About 72 results
https://drivepatents.com/patents/975160 · 7 May 2014
This invention relates to a multi-spool gas turbine engine, comprising: a first generator for providing electrical power to an electrical system, the generator being driveably connected to a first spool; a second generator for providing electrical power to...
https://drivepatents.com/patents/976236 · 16 Apr 2014
An object is to increase portions (increase the amount of correction), where the rotational balance of a rotary shaft of a turbocharging device incorporating an electric motor is adjusted, and to maintain sufficient motor driving force even under a high te...
https://drivepatents.com/patents/977213 · 19 Mar 2014
A system for cooling a generator (60) mounted in the tail-cone (58) of an engine comprises a fairing (66), which receives through an inlet (68) thereof air from a bypass duct (38) and directs the bypass air (40) towards a cavity (62) of the tail-cone (58) ...
https://drivepatents.com/patents/983643 · 9 Oct 2013
To suppress hunting occurring in generator output in a low load range below a rated load such as during test operation or immediately after loading. Provided is a gas turbine control device that is used in a generating facility including a gas turbine and ...
https://drivepatents.com/patents/983915 · 2 Oct 2013
A gas turbine engine power generation system includes first, 14, and second, 24, spools respectively connected to first and second turbine sections. First, 36, and second, 38, shafts respectively are coupled to the first, 14, and second, 24, spools. First ...
https://drivepatents.com/patents/983882 · 2 Oct 2013
The present invention relates to a method of decelerating a turbine rotor (12) of a turbine engine (1), wherein at least one electric motor (30) is engaged with the turbine rotor (12), wherein a braking system (40), preferably the starting system, is engag...
https://drivepatents.com/patents/987197 · 21 Aug 2013
In one embodiment, a gas turbine engine assembly comprises an engine assembly disposed about a longitudinal axis, a core nozzle positioned adjacent the engine assembly to direct a core flow generated by the engine assembly, a fan nozzle surrounding at leas...
https://drivepatents.com/patents/988165 · 31 Jul 2013
[Problem] To provide a control method and device for a turbine generator, which can reduce generated power without wasting fuel consumption of a diesel engine when the demand power decreases and thereby the generated power is brought into an excess state. ...
https://drivepatents.com/patents/990236 · 29 May 2013
Devices and methods for supporting an accessory (32) in a gas turbine engine (10) are disclosed. The accessory (32) has an interface (36) for coupling to a shaft (24) of the gas turbine engine (10). The device comprises a first support (38) configured to s...
https://drivepatents.com/patents/990525 · 22 May 2013
A twin-shaft gas turbine can be used for 50 and 60 Hz power generation without using a reducer. A gas generator (21) includes a compressor (11) that generates compressed air, a burner (12) that burns a fuel mixed with the compressed air received from the c...