Active and passive cooling technologies for thermal management of avionics in helicopters: Loop heat pipes and mini-Vapor Cycle System

2018 ◽  
Vol 5 ◽  
pp. 107-116 ◽  
Author(s):  
Claudio Zilio ◽  
Giulia Righetti ◽  
Simone Mancin ◽  
Romain Hodot ◽  
Claude Sarno ◽  
...  
Author(s):  
Randeep Singh ◽  
Tien Nguyen

Abstract This present paper investigates the potential of loop heat pipe (LHP), with respect to technological merits and application niche, in automotive thermal management. Broadly, LHP design and applicability for hot spot cooling in electronics (local dissipation), and for heat transport over longer distances (remote dissipation) has been proposed and discussed in detail. The basic module in these applications includes loop heat pipe with different shapes and sizing factors. Two types of LHP design have being tested and results discussed. The miniature version, with 10 mm thick and flat evaporator, for cooling ECU with 70 W chipset while keeping source temperature below 100 °C limit was evaluated. Two larger versions with cylindrical evaporator, 25 mm diameter & 150 mm length, and heat transfer distances of 250 mm and 1000 mm respectively were tested for power electronics and battery cooling, with more than 500 W transport capabilities in gravity field. In conclusions, loop heat pipes will provide an energy efficient passive thermal control solution for next generation low emission automotive, particularly for electric vehicles which have high level electrifications and more definitive cooling requirements.


Author(s):  
Gabriel B. Goodwin ◽  
Jesse R. Maxwell ◽  
Triem T. Hoang

As the electronics systems aboard air and spacecraft grow in scale and complexity, so too does the heat generated by those systems. A high-heat flux, compact, maintenance-free cooling system is required to meet the increased demand for heat removal. Loop heat pipes are robust and effective thermal management systems that are long-life and maintenance-free, making them ideal for use in unmanned spacecraft. Integrating a mechanical pump into a loop heat pipe system can drastically improve the system’s heat removal capacity through increased mass flowrate. Like loop heat pipes, magnetically-driven bearingless pumps are also maintenance-free, which is a necessity in the space environment. This work details the modeling of a low-flowrate, magnetically-driven bearingless centrifugal pump and a computational fluid dynamics study of the pump’s operation and performance under a range of conditions that are typical to the demands of a satellite thermal management system. The purpose of this computational study is to investigate the failure mechanism of a bench-test unit that was unable to generate a pressure head with its intended working fluid of ammonia. Model development, validation, and pump performance with multiple working fluids are discussed. The cause of the pump’s failure is investigated.


2018 ◽  
Author(s):  
Akhil Jaiswal ◽  
A. R. Anand ◽  
Simhachal Rao Chikkala ◽  
Venkata Raghavendra

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