Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Composite material turbomachine engine blade or vane, compressor stator segment or turbine nozzle segment incorporating such vanes and method for manufacturing same

Composite material turbomachine engine blade or vane, compressor stator segment or turbine nozzle segment incorporating such vanes and method for manufacturing same

US Patent 9062562 · Granted Jun 23, 2015

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Fibrous reinforcement for the manufacture of a composite part intended to be art2025
Method for manufacturing a composite material part intended to be articulated to2025
Method for three-dimensional weaving of a fibrous structure with orientation of 2025
Machinery for winding a fibrous textured material, and associated winding method2025
Fiber texture for a casing made of composite material with improved impact resis2025
Weaving loom with tiltable reed and weaving method2025
Turbine engine for an aircraft2025
Method for densifying a fibrous texture by injecting a slip2025
Method for densifying a fibrous texture by injecting a slip2025
Method for producing a preform for part of a blade or propeller by winding a wea2025
Fastening of an exhaust cone in a turbomachine turbine2025
Woven fibrous preform for producing a part from composite material, in particula2025