To provide a structure for power distribution, reduced in weight more than the conventional structure by utilizing the advantage that specified movable elements are operated in order.
In this power distribution structure especially adapted for operating the movable elements of the aircraft such as a landing device or a high lift element in order, the movable elements are operated by an electro-mechanical actuators to which the power is supplied in order from a power supplied by at least one power bus of the aircraft. This structure includes at least one distribution member, wherein at least one distribution member includes: a calibration means for calibrating the power sent from the power supply bus of the aircraft; and a switch means for selectively directing the calibrated power to one or the other of the electro-mechanical actuators.
COPYRIGHT: (C)2007,JPO&INPIT
| US5612579A | 1997-03-18 | |||
| WO2003007454A2 | 2003-01-23 | |||
| EP1099630A2 | 2001-05-16 | |||
| US5850113A | 1998-12-15 |
Jun Tsuruta
Tetsuro Shimada
Shinozaki Masami
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