Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Flexible girder with high energy absorption, and landing gear and tail skid for an aircraft equipped with such a girder

Flexible girder with high energy absorption, and landing gear and tail skid for an aircraft equipped with such a girder

US Patent 4645143 · Granted Feb 24, 1987

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Blade made of thermoplastic composite, in particular for ducted tail rotor of a 1995
Blade made of thermoplastic composite, in particular for ducted tail rotor of a 1995
Semi-finished product and thermoplastic composite material having liquid crystal1994
Balance-bar hub for a twin blade rotor1988
Process and apparatus for metallic impregnation of a web of conductive fibres1985
Laminated stop of curved shape, particularly for the rotors of helicopters1983