About 61 results
https://drivepatents.com/patents/965569 · 31 Dec 2014
A gas turbine engine assembly is connected to a pylon (14) for mounting the gas turbine engine (10) to an aircraft. The assembly has a frame (26) supporting at least one accessory (35, 50) independently of the gas turbine engine (10). The frame (26) is att...
https://drivepatents.com/patents/965813 · 24 Dec 2014
A gas turbine engine assembly is connected to a pylon (14) for mounting the gas turbine engine (10) to an aircraft. The assembly has a frame (26) supporting at least one accessory (35, 50) independently of the gas turbine engine (10). The frame (26) is att...
https://drivepatents.com/patents/967625 · 5 Nov 2014
The invention relates to a combustion chamber for a gas turbine with a combustion chamber head (37) and a heat shield (34), which are formed in one piece, wherein the heat shield (34) is provided with at least one recess (41) in which a burner (29) or an a...
https://drivepatents.com/patents/970828 · 27 Aug 2014
The aircraft gas turbine (1) has a first rotating shaft (16), through which torque is interchanged between the two units, and a coaxial-arranged second shaft (17), which is rotationally connected to an area near to a shaft end of the first shaft. A second ...
https://drivepatents.com/patents/973578 · 18 Jun 2014
An aircraft engine having a fan or propeller stage mounted to a planetary gearing system through a planetary gearing output drive shaft is provided with a lubricant system having a seal with lubricant delivery chamber for receiving a lubricant and a sealin...
https://drivepatents.com/patents/974943 · 14 May 2014
The nozzle has first and second guide devices (10, 20) arranged on a nozzle housing surface (4) and a nozzle rim (9) in a circumferential direction. The first guide device is provided with a first azimuthal guidance wall (11) and two wall elements (30). Th...
https://drivepatents.com/patents/974933 · 14 May 2014
The device has a crankshaft element rotatable about a stationary pivot axis by using an actuator. A lever is articulated by a joint to a stator vane adjusting ring with a free end of the lever connected by another joint to a center area of another lever. T...
https://drivepatents.com/patents/974931 · 14 May 2014
The nozzle (1) has nozzle-type and diffuser-type guiding devices (10, 20) alternately arranged in a circumferential direction of a nozzle surface area (4). Each guiding device comprises an azimuthal guide wall forming a trailing edge. A wall element connec...
https://drivepatents.com/patents/974912 · 14 May 2014
The combustion chamber tile (34) is designed like a plate and is provided with a mounting element (40). A bolt (38) is positively anchored on the mounting element which is provided as a separate component. A mounting section (47) is arranged at right angle...
https://drivepatents.com/patents/975147 · 7 May 2014
A booster assembly for a gas turbine engine having a first rotor assembly comprising a low pressure turbine drivingly connected to a fan via a first shaft and a second rotor assembly comprising a second turbine drivingly connected to a high pressure compre...