Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Gas turbine engine impeller having an annular collar platform

Gas turbine engine impeller having an annular collar platform

US Patent 5263823 · Granted Nov 23, 1993

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

One-block bladed disk provided with blades with adapted foot profile2017
Injecting air into the flow path of a turbomachine compressor2013
Checking of turbomachine blades2010
Compressor stator having a constant clearance2003
Axisymmetric, directable and adjustable turbojet-engine exhaust nozzle2001
Turbojet engine thrust reverser and exhaust nozzle assembly2001
Hybrid component with high strength/mass ratio and method of manufacturing said 2000
System for the admission of air into a working section of a gas turbine engine2000
Variable geometry turbojet engine exhaust nozzle1999
Hybrid component with high strength/mass ratio and method of manufacturing said 1999
Drill bit having a hemispherical head with an evolutive cut1998
Turbomachine blade made of composite material1997