Auxiliary Power Unit Apu Compartment

The airborne auxiliary power is obtained from a gas turbine auxiliary power unit apu.

Auxiliary power unit apu compartment.

The galley power will automatically be load shed if the apu load reaches 165a. The apu compartment is by definition a fire zone see fig. The auxiliary power unit apu is installed within a fireproof titanium enclosure in the aft equipment compartment. The hgt400 g provides an alternate source of electrical power on the ground and in flight to 45 000 feet.

If the apu egt reaches 620 650 c the bleed air valve will modulate toward. The auxiliary power unit apu is a honeywell gas turbine hgt400 g. Aircraft apus generally produce 115 v alternating current ac at 400 hz rather than 50 60 hz in mains supply to run the electrical systems of the aircraft. However if you should accidentally take off with the apu on the busses then it will continue to power both busses.

It is isolated from the rest of the airplane by a firewall. Others can produce 28 v. The apu is a fully automated gas turbine power plant which drives an electrical generator. The purpose of the ejector is to ensure t hat a steady fl ow of air.

Automatic shutdown of the apu. An improved passive cooling system for an aircraft apu compartment that includes a lightweight annular air cooled oil cooler that is strategically oriented and shrouded to face its annular inlet away axially downstream from the exhaust of the apu to make it inherently fireproof to flames from the apu or any location within the apu compartment that fuel can accumulate. The apu installation uses the same fire hazard mitigation principles as the engines listed above plus. It also provides pneumatic power for the environmental control system ecs and for main engine starting on the ground and in flight up to 30 000 feet.

Automatic shutoff of air source. Auxiliary power unit rev 41 jul 08 2004 flight crew operating manual. Operation and control of the apu electric and bleed system is performed at the electrical and bleed air conditioning anti ice panel respectively. The unit provides compressed air for air conditioning while the airplane is on the ground and at limited altitude in flight.

Apu compartment while the sep arate consists of two inlets one for the apu engine and the o ther for the apu compartment. Standardized definitions of safety significant propulsion system and auxiliary power unit apu malfunctions and rationale for definition changes from the first report. Because of these limits the apu may only power one bus in the air. For apu operating limitations refer to the flight crew operating manual fcom csp 700 6 vol 1 chapter 2 limitations.

Standardized definitions of propulsion system and apu related aircraft hazard levels based on the consequences to the aircraft passengers and crew and rationale for. A typical apu compartment.