#B64D15/12

TURBO EXPANDERS FOR TURBINE ENGINES HAVING HYGRODEN FUEL SYSTEMS

An aircraft propulsion system includes aircraft systems having at least one hydrogen tank and an aircraft-systems heat exchanger and engine systems having at least a main engine core, a high pressure …

DRIVE·May 27·2 min read

B64D15/12 RTX CORP [US]

TURBO EXPANDERS FOR TURBINE ENGINES HAVING HYDROGEN FUEL SYSTEMS

DRIVE·May 6·2 min read

B64D15/12 RTX CORP [US]

NACELLE INLET STRUCTURE WITH FOAM CORE

An assembly (54) for an aircraft propulsion system (20) includes a nacelle inlet structure (34) extending axially along and circumferentially about an axis. The nacelle inlet structure (34) includes a…

DRIVE·Apr 22·2 min read

B64D15/12 ROHR INC [US]

DIFFERENTIAL LEAKAGE CURRENT MEASUREMENT FOR HEATER HEALTH MONITORING

A system and method for monitoring leakage current in a heater (20) connected to a heater power supply by a power cable (14) having a first power lead (16) conducting an inlet current defining an inle…

DRIVE·Oct 15·1 min read

B64D15/12 ROSEMOUNT AEROSPACE INC [US]

ELECTRIC AIRCRAFT ENGINE

The present invention provides an electric aircraft engine. It also provides an aircraft, comprising such an electric aircraft engine. According to a first aspect of the present invention, the electri…

DRIVE·Aug 21·2 min read

B64D15/12 LILIUM EAIRCRAFT GMBH [DE]

AIRCRAFT LASER CONTRAIL REDUCTION APPARATUS AND SYSTEM

A method, system and apparatus are provided for reducing or eliminating contrails formed by an aircraft as it travels through the sky, and more particularly, to disrupting formation of contrails and a…

DRIVE·Aug 7·1 min read

B64D15/12 BOEING CO [US]

STRUCTURAL COMPONENT FOR AN AIRCRAFT WITH INTEGRATED HEATING LAYER AND STRUCTURAL BATTERY

A structural component for an aircraft including at least one heatable component section having a layer structure including an inner base structure, at least one heating layer having carbon allotropes…

DRIVE·Nov 25·1 min read

B64D15/12 Airbus Operations GmbH

Transparency including a Wireless Sensor

A transparency includes a plurality of sheets. Each sheet of the plurality of sheets can include a first major surface, an opposite second major surface, and a peripheral surface between the first maj…

DRIVE·Apr 8·1 min read

B64D15/12 PPG Industries Ohio, Inc.

Turbomachine Nacelle And Anti-Icing System And Method Therefor

An anti-icing system (60,80) and method for an aircraft engine nacelle (50,70). The nacelle (50,70) has an inlet lip (56,76) that defines a leading edge of the nacelle (50,70) and has a cross-sectiona…

DRIVE·Aug 10·1 min read

B64D15/12 MRA SYSTEMS INC [US]