Unsteady modes behaviour of cabin air temperature control system

Аuthors

Volkov A. A.

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

e-mail: aa_volkov@scac.ru

Abstract

The article is dedicated to developing and analisis of mathemetical model for pressured cabin which is an object of temperature regulating system for regional aircraft. Article considers the impact of temperature sensor location onto unsteady processes in temperature regulating system.

Keywords:

сertification, pressured zone, bay, flow, temperature, time, delay, feedback sensor, heating rate, thermal inertia.