返回首页
当前位置: 主页 > 通航资料 > TB >

TB20 MAINTENANCE MANUAL 73 发动机燃油和控制 TB20飞机维护手册(4)

时间:2011-11-12 05:05来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
  
 
PAGE INTENTIONALLY LEFT BLANK
WA
Validity : S / N 1 - 9999 73-00-00 (BA, Page 2 SEP 02
 
FUEL SUPPLY
DESCRIPTION AND OPERATION
1. GENERAL
Fuel supply is the part of the fuel system located, on one hand, between the union on firewall and the engine regulation section and, on the other hand, between the engine regulation section and the engine combustion chamber.
Fuel supply includes :
- engine pump,
- flow divider,
- injectors.
2. LOCATION (Figure 1)

COMPONENT QTY AREA ACCESS DOOR REFERENCE
Engine pump 1 100 121 / 131 73-10-01
Flow divider 1 100 121 73-10-00
Injectors 6 100 121 73-10-02

3. DESCRIPTION (Figure 2)
A. Engine pump
The engine pump supplies the injection pump with the fuel necessary to the engine operation. This pump, mechanically driven by the engine, is located on the rear table of the latter. The external part of the pump is cooled through a housing supplied by the air picked up at the level of L.H. rear bulkhead.
B. Flow divider
The flow divider receives the fuel from the injection pump. It distributes it fairly to the injectors in the cylinders and regulates injectors fuel supply depending on the mixture position on the injection pump. The junction between the injection pump and the flow divider is ensured through a hose, the junction between the flow divider and the injectors is ensured through stainless steel rigid pipes.
The flow divider transmits the fuel pressure to a dual indicator.
The flow divider is located at the engine upper part at the base of cylinders. NOTE : The flow divider does not require any adjustment.
C. Injectors
The constant flow injectors are fitted with an integrated air intake which enables fuel atomization and better spraying.
The fuel injectors flow is calibrated at ± 2 %.
The injectors are located on the external upper part of the engine cylinders.
ABAA
Validity : S / N 1 - 9999 73 10-00 (DA) Page 1 SEP 02
 
ABAA
Validity : S / N 1 - 9999 Fuel supply - Identification and location of components
Figure 1
73-10-00 (DA) Page 2 SEP 02
 

7  1 - Air vent (divider)
2 - Diaphragm (divider)
3 - Flow divider
4 - Injector
5 - Outlet towards manifold pressure / fuel flow indicator
6 - Fuel inlet from injection pump
7 - Fuel inlet (injector)
8 - Air filter
9 - Air inlet
10 - Mixture outlet (air / fuel) in cylinder
11 - Metered jet (nozzle)
  
 10  

Flow divider and injector - Description and operation
Figure 2
ABAA
Validity : S / N 1 - 9999 73-10-00Page 3
(DA) SEP 02
 
PAGE INTENTIONALLY LEFT BLANK
 
中国通航网 www.ga.cn
通航翻译 www.aviation.cn
本文链接地址:TB20 MAINTENANCE MANUAL 73 发动机燃油和控制 TB20飞机维护手册(4)
 

------分隔线----------------------------