Resources Contact Us Home
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










 
 
  Recently Added Patents
Wound dressings
Optimized control of an energy supplying system and an energy consuming system
Semiconductor device manufacture in which minimum wiring pitch of connecting portion wiring layer is less than minimum wiring pitch of any other wiring layer
Methods and compositions for improved F-18 labeling of proteins, peptides and other molecules
Memory access monitoring method and device
Peer to peer (P2P) missing fields and field valuation feedback
Image processing apparatus, image processing method, and program
  Randomly Featured Patents
Surface traversing vehicle
User configuration file for access control for embedded resources
Magnetic recording and/or reproducing apparatus in which a head and a recording medium are detached from each other pursuant to the position of the head confronting the medium
Multilayer printed circuit board
Shallow angle elbow
Screw - thread arrangement
Method for forming MOS transistors with improved sidewall structures
System, method and computer program product for intuitive interactive navigation control in virtual environments
Detachable tool and paint caddy for use with a ladder
Method and apparatus for producing half-tone printing forms with rotated screens on the basis of randomly selected screen threshold values