Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Compressor bleed manifold for a gas turbine engine

Compressor bleed manifold for a gas turbine engine

US Patent 5203162 · Granted Apr 20, 1993

Estimated economic value: $3,668,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Gas turbine engine systems involving mechanically alterable vane throat areas2011
Small radial profile shroud for variable vane structure in a gas turbine engine2010
Blade clearance control2009
Apparatus and method for cooling Axi-Centrifugal impeller2001
Gas turbine compressor spool with structural and thermal upgrades2001
Otological drain tube1998
Turbine engine rotor blade vibration damping device1996
Joining means for rotor discs1994
Case tying means for gas turbine engine1993
Segmented stator vane seal1992
Otological drain tube1992
Compressor case with controlled thermal environment1992