#B64D31/14

DEVICE FOR INHIBITING THE INTERRUPTION OF A PROPULSION ENGINE FOR AN AIRCRAFT

An inhibition device is intended to prevent an inappropriate shutdown of an engine of an aircraft. The inhibition device authorizes by default an actuation of the shutdown member and receives informat…

DRIVE·Mar 18·2 min read

B64D31/14 AIRBUS OPERATIONS SAS [FR]

ELECTRIC POWER GENERATION CONTROLLER FOR USE IN AIRCRAFT

An electric power generation controller for use in an aircraft is a controller of an electric power generating apparatus including a manual transmission which changes speed of rotational power of an a…

DRIVE·Jul 17·2 min read

B64D31/14 KAWASAKI HEAVY IND LTD [JP]

SYSTEMS AND METHODS FOR FUEL CELL AUXILIARY POWER IN SECONDARY FUEL APPLICATIONS

A cryogenic fuel auxiliary power system (200) for an engine (20) may include a cryogenic fuel supply (210), a first valve (212) in fluid communication with the cryogenic fuel supply and configured to …

DRIVE·Oct 11·1 min read

B64D31/14 RAYTHEON TECH CORP [US]

POWER DISTRIBUTION SYSTEM AND POWER DISTRIBUTION METHOD

A power distribution system is installed in an aircraft, and comprises: a first DC power supply unit including a generator ; a second DC power source unit including a battery , a step-up/down converte…

DRIVE·Sep 8·1 min read

B64D31/14 MITSUBISHI HEAVY INDUSTRIES, LTD.

Redundant Electric Propulsion System

A propulsion system for providing propulsion of an aircraft includes a plurality of electric motors coupled with a rotor of the aircraft to drive the rotor and a propulsion motor control. The propulsi…

DRIVE·Aug 18·1 min read

B64D31/14 Bell Textron Inc.

Method for control scheduling to achieve linear thrust response

A method for achieving linear engine thrust response comprising the steps of measuring a throttle position (FNRQ), measuring a plurality of engine parameters, inputting the plurality of engine paramet…

DRIVE·Jun 8·1 min read

B64D31/14 UNITED TECHNOLOGIES CORP [US]