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https://drivepatents.com/patents/1014093 · 6 Apr 2011
The charger (1) has a cooling device attached to a component, which comprises a power electronic device (6), an electrical motor (3), a turbine (5) and a compressor (4). The cooling device comprises a cooling plate (2), which exhibits groove type opened co...
https://drivepatents.com/patents/1014925 · 16 Mar 2011
Embodiments of the invention relate generally to turbines and, more particularly, to steam turbines, single-shaft combined-cycle turbines, and turbine systems having novel startup cooling flow configurations. In one embodiment, the invention provides a sin...
https://drivepatents.com/patents/1066449 · 14 Jun 2006
A gas turbine engine (10) is provided with an oil cooler which receives cooling air from a turbo fan (14). At times when the turbo fan (14) is operating at lower speeds, the volume of cooling air is also lowered. At such times, a supplemental airflow is pr...
https://drivepatents.com/patents/1067980 · 26 Apr 2006
A cooling system (100) and assembly method for a gas turbine engine assembly (10) that includes mounting a gas turbine engine including an inlet and an exhaust within a module (60) that includes an inlet area (62), an exhaust area (64), and an engine area ...
https://drivepatents.com/patents/1070586 · 25 Jan 2006
An ignition device assembly (40) for a gas turbine engine combustor (16). The ignition device includes a body (106) and a shroud (120), the body extending from an inlet end to an outlet end (102), the shroud extending circumferentially around at least a po...
https://drivepatents.com/patents/1070944 · 11 Jan 2006
The method for the filtering of an air mixture entails coarse filtering of the air mixture (3), feeding the coarse filtered air mixture to a compressor (11), and fine filtering of the air mixture leaving the compressor. At least a portion of the fine filte...
https://drivepatents.com/patents/1070947 · 11 Jan 2006
The method for the cooling of a gas turbine (15) entails drawing in an air mixture (5) from the environment (7) and compressing it, filtering the compressed air mixture, and feeding the filtered air mixture to at least one component of a gas turbine. The c...
https://drivepatents.com/patents/1071425 · 28 Dec 2005
A device and method for controlling fluid flow for heating or cooling an associated system such as a jet engine electronic control system, is provided. The present invention includes a housing (40) having a flow control member (66) that includes a bendable...
https://drivepatents.com/patents/1073492 · 5 Oct 2005
A gas turbine engine (20) having a turbine section cooling system is disclosed which is able to cool the turbine section (26) of the g as turbine engine (20) to an optimal operating temperature range, while at the same time not substantially degrading engi...
https://drivepatents.com/patents/1077529 · 25 May 2005
A turbofan engine (10) includes in serial flow communication a first fan (12), second fan (14), multistage compressor (16), combustor (20), first turbine (26), second turbine (30), and third turbine (34). The first turbine (26) is joined to the compressor ...