About 61 results
https://drivepatents.com/patents/988341 · 24 Jul 2013
The attachment element has a nacelle (30) and an annular tube element (31) that are connected with each other by a fastening unit, such that relative movement between nacelle and annular tuber element is ensured. Two struts are arranged at specific angle w...
https://drivepatents.com/patents/984830 · 26 Jun 2013
Accessories (35) are mounted to a gas turbine engine from a frame (14)attached to a pylon which is used to mount the engine to an airframe. The frame independently mounts the accessories so that engine vibrations are not transmitted to the accessories.
https://drivepatents.com/patents/990949 · 8 May 2013
The component has a base (11) that is arranged with high temperature coating portion (2). The base is provided with structural element (1) which is connected with high temperature coating portion. The cross section of structural element is provided with th...
https://drivepatents.com/patents/985658 · 13 Mar 2013
The assembly (25) has a combustion fuel pump of a combustion fuel cycle, and hydraulic fluid pumps (28 to 31) of a hydraulic fluid circulation system, where the assembly with an accessory gearbox shaft (39) is coupled to an accessory gearbox unit (9) of an...
https://drivepatents.com/patents/985797 · 6 Mar 2013
The generator (12) has a rotor (23) coupled to a shaft (13) of an auxiliary gearbox device (9) of an engine and rotatably mounted relative to a stator (25). A stator region (28) receiving the stator is separated from a rotor region (27) receiving the rotor...
https://drivepatents.com/patents/985800 · 6 Mar 2013
The gearbox device (9,10) has drive shaft (13,21) that are connected with engine shaft (14) of the jet engine (1). The generators (12,36) are provided on the drive shaft and/or in the region of the operative connection between the drive shaft. The engine s...
https://drivepatents.com/patents/985792 · 6 Mar 2013
The auxiliary equipment gear device (9) has a drive shaft that is actively connected to the main shaft (11) of the engine (1). An extension shaft is provided that is coaxial to the drive shaft and is operatively connected to the releasable drive shaft, whe...
https://drivepatents.com/patents/993346 · 30 Jan 2013
The cone (28) has honeycomb-structured layer (30) which is arranged inside outer wall (29) extending along inner side of outer wall. An inner wall (31) connected to honeycomb structure has passage recesses connecting area of honeycomb structure to annular ...
https://drivepatents.com/patents/994035 · 9 Jan 2013
The aircraft gas turbine engine has an engine core (10) that is surrounded by a secondary flow channel (29). A side wall (30) is arranged radially outside the secondary flow channel. The radial inner wall (31) of the secondary flow channel is extended simi...
https://drivepatents.com/patents/995653 · 28 Nov 2012
The device has an annular tubular element (31) extended along a circumferential direction. The tubular element comprises outflow openings for supplying hot air to a ring lip region (29) of a double-walled nacelle (30) for removing snow and ice. The tube el...