Accelerometer based power control apparatus for aircraft subsyst

Details Accelerometer based power control apparatus for aircraft subsyst Accelerometer based power control apparatus for aircraft subsyst

1990-03-13

1991-04-02

Hickey, R. J.

Electricity: battery or capacitor charging or discharging

Serially connected batteries or cells

With discharge of cells or batteries

307 107, 307121, H02J 700, H01H 3514

Patent

active

050049631

ABSTRACT:
An accelerometer based power control apparatus for use in an aircraft subsystem (where the subsystem may be a fire extinguishing system) utilizes an independent battery source. The battery is connected to the aircraft subsystem only during the flight of the aircraft by a positive indication of an associated accelerometer which closes a switch connecting the battery to the aircraft subsystem.

REFERENCES:
patent: 3803475 (1974-04-01), Anichini
patent: 3967180 (1976-06-01), Weber et al.
patent: 4207511 (1980-06-01), Radtke
patent: 4581571 (1986-04-01), Hansen
patent: 4849655 (1989-07-01), Bennett

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