Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Variable cycle propulsion engine for supersonic aircraft

Variable cycle propulsion engine for supersonic aircraft

US Patent 5311736 · Granted May 17, 1994

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Turbine engine with an alternator and method for transmitting movement to an alt2010
Method for air circulation in a turbomachine compressor, compressor arrangement 2009
Aircraft braking method and ducted fan jet engine for implementing the method2008
Turbomachine with low noise emissions for aircraft2007
Twin-spool turbojet with means for driving ancillary machines2007
Turbine wheel for turbomachine and the assembly method for such a wheel2006
Drive system for a propeller driven transport aircraft2001
Method and device for reversing the thrust of very high bypass ratio turbojet en2000
Hollow blade for a turbomachine1995
Hollow blade for a turbomachine and method of manufacturing said blade1994
Thrust reverser for a high-bypass ratio turbofan engine1993
Combined turborocket and ramjet propulsion unit1992