15.11 Fuel Systems (Level 1, 4 Questions) Flashcards
(80 cards)
What could happen if the fuel flow becomes excessive in a gas turbine engine?
a) The turbine blades might freeze
b) A compressor stall or rich blowout could occur
c) The engine might accelerate too quickly
b) A compressor stall or rich blowout could occur
What are the three categories of gas turbine engine fuel control systems?
a) Hydromechanical, manual, and digital systems
b) Hydromechanical, hydromechanical/electronic, and FADEC
c) Manual, automatic, and semi-automatic systems
b) Hydromechanical, hydromechanical/electronic, and FADEC
How many categories of gas turbine engine fuel control systems are there?
a) Two
b) Three
c) Four
b) Three
What is the key advantage of the hydromechanical/electronic fuel control system?
a) It operates entirely without electronics.
b) It can function as both a hydromechanical and an electronic control.
c) It eliminates the need for servo motors in fuel control.
b) It can function as both a hydromechanical and an electronic control.
What enables FADEC to have complete control over the engine?
a) Manual pilot inputs and traditional controls.
b) Electronic sensors and outputs that meter fuel flow.
c) Hydromechanical backups and emergency overrides.
b) Electronic sensors and outputs that meter fuel flow.
What is the primary goal of all turbine engine fuel control systems?
a) To match the power requested by the flight crew through precise fuel scheduling.
b) To limit engine thrust regardless of fuel delivery.
c) To sense weather conditions and automatically adjust thrust.
a) To match the power requested by the flight crew through precise fuel scheduling.
What are the two sections of a hydromechanical fuel control system?
a) Speed sensing and pressure monitoring
b) Computing and metering
c) Electronics and hydraulics
b) Computing and metering
What differentiates a pure hydromechanical fuel control system from other types?
a) It uses electronic sensors to assist fuel flow computation.
b) It has no electronic interface and relies solely on mechanical components.
c) It operates only during high engine speeds.
b) It has no electronic interface and relies solely on mechanical components.
What is a drawback of hydromechanical fuel control systems compared to electronic controls?
a) They cannot sense engine speed.
b) Their fuel metering is less accurate.
c) They are too complex to operate.
b) Their fuel metering is less accurate.
What advancement improved the hydromechanical fuel control system?
a) Adding a fuel shut-off section
b) Combining with an electronic control system
c) Using atomised fuel delivery
b) Combining with an electronic control system
What device adjusts the fuel flow in a hydromechanical/electronic fuel control system?
a) Hydromechanical assembly
b) Fuel shut-off valve
c) Electronic Engine Control (EEC)
c) Electronic Engine Control (EEC)
What is the purpose of the vane fuel pump in the engine fuel system?
a) To provide low-pressure fuel for the engine
b) To deliver high-pressure fuel to the control system
c) To bypass excessive fuel to the combustion chamber
b) To deliver high-pressure fuel to the control system
What happens when the pressure drop across the fuel filter is excessive?
a) The filter automatically cleans itself
b) The fuel bypasses the filter via a bypass valve
c) The engine shuts down to prevent damage
b) The fuel bypasses the filter via a bypass valve
What does FADEC stand for?
a) Fuel Automatic Digital Electronic Control
b) Full Authority Digital Electronic Control
c) Fast Action Digital Engine Control
b) Full Authority Digital Electronic Control
Does the FADEC system have a hydromechanical backup?
a) Yes, it has a full hydromechanical backup
b) No, it does not have a hydromechanical backup
c) It depends on the engine type
b) No, it does not have a hydromechanical backup
How does the FADEC system control fuel flow?
a) Manually by the pilot
b) By using electronic sensors and adjusting the fuel metering valve through the EEC
c) By a mechanical linkage connected to the throttle
b) By using electronic sensors and adjusting the fuel metering valve through the EEC
What is the primary component of the FADEC engine fuel control system?
a) Fuel metering valve
b) Electronic Engine Control (EEC)
c) Throttle lever
b) Electronic Engine Control (EEC)
How many electronic channels does the EEC have?
a) One
b) Two (A and B)
c) Three
b) Two (A and B)
Where is the EEC usually located?
a) In the cockpit
b) In a cool area of the engine nacelle
c) Inside the fuel tank
b) In a cool area of the engine nacelle
What kind of memory does the EEC contain for storing performance and maintenance data?
a) Only volatile memory
b) Only non-volatile memory
c) Both volatile and non-volatile memory
c) Both volatile and non-volatile memory
What is the main purpose of the secondary fuel system?
a) To store fuel
b) To supply fuel to the combustion chamber
c) To monitor engine temperature
b) To supply fuel to the combustion chamber
What is the difference between the primary and secondary fuel systems on an aircraft?
a) Primary stores fuel, secondary supplies it to the engine
b) Primary controls engine speed, secondary adjusts thrust
c) There is no difference between them
a) Primary stores fuel, secondary supplies it to the engine
What are the two subsystems of the engine fuel system?
a) Combustion and distribution subsystems
b) Fuel distribution and fuel control subsystems
c) Storage and control subsystems
b) Fuel distribution and fuel control subsystems
What is one main task of the engine fuel distribution system?
A) To safely supply fuel to the combustion chamber
B) To reduce fuel consumption
C) To store extra fuel
A) To safely supply fuel to the combustion chamber