15.11 Fuel Systems Flashcards
(98 cards)
How is power increased or decreased in the engine?
By varying the amount of fuel flow to the combustion chamber.
What is a ‘Rich blowout’?
Excess fuel cools the air-fuel mixture below combustion temperature.
The amount of oxygen in the air supply is insufficient to support combustion.
What’s the 3 main functions of an engine fuel system?
- Pressurise the fuel.
- Meter the fuel flow.
- Deliver atomised fuel flow to the combustion chamber.
What are the three main types of fuel control system?
- Hydromechanical.
- Hydromechanical/electronic.
- FADEC.
What’s the main fact about a ‘Pure hydromechanical system’?
It has no electronic interface in assisting the computing and metering of fuel.
What’s true about the accuracy of the fuel metering function in a pure hydromechanical system?
It’s not as accurate as an electronic system.
What are the two main sections of a fuel control system?
- Computing section.
- Metering section.
What be can added to a hydromechanical unit to improve fuel flow metering?
An electronic system.
What’s the 3 advantages of adding an electronic system to a hydromechanical unit?
- Can receive more inputs.
- Is more accurate.
- The hydromechanical section can then act as a backup if the electronic system fails.
What is an EEC?
Electronic engine control.
What does a hydromechanical/electronic system consist of?
A hydromechancal unit, and a remotely located EEC.
What are the two modes of a Hydromechanical/electronic system?
- Automatic mode.
- Manual mode.
What is automatic mode in a Hydromechanical/electronic system?
The EEC is in control of fuel flow metering.
What is manual mode in a Hydromechanical/electronic system?
The hydromechanical unit takes over control of fuel flow metering.
In normal operation, what does the Engine Fuel Control Unit control? (4)
- Thrust setting.
- Speed governing.
- Acceleration.
- Deceleration.
What happens if the electronic unit fails, in a Hydromechanical/electronic system?
Manual mode is activated and allows the engine to operated at a reduced power under full control of the hydromechanical unit.
Is the solenoid energised or de-energised, when in automatic mode?
The solenoid is energised.
What type of filter is the fuel supplied to the unit through?
A 200 micron inlet filter screen.
What determines the position of the metering valve, in terms of a specific ratio?
Fuel flow (wf) / Compressor discharge pressure (P3).
(wf/P3 ratio).
What does a fixed wf/P3 ratio give, in terms of thrust?
A minimum of 90% thrust, up to 30000ft, surge-free.
What drains the fuel nozzles and manifold after engine shutdown?
Drain valve assy.
Where is the Engine Fuel Control Unit usually located?
Remotely located and airframe mounted.
How is the interface between the remotely located EFCU and the engine/aircraft, achieved?
Branched wiring harness.
What does FADEC stand for?
Full Authority Digital Engine Control.