Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Method for air circulation in a turbomachine compressor, compressor arrangement using this method, compression stage and compressor incorporating such a arrangement, and aircraft engine equipped with such a compressor

Method for air circulation in a turbomachine compressor, compressor arrangement using this method, compression stage and compressor incorporating such a arrangement, and aircraft engine equipped with such a compressor

US Patent 7581920 · Granted Sep 1, 2009

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
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
Variable cycle propulsion engine for supersonic aircraft1994
Thrust reverser for a high-bypass ratio turbofan engine1993
Combined turborocket and ramjet propulsion unit1992