AIRCRAFT CAB TEMPERATURE CONTROL METHOD Russian patent published in 2009 - IPC B64D13/08 

Abstract RU 2375256 C2

FIELD: aircraft engineering.

SUBSTANCE: proposed invention covers device and method to control aircraft cab temperature. In compliance with this invention, first feed control device control feed of heated air from first source into first climatic zone of aircraft cab depending upon first temperature preset for first climatic zone. In case first aforesaid first device fails, current pressure of heated air forced from first source is controlled in first air feed device depending upon first temperature.

EFFECT: higher efficiency of control.

21 cl, 5 dwg

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RU 2 375 256 C2

Authors

Sentofante Niko

Petrak Markus

Sherer Tomas

Bukhkhol'Ts Uve

Dates

2009-12-10Published

2004-12-30Filed