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Browse by: INVENTOR PATENT HOLDER PATENT NUMBER DATE
 
 
Inventor:
Loisy; Jean
Address:
Ponthierry, FR
No. of patents:
5
Patents:












Patent Number Title Of Patent Date Issued
7363757 Turbine engine with semi-fixed turbine driving a receiver controlled so as to preserve a roughly April 29, 2008
The invention relates to a turbine engine (1) with a semi-fixed turbine, particularly for aircraft driving a receiver (2) controlled so as to preserve a roughly constant rotation speed. The turbine engine, in particular via a gear system (20), drives the receiver and an LP compressor
7162859 Variable cycle propulsion system with gas tapping for a supersonic airplane, and a method of ope January 16, 2007
A variable cycle propulsion system for a supersonic airplane, the system comprising at least one engine having means for producing exhaust gas and a gas exhaust nozzle for generating thrust for supersonic flight speeds, and at least one separate auxiliary propulsion assembly dissociated
6926232 Variable cycle propulsion system with compressed air tapping for a supersonic airplane August 9, 2005
A variable cycle propulsion system for a supersonic airplane, the system comprising at least one engine having at least one compressor and capable of generating thrust for supersonic flight speeds, and at least one auxiliary propulsion assembly separate from said engine, and capable of
6845606 Variable cycle propulsion system with gas tapping for a supersonic airplane, and a method of ope January 25, 2005
A variable cycle propulsion system for a supersonic airplane, the system comprising at least one engine having means for producing exhaust gas and a gas exhaust nozzle for generating thrust for supersonic flight speeds, and at least one separate auxiliary propulsion assembly dissociated
6688552 Variable cycle propulsion system with mechanical transmission for a supersonic airplane February 10, 2004
A variable cycle propulsion system for a supersonic airplane comprises at least one engine capable of generating thrust for flight at supersonic speeds together with at least one auxiliary propulsion assembly that is separate from the engine and that is capable of generating additional










 
 
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