초록

Provided is a method and system for providing fire shield protection to an aircraft auxiliary power unit, or portion thereof, or to other aircraft systems.

대표청구항 ▼

We claim: 1. A fire protection apparatus for an aircraft engine air-cooled heat exchanger located in a compartment, the heat exchanger having an air-entry inlet facing the compartment and a flammable fluid contained therein, the fluid being pressurized during engine operation, the fire protection a

We claim: 1. A fire protection apparatus for an aircraft engine air-cooled heat exchanger located in a compartment, the heat exchanger having an air-entry inlet facing the compartment and a flammable fluid contained therein, the fluid being pressurized during engine operation, the fire protection apparatus comprising: a cover mounted adjacent the heat exchanger and moveable between at least an open position and a closed position wherein the cover substantially covers the air-entry inlet and thereby adapted to at least partially block flames in the compartment from directly impinging the heat exchanger; and a cover-moving assembly adapted to move the cover between the open and closed positions, the cover-moving assembly communicating with pressure of said fluid inside the heat exchanger, said pressure providing a primary moving force to the cover-moving assembly. 2. The fire protection apparatus of claim 1 wherein the pressure causes the cover-moving assembly to moves the cover to the open position. 3. The fire protection apparatus of claim 1 wherein a lack of pressure causes the cover-moving assembly to moves the cover to the closed position. 4. The fire protection apparatus of claim 1 wherein the cover is biased towards the closed position. 5. The fire protection apparatus of claim 1 wherein the cover-moving assembly is a cylinder and piston. 6. A fire protection apparatus for a compartment of an aircraft, the fire protection apparatus comprising: at least one shield member adapted to substantially block impingement of flames of a compartment fire on a body when the at least one shield member is in a closed position; and actuation means for moving the at least one shield member between said closed position and an open position, the actuation means partially comprising a source of pressute generated on the aircraft for a first purpose unrelated to operation of said actuation means.