Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Front lip of a turbofan engine nacelle comprising hot-air bores upstream from acoustic panels

Front lip of a turbofan engine nacelle comprising hot-air bores upstream from acoustic panels

US Patent 10487738 · Granted Nov 26, 2019

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Additive manufacturing process for producing a structure2025
Assembly for an ejection cone of an aircraft turbomachine2025
Method for creating alveolar cores having open inner conical shapes2025
Method for manufacturing a structure with cellular cores for a turbojet nacelle2025
Method for coating short fibres2025
Acoustic attenuation panel and its manufacturing methods2025
Acoustic panel for a turbine engine2024
Acoustic attenuation panel for low-frequency waves2024
Acoustic sealing element2024
Structural and/or acoustic panel of a nacelle of an aircraft propulsion assembly2024
Nacelle air intake and nacelle comprising such an air intake2024
Method for manufacturing an environmental barrier2024