Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Exhaust nozzle thermal distortion control device

Exhaust nozzle thermal distortion control device

US Patent 4934600 · Granted Jun 19, 1990

Estimated economic value: $11,535,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Turbine blade retainer seal2007
Gland for transferring cooling medium to the rotor of a gas turbine1998
Low thermal stress impingement cooling apparatus1996
Aircraft gas turbine engine sideways mount1995
Scaled heat transfer surface with protruding ramp surface turbulators1994
Multi-axis vectorable exhaust nozzle1994
Squeeze film damper composite ring seal1993
Squeeze film damper oil control1993
Overwing thrust reverser1993
Squeeze film damper piston ring seal1993
Reduced weight nozzle actuation mechanism1993
Proportioned piston ring seals1992