About 14 results
https://drivepatents.com/patents/975217 · 7 May 2014
Thrust reversers (300) and methods to provide reverse thrust are disclosed. An example thrust reverser includes a cascade (316) to direct air from an interior volume of an engine nacelle (304) to generate reverse thrust with respect to a direction of trave...
https://drivepatents.com/patents/975472 · 30 Apr 2014
A gas turbine engine has a core engine and a nacelle having a cowl translatable along the axis of the engine from a stowed position to a deployed position, A thrust reverser cascade extends circumferentially about the engine axis. To obviate the need for a...
https://drivepatents.com/patents/975470 · 30 Apr 2014
A blocker door for a gas turbine engine thrust reverser having a tray with a base and sidewalls extending about the base to define a volume, the volume being closed by a cover that extends beyond the periphery of the tray. The extension of the cover beyond...
https://drivepatents.com/patents/985103 · 17 Apr 2013
An aircraft engine thrust reverser cascade assembly (100) includes a plurality of circumferentially spaced cascade segments (102), each cascade segment (102) including a plurality of spaced vanes (105), including an aft-most vane (107), and rails (104) def...
https://drivepatents.com/patents/1001202 · 20 Jun 2012
A thrust reverser assembly (12) for use in a turbofan engine assembly (10) is provided. The engine assembly including a core gas turbine engine (14), a core cowl (18) which circumscribes the core gas turbine engine, a nacelle (32) positioned radially outwa...
https://drivepatents.com/patents/1079253 · 16 Mar 2005
An aircraft structure comprising a duct having an inlet for fluid flow into the duct and a first outlet for fluid flow out of the duct is disclosed. The duct is configured to guide fluid flow out of the duct through the first outlet in an at least partiall...
https://drivepatents.com/patents/1084006 · 15 Sep 2004
A thrust reverser for a jet engine of a mobile platform. The thrust reverser includes a hinge beam (104) defining a first track (112) and a latch beam (104') defining a second track (112'). The thrust reverser also includes at least one cascade support rin...
https://drivepatents.com/patents/1087404 · 6 May 2004
A bulkhead (18) is mounted on a fan cowl (16). A translating cowl (20) is supported for movement between a closed position adjacent the bulkhead and an open position spaced apart from the bulkhead to form an outlet (35) for discharging air from an air duct...
https://drivepatents.com/patents/1097121 · 2 Apr 2003
The lock is for a bypass aircraft gas turbine thrust reverser with guides (60) for the movable reverser sections (50) having rails (64) attached to the movable sections (50) and slides (62) attached to longitudinal beams (36). The lock has locking assembli...
https://drivepatents.com/patents/1097884 · 5 Mar 2003
A synchronization cross-feed system for a thrust reverser having at least first and second sides. Each side of the thrust reverser has a thrust reverser actuation system having a plurality of actuators. The actuators in each thrust reverser actuation syste...