Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Method and a rotary wing aircraft that are optimized so as to minimize the consequences for the occupants of said aircraft of an off-specification emergency landing

Method and a rotary wing aircraft that are optimized so as to minimize the consequences for the occupants of said aircraft of an off-specification emergency landing

US Patent 8523104 · Granted Sep 3, 2013

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Power plant for a rotary-wing aircraft provided with an engine brake as well as 2024
Rotorcraft having at least one undercarriage with at least one inclined wheel, a2022
Aircraft and landing gear provided with at least one pair of shock absorbers, an2021
Caliper braking system for aircraft landing gear having a plurality of brake dis2021
External anchoring harpoon for aircraft2019
Rotorcraft having fuel tanks mounted in suspension under a load-bearing middle f2018
Aircraft fuselage frame made of laminated composite materials and including rein2016
System for fastening a load to a rotorcraft, and a rotorcraft2016
Rotorcraft fitted with an anti-torque tail rotor that contributes selectively to2016
Rotorcraft fitted with an anti-torque tail rotor that contributes selectively to2016
Suspension system for carrying an external load with an aircraft, and an aircraf2016
Device for protecting a rotorcraft against a pyramid-shaped structure for carryi2016