Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Aircraft engine assembly comprising a pylon leading edge incorporated with an annular row of unfaired after-guide vanes

Aircraft engine assembly comprising a pylon leading edge incorporated with an annular row of unfaired after-guide vanes

US Patent 10556699 · Granted Feb 11, 2020

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Forward engine mount for a half or full wraparound pylon2025
Forward engine mount for a half or full wraparound pylon2025
Assembly for an aircraft comprising a wing and an engine pylon for coupling a pr2025
Aircraft having an engine pylon with a mobile cowl2025
Assembly for an aircraft comprising a wing and an engine pylon for coupling a pr2025
Engine pylon for coupling a jet engine to a wing of an aircraft2024
Aircraft comprising an engine pylon with a movable cover assembly and a specific2024
System and method for non-model based control utilizing turbine exit mach number2024
Method for manufacturing a cellular structure obtained from bent strips of mater2024
Assembly for a nacelle of an aircraft engine, said assembly comprising a fixed c2024
Shackle for fastening an aircraft engine comprising a pair of encapsulated anti-2024
Propeller propulsion unit comprising a heat engine and an electric motor and air2024