Block 4 - EA-18G Power Plants Flashcards
Model type engine used in the Growler
F414-GE-400
Three modes of operation for the Auxiliary Power Unit (APU)
1) GMM - Ground
2) MES - Main Engine Start
3) ECS - Environmental Control System
Purpose of the In-Flight Refueling (IFR) probe
Allows for refueling while flying
What does the Aircraft Fuel Storage System consist of?
- 4 main bags/fuel cells
- 2 wing tanks
- 5 external drop tanks
Purpose of the foam-lined wing tanks
Allows aircraft to self seal small external damage
What does the Secondary Power Systems consist of?
- Auxiliary Power Unit (APU)
- Airframe Mounted Accessory Drive (AMAD)
- Secondary Power Compressed Air
Purpose of the APU
Gas Turbine Engine; Supplies air to ECS
Purpose of the AMAD
Transmits power to engine for starting
Purpose of Secondary Power Compressed Air
Provides pneumatic power for operating the ECS
What are the related systems in the Power Plant?
- Ignition
- Lubrication
- Main Fuel
- Afterburner Fuel
- Variable Exhaust Nozzle (VEN)
- Variable Geometry
- Anti-Icing
- Full Authority Digital Engine Control (FADEC)
- Throttle
Explain VEN
Cam and link-positioned hinged-flap, convergent-divergent nozzle mounted to the aft end of the afterburner case.
Helps push exhaust gases out the plane
Explain Variable Geometry
Consists of Fan Variable Geometry (FVG) and Compressor Variable Geometry (CVG)
- FVG provides better efficiency of the fan
- CVG provides better efficiency of the compressor
Explain Full Authority Digital Engine Control (FADEC)
Receives aircraft and engine sensor information and determines what will help the engine operate to its full potential
Components driven by the AMAD
Used to drive:
- Fuel boost / Motive flow pump
- Electrical generator
- 3000/5000 psi hydraulic pump
How does the AMAD interface with the APU and engine?
Pneumatically connected to APU through the Air Turbine Starts (ATS)