118你肯定知道推出一辆新车对于一个汽车公司来说是多么重要的一件事情。

全新Huracán 是Gallardo 的继任者,Gallardo 是兰博基尼历史上最为成功的车型,所以你肯定能想像出这个发布仪式将会多么的盛大。

兰博基尼找来了意大利的高级官员们参加揭幕仪式,因为这是意大利,他们的穿着走在时尚的前沿,所以兰博基尼的首席执行官Stephan Winkelmann 的衣着要比T 台上面的男模更加耀眼。

更令人惊讶的是另外一个男人出现在展台上,站在这辆全新的超级跑车旁边,眯着眼睛透过厚厚的眼镜片上下打量着Huracán ,仿佛在家中一样悠哉。

他穿着西装看起来像一个中级会计师。

然而,Ulrich Hackenberg 可是汽车业的大咖,这个严肃的德国人以严谨的态度和方式协调着整个大众集团的产品开发。

那个人有责任通过他的努力让一个在2013年销售出920万辆汽车的商业帝国,转变方向推出了一个全新的经营模式,因为最乐观的估计,Huracán 的销量也不会超过集团销售额的三千分之一。

如果我们不能清楚地知道Huracán 对于兰博基尼有多么重要,也就不知道兰博基尼对于奥迪和大众有多么重要。

如今,兰博基尼迎来了它的黄金年代,刚刚过去十年中售出的兰博基尼数量是前40年销量的两倍。

事实上,从2003年到2013年之间生产的14000辆Gallardo 是兰博基尼公司历史上总产量的一半。

双龙2014款爱腾

双龙2014款爱腾

爱腾(ActYon)的名字来源于单词active 和young的组合,有活泼、年轻之意。

它上市之初旨在打造一款个性、活力、向往自由生活的紧凑型SUV。

可爱腾从一出生就成为了争鸣文学的代表人物,在10年前,它那种张扬的个性让许多人看不顺眼,当时的大环境下提前降生的爱腾虽然拥有狂野的性能,却因其不合世俗的外表而饱受微词。

不过爱腾在环塔等比赛上的表现还是非常出色的,不辱其狂野的内心。

当时的爱腾可谓生不逢时,之后出世的宝马X6等等一系列融入了跑车个性的SUV却红得要命。

双龙也并没有气馁,正所谓“退一步,海阔天空”,于是2014款爱腾迈着时尚的步伐来到了消费者面前。

与其个性更加贴切的设计语言上一代爱腾的前脸太过于个性了,现在双龙终于走出了自我欣赏,在保持纯爷们底蕴的同时,外观也与世界潮流相符合。

前脸大胆采用了柯兰多的设计语言,发动机舱盖上凸起的线条肌肉感十足,黑色六边形进气格栅和凌厉的鹰眼前大灯使得外观更加刚劲有力。

只是前脸的修改就达到了洗心革面的效果,转眼之间变成了一位充满肌肉的爷们,韩国的美容技术确实厉害。

它依然保持了双门跑车的轮廓,在继续追求个性的同时力求更加贴合大众审美。

新爱腾车身尺寸为4465×1890×1765mm,轴距为2740mm,车身尺寸虽然紧凑,可轴距不小,在城市SUV中可以称作“中规中矩”;另外,爱腾接近角和离去角分别达到了26°和29°,最小离地间隙达到227mm,使其超越了城市SUV,这些奠定了灵活的操控性和出色的越野通过性。

爱腾后排座椅可以3种方式折叠以适应不同的行李形状,使其Active + Young=ActYon爱腾两驱模式是后轮驱动,这也是它不同于城市SUV的地方,它会带给你一些后驱车的驾驶乐趣行李空间从374L扩展到1081L,加上车顶的行李架,轻松应对自驾出游。

城市表现流畅我体验的是G23D汽油四驱自动豪华版,其匹配的是一款经典的2.3L汽油发动机,最大功率110kW/5500rpm、最大扭矩214Nm/3500~4600rpm。

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后悬挂类型:
横向推杆水平悬挂
车轮制动:
2013款Aventador LP 700-4 Roadster
前制动器类型:
通风盘式
后制动器类型:
通风盘式
驻车制动类型:
电子驻车
前轮胎规格:
255/35 R19
后轮胎规格:
335/30 R20
备胎:

