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时间:2011-04-23 10:04来源:蓝天飞行翻译 作者:航空
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Блок роликов      Roller block
Кронштейн ручки управления   Circular pitch control knob holder
циклическим шагом
Узел натяжения троса    Cable tension node
Педали      Pedals
Качалка      Walking beam
 
 


 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
POWER-SUPPLY SYSTEM
 
7.1. GENERAL PROVISIONS
The helicopter’s power-supply system (Fig. 7.1) is centralized and provides energy for the helicopter’s equipment. It includes the 12V and 27V direct-current system and the 36V three-phase alternate current system.
7.2. 12V AND 27V DIRECT-CURRENT SYSTEM
The direct-current system includes:
- a 12V, 60 ./hr acid storage battery;
- a 12V 70. generator;
- a PN-27 transducer.
 7.3. 36V THREE-PHASE ALTERNATE CURRENT SYSTEM
The 36V 400 Hz three-phase alternate current system includes a PT-3-36-400 static transducer. 
 

 
 
 
Figure 7.1. ELECTRIC CIRCUIT DIAGRAM
 
 
 
 
 
 
 
 
 
Legend: 
 Электромеханизм прижимного ролика  Clamping roller electric mechanism
Стеклоочиститель    Screen wiper
Лампа освещения кабины   Cockpit lighting lamp
Электрический двигатель отопителя Heater electric engine
Генератор     Generator
Стартер     Starter
Реле старт     Start relay
Двигатель     Engine
Лампа      Lamp
Блок навигационных огней   Navigation lights block
Контроллер     Control unit
Кнопка пуска     Start button
Вентиляторы системы охлаждения  Cooling system fans
Топливный насос    Fuel pump
Указатель шага    Pitch indicator
Тахометр НВ и двигателя   Anti-torque rotor and engine tachometer
Датчик оборотов НВ    ATR rotation sensor
Гарнитуры     Headsets
Тангента     Flap
Антенна     Aerial
Датчик шага     Pitch sensor
Датчик засорения    Blockage sensor
Радиостанция .Бриз.   Breeze radio station
Пульт      Control panel
Сигнальное табло    Annunciation panel
Блок световой сигнализации  Annunciation unit
Датчик температуры главного редуктора Propulsion reduction gear temperature sensor
 
 


 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
FUEL SYSTEM
 
8.1. GENERAL PROVISIONS
The fuel system (Fig. 8.1) is designed for storing fuel in the helicopter and supplying the engine with it. The fuel used is high-octane petroleum of no less than 95 quality. Fuel tank capacity is 80 liters. The fuel is supplied from the tank to the engine through two fuel pumps. The fuel quantity in the tank is monitored by a fuel gauge, which has an indicator in the middle of the control panel. Monitoring of the pumps is done through annunciation panels.
Monitoring the engine fuel supply is done with the help of pressure indicator, which is situated on the control panel.

 
 
 
Figure 8.1 FUEL SYSTEM DIAGRAM
Legend:
 Указатель количества топлива  Fuel quantity indicator
Топливный бак    Fuel tank
Аварийный остаток   Emergency resource
 
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本文链接地址:Ultra light Helicopter AK1-3(8)