فن آوری های خنک کننده فعال و منفعل برای کنترل حرارتی هواپیما در هلیکوپتر ها: لوله های گرمای حلقه و سیستم چرخه مینی بخار

This paper presents the development of a new electronic cooling concept especially conceived for helicopter avionics thermal management in the framework of 7 th FP EU project TOICA (Thermal Overall Integrated Conception of Aircraft, www.toica-fp7.eu). A prototype was developed and tested. It consists of a hybrid active-passive cooling system that combines a compact loop heat pipe (LHP) specifically designed for the hot spot treatment at blade level and an air cooled mini-Vapor Cycle System (mini-VCS), which is devoted to the overall heat rejection. This paper presents in details the design and the experimental assessment of each of the main components of the innovative cooling system at different operating test conditions. The tests explore the behavior of the LHP and of the integrated system at different hot spot heat loads, from 10 W to 50 W and heat sink temperatures. The results allow full exploitation of the potential of the proposed technology in a typical airborne scenario.