Aircraft video monitor deployment and retraction apparatus

Aeronautics and astronautics – Miscellaneous

Patent

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Details

2441185, 312 72, 312245, 307 91, 307119, A47B 4600, B64D 1100

Patent

active

057434875

ABSTRACT:
A video monitor is deployed from an aircraft overhead storage compartment via a monitor-drive shaft selectively connected to an electric motor and retracted back into the compartment by a spring connected to the shaft. The monitor has limited rotational movement in both directions relative to the shaft. A bump sensor detects when the monitor has moved from its deployed position relative to the shaft as a result of being struck by a passenger and trips a solenoid. The solenoid, in turn, disengages the monitor-drive shaft from the motor and allows the spring to return the monitor to its stores position.

REFERENCES:
patent: 4639106 (1987-01-01), Gradin
patent: 5096271 (1992-03-01), Portman
patent: 5145128 (1992-09-01), Umeda
patent: 5181771 (1993-01-01), Robak et al.
patent: 5456529 (1995-10-01), Cheung
patent: 5583735 (1996-12-01), Pease et al.

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