Fuel Metering System Flashcards
(98 cards)
What factor is not used in the operation of an aircraft gas turbine engine fuel control unit?
mixture control position
In order to stabilize cams, springs, and linkages within the fuel control, manufacturers generally recommend that all final turbine engine trim adjustments be made in the
increase direction
When trimming a turbine engine, the fuel control is adjusted to
set idle RPM and maximum speed or EPR
A supervisory electronic engine control (EEC) is a system that receives engine operating information and
adjust a standard hydro mechanical fuel control unit to obtain the most effective engine operation
A full-authority electronic engine control (EEC) is a system that receives all the necessary data for engine operation and
develops the commands to various actuators to control engine parameters
In a supervisory EEC system, any fault in the EEC that adversely affects engine operation
causes an immediate reversion to control by the hydro mechanical fuel control unit
The active clearance control (ACC) portion of an EEC system aids turbine engine efficiency by
ensuring turbine blade to engine case clearance are kept to a minimum by controlling case temperatures
What should be checked/changed to ensure the validity of a turbine engine performance check if an alternate fuel is to be used?
fuel specific gravity setting
The generally acceptable way to obtain accurate on-site temperature prior to performing engine
trimming is to
hang a thermometer in the shades of the nose wheel well until the temperature reading stabilizes
An aircraft should be facing into the wind when trimming an engine. However, if the velocity of the wind blowing into the intake is excessive, it is likely to cause a
false high compression and turbine discharge pressure, and a subsequent low trim
Generally, the practice when trimming an engine is to
turn all accessory bleed air off
A reciprocating engine automatic mixture control responds to changes in air density caused by changes in
altitude or temperature
On a float-type carburetor, the purpose of the economizer valve is to
provide a richer mixture and cooling at maximum power output
The fuel metering force of a conventional float-type carburetor in its normal operating range is the difference between the pressure acting on the discharge nozzle located within the venturi and the pressure
acting on the fuel in the float chamber
If the main air bleed of a float-type carburetor becomes clogged, the engine will run
rich at rated power
Which method is commonly used to adjust the level of a float in a float-type carburetor?
add or remove shims under the needle valve
What is the possible cause of an engine running rich at full throttle if it is equipped with a float-type carburetor?
clogged air bleed
One of the things a metering orifice in a main air bleed helps to accomplish (at a given altitude) in a carburetor is
better fuel Evaporation and control of fuel discharge, especially at lower engine speeds
A punctured float in a float-type carburetor will cause the fuel level to
rise and en-richen the mixture
The back-suction mixture control system operates by
varying the pressure acting on the fuel in the float chamber
If an aircraft engine is equipped with a carburetor that is not compensated for altitude and temperature variations, the fuel/air mixture will become
richer as either the altitude of temperature increases
Float-type carburetors which are equipped with economizers are normally set for
their leanest practical mixture delivery at cruising speeds and enriched by means of economizer
system at higher power settings
If a float-type carburetor becomes flooded, the condition is most likely caused by
a leaking needle valve and seat assembly
If an engine is equipped with a float-type carburetor and the engine runs excessively rich at full throttle,
a possible cause of the trouble is a clogged
main air bleed