#B64D33/00

ENGINE BLEED POWER RECOVERY SYSTEMS AND RELATED METHODS

Engine bleed air power recovery systems (202) and related methods are disclosed. An example power recovery system (202) for an aircraft engine (110) includes a power recovery turbine (250) coupled to …

DRIVE·May 6·1 min read

B64D33/00 BOEING CO [US]

PROPULSION ASSEMBLY FOR AN AIRCRAFT, HAVING AN EXTRACTION FAN

An aircraft propulsion assembly that has a nacelle with a front opening and a rear opening, a propeller driven by an electric motor, a fuel cell supplying the electric motor with electric current, an …

DRIVE·Aug 7·1 min read

B64D33/00 Airbus Operations SAS

CONTROL CIRCUIT FOR A POWER DISTRIBUTION NODE

A power distribution node, includes a power switch controllably operable to supply energy from an input to an output when the power switch is closed and to not supply energy from the input to the outp…

DRIVE·Mar 3·1 min read

B64D33/00 GE Aviation Systems Limited

HYBRID ELECTRIC POWER DISTRIBUTION AND CONTROL FOR AN AIRCRAFT

A power system of an aircraft includes a hybrid energy storage system with at least two energy storage subsystems each having a different power-energy density, power draw characteristics and/or dissim…

DRIVE·Dec 23·2 min read

B64D33/00 United Technologies Corporation