Quick replaceable thermal control system

Details Quick replaceable thermal control system Quick replaceable thermal control system

1986-06-23

1988-08-16

Barefoot, Galen

Aeronautics and astronautics

Aircraft structure

Passenger or crew accommodation

62382, B64D 1308

Patent

active

047638591

ABSTRACT:
An environmental control system for affording quick attachment and disconnection of a thermal control unit with respect to an aircraft fuselage. The fuselage includes a compartment communicating with the exterior of the aircraft for receiving the temperature control unit. The control unit is supported on a drawer-like mechanism positionable in the compartment by complementary interengaging guides which provide push-pull movement of the supported control unit into and out of the compartment. Complementary fluid connections and electrical connections on the thermal control unit and the aircraft fuselage are located for interconnection automatically in response to pushing the control unit into position in the fuselage compartment.

REFERENCES:
patent: 2938686 (1960-05-01), Van Winkle et al.
patent: 2948498 (1960-08-01), Johnsen et al.
patent: 3230733 (1966-01-01), Rutishauser et al.
patent: 3438219 (1969-04-01), Brugler
patent: 3640492 (1972-02-01), Star
patent: 3712078 (1973-01-01), Maynard et al.
patent: 4457140 (1984-07-01), Rastelli
patent: 4591114 (1986-05-01), Block

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