Fluid splash barrier apparatus for aircraft circuit breakers and

Electricity: electrothermally or thermally actuated switches – Electrothermally actuated switches – Fusible element actuated

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Details

2003022, 200345, 200314, 200DIG40, H01H 8502, H01H 1306, H01H 1370, H01H 900

Patent

active

054594464

ABSTRACT:
A miniature aircraft type circuit breaker (10') has a threaded mounting bushing (18) in which a push button (20) is slidably received. Push button (20) is coupled to a movable contact arm (24) to move a movable electrical contact (26) into and out of engagement with a stationary electrical contact (28). A flexible fluid splash barrier sleeve (32) is telescopically received on a reduced diameter portion (34) of push button (20) above a white indicator portion (30) of the push button and has a lower distal end portion (36) which engages an annular top surface (38) of the bushing when push button (20) is depressed to bring the electrical contacts into engagement. Adhesive material may be used to affix the barrier sleeve to the reduced diameter portion (34) which optionally can have a roughened surface to enhance adhesion.

REFERENCES:
patent: 3161743 (1964-12-01), Roeser
patent: 3175065 (1965-03-01), Strader
patent: 3316379 (1967-04-01), Clark et al.
patent: 3668356 (1972-06-01), Kekas
patent: 3678424 (1972-07-01), Iwashima
patent: 3767022 (1973-10-01), Olson
patent: 4277665 (1981-07-01), Kondo
patent: 4400677 (1983-08-01), Cobb, III et al.
patent: 4419555 (1983-12-01), Kim
patent: 4874913 (1989-10-01), Aoki

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