#B64D31/04

METHOD AND SYSTEM FOR SMART AND CONTINUOUS ENGINE OPERATION MONITORING

There is provided a system for monitoring an engine. The system includes a processor. A memory including instructions that, when executed by the processor, cause the processor to perform certain opera…

DRIVE·Apr 22·2 min read

B64D31/04 GEN ELECTRIC [US]

ELECTRIC POWER GENERATION CONTROLLER FOR USE IN AIRCRAFT AND ELECTRIC POWER GENERATING APPARATUS INCLUDING SAME

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

DRIVE·Aug 28·1 min read

B64D31/04 KAWASAKI HEAVY IND LTD [JP]

SINGLE LEVER CONTROL SYSTEM FOR ENGINES WITH MULTIPLE CONTROL MODES

An engine control system includes a first user control lever 10 configured for rotational movement between a first control position and a second control position and a second user control lever 14 con…

DRIVE·Aug 7·1 min read

B64D31/04 GEN ELECTRIC [US]

SYSTEM AND METHOD FOR OPERATING A MULTI-ENGINE AIRCRAFT

In an asymmetric operating regime, a first engine (102) is operating in an active mode to provide motive power to an aircraft (100) while a second engine (104) is operating in a standby mode and de-cl…

DRIVE·Apr 17·2 min read

B64D31/04 PRATT & WHITNEY CANADA [CA]

METHOD AND SYSTEM FOR DETERMINING A THROTTLE POSITION OF AN AIRCRAFT

Systems and methods for determining a throttle position of an aircraft are described herein. A first throttle position is obtained from a first sensor, a second throttle position is obtained from a se…

DRIVE·Jun 24·2 min read

B64D31/04 PRATT & WHITNEY CANADA CORP.