LP 570-4 SQUADRA CORSE
325
0-100加速时间(s):
3.2
工信部油耗(L/100km):
12.5
官方综合油耗(L/100km):
-
保修政策:
3年不限公里
车身参数:
2014款Huracan LP 610-4
车长(mm):
4459
车宽(mm):
1924
车高(mm):
1165
轴距(mm):
2620
车重(kg):
1422
最小离地间隙(mm):
供油方式:
多点电喷
环保标准:
欧IV
变速箱:
2011款Aventador LP700-4
挡位个数:
7
变速箱类型:
AMT
变速箱名称:
序列变速箱
底盘转向:
2011款Aventador LP700-4
驱动方式:
中置四驱
车体结构:
承载式
助力类型:
电动助力
前悬挂类型:
横向推杆水平悬挂
后悬挂类型:
横向推杆水平悬挂
供油方式:
多点电喷
环保标准:
欧IV
变速箱:
2013款Aventador LP 700-4 Roadster
挡位个数:
7
变速箱类型:
AMT
变速箱名称:
序列变速箱
底盘转向:
2013款Aventador LP 700-4 Roadster
驱动方式:
中置四驱
车体结构:
承载式
助力类型:
电动助力
前悬挂类型:
横向推杆水平悬挂
-
保修政策:
3年不限公里
车身参数:
2013款Aventador LP 700-4 Roadster
车长(mm):
4780
车宽(mm):
2030
车高(mm):
1136
轴距(mm):
2700
车重(kg):
1575
最小离地间隙(mm):
-
车身结构:
硬顶敞篷车
车门数:
2
座位数:
2
油箱容积(L):
90
行李箱容积(L):
-
行李箱最大容积(L):
-
发动机:
2013款Aventador LP 700-4 Roadster
排量(L):
6.5
进气形式:
自然吸气
气缸排列形式:
V型
汽缸数:
12
最大功率(kW):
515
最大功率转速(rpm):
8250
最大扭矩(Nm):
690
最大扭矩转速(rpm):
5500
燃料:
汽油
燃油标数:
2011款Aventador LP700-4
厂商指导价:
666.89万
品牌:
兰博基尼
级别:
跑车
发动机:
6.5L515kW
变速箱:
7挡AMT
长×宽×高(mm):
4780×2030×1136
车身结构:
2门2座跑车
上市年份:
2011
最高车速(km/h):
350
0-100加速时间(s):
2.9
工信部油耗(L/100km):
6500
燃料:
汽油
燃油标号:
97号(京95号)
供油方式:
直喷
环保标准:
欧V
变速箱:
2014款Huracan LP 610-4
挡位个数:
7
变速箱类型:
双离合
变速箱名称:
双离合变速箱
底盘转向:
2014款Huracan LP 610-4
驱动方式:
中置四驱
车体结构:
承载式
助力类型:
电动助力
前悬挂类型:
双叉臂式独立悬架
2014款HuracanLP 610-4参数配置
基本参数:
2014款Huracan LP 610-4
厂商指导价:
429.09万
品牌:
兰博基尼
级别:
跑车
发动机:
5.2L449kW
变速箱:
7挡双离合
长×宽×高(mm):
4459×1924×1165
车身结构:
2门2座跑车
上市年份:
2014
最高车速(km/h):
厂商指导价:
738.88万
品牌:
兰博基尼
级别:
跑车
发动机:
6.5L515kW
变速箱:
7挡AMT
长×宽×高(mm):
4780×2030×1136
车身结构:
2门2座硬顶敞篷车
上市年份:
2013
最高车速(km/h):
350
0-100加速时间(s):
3
工信部油耗(L/100km):
-
官方综合油耗(L/100km):
-
车身结构:
跑车
车门数:
2
座位数:
2
油箱容积(L):
-
行李箱容积(L):
-
行李箱最大容积(L):
-
发动机:
2014款Huracan LP 610-4
排量(L):
5.2
进气形式:
自然吸气
气缸排列形式:
V型
汽缸数:
10
最大功率(kW):
449
最大功率转速(rpm):
8250
最大扭矩(Nm):
560
最大扭矩转速(rpm):
-
官方综合油耗(L/100km):
-
保修政策:
3年不限公里
车身参数:
2011款Aventador LP700-4
车长(mm):
4780
车宽(mm):
2030
车高(mm):
1136
轴距(mm):
2700
车重(kg):
1575
最小离地间隙(mm):
-
车身结构:
跑车
车门数:
2
座位数:
2
油箱容积(L):
90
后悬挂类型:
双叉臂式独立悬架
车轮制动:
2014款Huracan LP 610-4
前制动器类型:
通风盘式
后制动器类型:
通风盘式
驻车制动类型:
电子驻车
前轮胎规格:
245/30 R20
后轮胎规格:
305/30 R20
备胎:

安全配置:
2014款Huracan LP 610-4
2011款AventadorLP700-4参数配置
行李箱容积(L):
-
行李箱最大容积(L):
-
发动机:
2011款Aventador LP700-4
排量(L):
6.5
进气形式:
自然吸气
气缸排列形式:
V型
汽缸数:
12
最大功率(kW):
515
最大功率转速(rpm):
8250
最大扭矩(Nm):
690
最大扭矩转速(rpm):
5500
燃料:
汽油
燃油标号:
97号(京95号)
车轮制动:
2011款Aventador LP700-4
前制动器类型:
通风盘式
后制动器类型:
通风盘式
驻车制动类型:
电子驻车
前轮胎规格:
255/35 R19
后轮胎规格:
335/30 R20
备胎:

2013款AventadorLP 700-4 Roadster参数配置
基本参数:
2013款Aventador LP 700-4 Roadster
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