About 35 results
https://drivepatents.com/patents/1386150 · 15 Apr 2026
The present invention concerns a method for controlling an aircraft (1) comprising at least two engines (16, 17), each engine (16, 17) being arranged in its own engine compartment (21, 22), each engine (16, 17) being connected to a fuel supply circuit (31,...
https://drivepatents.com/patents/1386298 · 25 Feb 2026
Aircraft (1) fitted with a turbine engine (10) comprising a gas generator (15), the gas generator (15) comprising a compression assembly (20) supplying air to a combustion chamber (24) as well as a turbine assembly (25) supplied with gas by the combustion ...
https://drivepatents.com/patents/1386550 · 25 Feb 2026
The present invention relates to a method for controlling a rotorcraft (1), said rotorcraft (1) comprising at least two combustion engines (2, 3), at least one control system (13) and a transmission system (4), said at least two engines (2, 3) being mechan...
https://drivepatents.com/patents/1395433 · 21 Jan 2026
La présente invention concerne un procédé de détection d'une ingestion de gaz chauds au sein d'un aéronef (1) ayant au moins une entrée d'air (20) configurée pour alimenter en air frais au moins un moteur (15). Le procédé comporte (i) une mesure d...
https://drivepatents.com/patents/1396301 · 31 Dec 2025
La présente invention concerne un système et un procédé (20) d'aide au pilotage d'un aéronef, ledit procédé (20) comportant lors d'une phase de vol dudit aéronef au moins deux étapes de mesure (21, 21') d'au moins deux valeurs courantes respective...
https://drivepatents.com/patents/1386712 · 24 Dec 2025
The present invention relates to a partition for a vehicle (10) comprising a structure (41) pierced with an opening (43) forming an emergency exit (44) closed off by a movable panel (45) as well as an assistance device (1) for the evacuation of persons thr...
https://drivepatents.com/patents/1397552 · 26 Nov 2025
The present invention relates to a rotary wing aircraft 100 that extends along a roll axis R between a nose region 101 and an aft region 102, comprising: at least one first single-blade rotor 120 and at least one second single-blade rotor 130 which are spa...
https://drivepatents.com/patents/1386425 · 12 Nov 2025
The present invention relates to an actuator (10) equipped with a pump (15) connected to a first hydraulic line (30) connected to a reservoir (25) and to a second hydraulic line (35). A control controller (40) communicates with a first pressure sensor (41)...
https://drivepatents.com/patents/1387857 · 13 Aug 2025
The present invention relates to a method of training for the piloting of a rotorcraft (1) comprising at least two engines (3, 4) and at least one rotor (5) participating in the lift of said rotorcraft (1) in the air. Such a said method (10, 20) comprises ...
https://drivepatents.com/patents/1388075 · 25 Jun 2025
The present invention relates to a method of controlling an economical operating mode for an aircraft (1) comprising two heat engines (11), only one of said heat engines (11) being active and supplying mechanical power to said rotor (2,3) in said economica...