當前的位置: 引擎 Engine> UAV> AR682 (FOR UAV)
引擎
AR682 (FOR UAV)



AR682 (FOR UAV) 性能與規格

AR682
 Type

 Twin Rotor Wankel – type rotary engine ?

 Displacement 排氣量  294 cm3 per rotor
 Power Output 動力輸出  100 kW nominal at 6000 engine RPM
 Weight 重量  51 kg for full wet running installed assembly. As illustrated including 2 kW generator, throttle
 actuator, fuel pump and pressure regulator etc . Propeller not included
 Housing Cooling 外殼冷卻

 Water – Glycol mixture with centrifugal pump and dual parallel fail – safe thermostat system

 Rotor Cooling 轉子冷卻

 Air – cooling using belt – driven centrifugal fan

 Direction of System 旋轉方向  Anti – clockwise (looking at prop flange)
 Ignition System 點火系統

 Full duplicated 28 V C.D system with magnetic triggering firing twin sparkplugs. R.F shielded

 Carburettors 化油器  Twin Tillotson diaphragm type. Close in mounting minimises possible icing  ACD option ,ESI  option
 Fuel feed 供油裝置

 Electric pump

 Fuel Type 燃油類型

 AVGAS (100 LL) or Regular grade

 (min 92 RON) Mogas automotive (leaded or unleaded)
 Lubrication 潤化裝置

 Total loss via metering pump from separate tank

 Oil Usage 機油使用量

 403cm3 per hour at 5000 RPM and proportional to RPM.l

 Oil Type 機油種類

 Mobil Pegasus 1 or direct equivalents

 Starting System 啟動系統

 By external cranking device to prop flange

 Generator 發電機

 Optional direct drive types

 Propeller Flange

 6 x M8 at 75 PCD

 Reduction Drive Option

 See AR682R