Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Turbojet engine nacelle with translatable upstream cowl

Turbojet engine nacelle with translatable upstream cowl

US Patent 9211956 · Granted Dec 15, 2015

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Thrust reverser with door of a nacelle of a turbojet engine of an aircraft with 2025
Fastening of an exhaust cone in a turbomachine turbine2025
Nacelle for an aircraft propulsion assembly comprising a flap for closing a rece2024
Front frame and deflection grid of a thrust reverser of an aircraft nacelle2024
Acoustic sealing element2024
Air intake for a turbojet engine nacelle2024
Fastening of an exhaust cone in a turbomachine nozzle2024
Thrust reverser for an aircraft bypass turbojet engine nacelle2024
Air inlet of a turbomachine nacelle including a circulation conduit of a hot air2024
Supersonic air inlet of an aircraft propelling assembly comprising a support arm2024
Supersonic speed attenuator of an air intake of an aircraft propulsion assembly 2024
Exhaust cone for a turbomachine2024