Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Shape of gas passage in axial-flow gas turbine engine

Shape of gas passage in axial-flow gas turbine engine

US Patent 8192154 · Granted Jun 5, 2012

Estimated economic value: $546,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Airfoil geometry of blade for axial compressor2017
Vane profile for axial-flow compressor2017
Airfoil for axial-flow compressor capable of lowering loss in low Reynolds numbe2012
Airfoil for axial-flow compressor capable of lowering loss in low Reynolds numbe2012
Blade of axial flow-type rotary fluid machine2009
High-turning and high-transonic blade2006
Gas turbine engine2005
Advanced high turning compressor airfoils2004
Stator vane arrangement for rotating machinery2004
Turbine blade airfoil and turbine blade for axial-flow turbine2003
Turbine blade airfoil, turbine blade and turbine blade cascade for axial-flow tu2003
Stator blade and stator blade cascade for axial-flow compressor2003