Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Control system for turbojet engine nozzle flaps

Control system for turbojet engine nozzle flaps

US Patent 4817871 · Granted Apr 4, 1989

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Axisymmetric, directable and adjustable turbojet-engine exhaust nozzle2001
Turbojet engine thrust reverser and exhaust nozzle assembly2001
System for the admission of air into a working section of a gas turbine engine2000
Variable geometry turbojet engine exhaust nozzle1999
Turbojet equipped with a deicing system on the intake case1997
Actuating system for a variable area exhaust nozzle1997
Gas turbine engine rotor blading sealing device1997
Supersonic nozzle for a turbojet engine1996
Supersonic nozzle, in particular for a turbojet engine1996
Nozzle for a jet engine containing an adjustable convergent-divergent portion1996
Inter-blade platform for a bladed disc of a turbomachine rotor1995
Integral composite gas turbine afterburner structure1994