About 23 results
https://drivepatents.com/patents/1391062 · 28 May 2025
A tie rod-locking nut assembly (2000) includes a tie rod-locking nut (2100) threaded onto a jack bolt (1610), a jack bolt-locking nut (2200) inserted between the tie rod-locking nut (2100) and the jack bolt (1610), an anti-loosening washer (2300) formed to...
https://drivepatents.com/patents/1400658 · 17 Apr 2024
A first bracket adapted (42) to be coupled to an aircraft engine accessory (30) has a first bore with a first annular bushing (54) with a threaded radially inner surface extending through the first bore. A second bracket (44) operatively coupled to an engi...
https://drivepatents.com/patents/965916 · 24 Dec 2014
It is intended to provide a single-casing steam turbine and a single-shaft combined-cycle power plant using the steam turbine that are capable of suppressing the performance decline of the high-pressure blade rows. A steam turbine 3 is a single-casing stea...
https://drivepatents.com/patents/968879 · 15 Oct 2014
A boss for attachment of an auxiliary device to a fan case of an engine is comprised of a pedestal including a plurality of accumulated layers of reinforcement fibers and a matrix combining the reinforcement fibers together, the pedestal comprising a botto...
https://drivepatents.com/patents/968702 · 15 Oct 2014
A gas turbine engine 10 is provided that has a rigid dressing raft 200 mounted to a rigid part of the gas turbine engine 10. The rigid dressing raft 200 comprises at least a part of a component or system of the gas turbine engine. For example, the rigid dr...
https://drivepatents.com/patents/968692 · 15 Oct 2014
A rigid raft is provided for a gas turbine engine. The raft has an electrical system and/or a fluid system embedded in the material of the raft. The raft further has one or more first mounts for mounting the raft to the gas turbine engine, and one or more ...
https://drivepatents.com/patents/969612 · 24 Sep 2014
A supporting device for a gas turbine includes a base frame (200); a fixing member (10) installed on the base frame (200) so as to support one endof a gas turbine; and an absorbing member (20) installed on the base frame (200) so as to support the other en...
https://drivepatents.com/patents/977177 · 19 Mar 2014
A method and a system for a mounting device (220) are provided. The mounting device includes at least two shells (222,224), each shell having an inner surface (228) and an outer surface (234) wherein the outer surface includes a first banding zone (246), a...
https://drivepatents.com/patents/983857 · 2 Oct 2013
An exhaust diffuser for a gas turbine comprises an annular duct (1). A row of struts (6) is arranged in the duct. In a region downstream of the trailing edges (TE) of the struts (6), the cross-sectional area of the duct decreases to a local minimum (M) and...
https://drivepatents.com/patents/984142 · 4 Sep 2013
A gas turbine fuel feeding system (1) including at least one flexible conduit (4) connecting a fuel manifold (5) with a burner (2); wherein the flexible conduit includes a first piping with multiple metal walls (10) including at least one bellows sleeve (1...