Independent compartment temperature control for single-pack oper

Refrigeration – Automatic control – Air compessor – cooler and expander

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Details

62 87, 62402, F25D 900

Patent

active

055113850

ABSTRACT:
A dual-pack, aircraft environmental control system has each pack dedicated to providing a temperature-controlled air supply to a corresponding compartment, either the crew or passenger, of the aircraft. Each refrigeration pack is fed hot, compressed bleed air from an associated turbine engine on the aircraft. During normal operation, the pack associated with a particular compartment on the aircraft provides the air supply with independent temperature control to that compartment. However, during failure of one of the refrigeration packs and the resulting operation of the other pack, the environmental control system is able to provide independent temperature control of the air supplied to each compartment.

REFERENCES:
patent: 2767562 (1956-10-01), Hall
patent: 3177679 (1965-04-01), Quick et al.
patent: 4283924 (1981-08-01), Schutze
patent: 4550573 (1985-11-01), Rannenberg
patent: 4966005 (1990-10-01), Cowell et al.
patent: 5309724 (1994-05-01), Schreiber et al.

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