INSTALLATION FOR TESTS OF THE CIRCUIT HEAT PIPE OF THE SYSTEM OF THERMAL REGULATION OF THE AIRCRAFT Russian patent published in 2018 - IPC F28D15/02 

FIELD: heating equipment.

SUBSTANCE: technical solution relates to heat engineering, in particular, to thermal control systems (TCS) of aviation and rocket technology devices. In the installation for testing the contour heat pipe of TCS of an aircraft containing frame, heater, cooler and temperature measuring instruments, the frame is made in the form of a spatial power frame with the ability to withstand the mechanical loads acting in flight on the aircraft; the installation is equipped with a CHP condenser cooler installed in the frame, made in the form of a heat accumulator with a predetermined mass of the working substance, at the same time, the condenser cooler and the heater with the CHP evaporator are located at opposite ends of the frame, the steam pipe and the CHP condensate line are fixed on the frame of the unit with the specified mounting step, and the heater with the CHP evaporator and heat accumulator are thermally insulated.

EFFECT: confirmation of the efficiency of the contour heat pipe of TCS of an aircraft, flying in conditions of alternating and time-varying external mechanical loads (significant overloads, vibrations).

1 cl, 1 dwg