Power switching system and method for an aircraft electrical...

Electrical transmission or interconnection systems – Vehicle mounted systems

Reexamination Certificate

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C701S070000

Reexamination Certificate

active

07875993

ABSTRACT:
A system and method for switching power sources for an aircraft electric brake system is disclosed. The method removes battery power from electric brake actuator controls during flight until landing gear extension occurs. The method utilizes a logic circuit to switch between available power sources based on a plurality of control signals. The method minimizes the total power drawn during flight, and saves battery power if the aircraft calls for operating on battery power only.

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patent: 6702069 (2004-03-01), Ralea et al.
patent: 2002/0185992 (2002-12-01), Kouwa
patent: 2003/0068981 (2003-04-01), Duthie
patent: 2004/0154880 (2004-08-01), Guaraldo
patent: 2006/0028327 (2006-02-01), Amis
patent: 2007/0102998 (2007-05-01), Jordan et al.
patent: 2008/0142318 (2008-06-01), Griffith et al.
PCT, US2007/088465, PCT International Search Report, Dec. 4, 2008.

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