초록 ▼

An improved pressure relief system for a turbine engine (10). The pressure relief system includes a pressure relief door (12) attached to the engine shroud (16) at its forward edge. The aft edge of the door (12) is free to pivot outward in the occurrence of a bleed duct failure. The door (12) is mou

An improved pressure relief system for a turbine engine (10). The pressure relief system includes a pressure relief door (12) attached to the engine shroud (16) at its forward edge. The aft edge of the door (12) is free to pivot outward in the occurrence of a bleed duct failure. The door (12) is mounted within a cutout (26) in the engine shroud (16). The cutout (26) is sized so that the width of the forward edge of the cutout is greater than the width of the aft edge of the cutout. Opposing walls (42) on either side of the door (12) extend from the forward edge of the door at least partially to the aft edge of the door. The walls (42) extend inward approximately normal to the surface of the door (12). The walls (42) prevent hot engine gases (36) from flowing out of the sides of the cutout. Preventing hot engine gases (36) from flowing out the sides of the cutout helps to alter the air flow around the door (12) to obtain greater mixing of cool bypass air with the hot engine gases. The resulting cooler air flow decreases engine shroud (16) temperatures aft of the pressure relief door (12). The decreased temperatures on the engine shroud (16) during a bleed duct failure help to eliminate the structural requirements for high temperature materials or insulating blankets.

대표청구항 ▼

A pressure relief system for an engine shroud of a turbine engine, comprising: a cutout in the engine shroud through which gases from the engine may escape the engine shroud in the occurrence of a bleed duct failure, the cutout having a forward edge, an aft edge and opposing sides; a door having a f

A pressure relief system for an engine shroud of a turbine engine, comprising: a cutout in the engine shroud through which gases from the engine may escape the engine shroud in the occurrence of a bleed duct failure, the cutout having a forward edge, an aft edge and opposing sides; a door having a forward edge, an aft edge, and opposing sides, the forward edge of the door being pivotally coupled to the engine shroud upstream along the direction of movement of a bypass air flow; and a wall located on the opposing sides of the door and extending inward approximately normal to the door into the cutout, the wall extending at least partially from the forward edge of the door to the aft edge of the door.