Numerical study of thermoelectric power generation for an helicopter conical nozzle

被引:35
|
作者
Kousksou, Tarik [1 ]
Bedecarrats, Jean-Pierre [1 ]
Champier, Daniel [2 ]
Pignolet, Pascal [2 ]
Brillet, Christophe [3 ]
机构
[1] Univ Pau & Pays Adour UPPA IFR A Jules Ferry, Lab Sci Ingn Appliquees Mecan & Genie Elect SIAME, Federat CNRS IPRA, F-64000 Pau, France
[2] Univ Pau & Pays Adour, Lab Genie Elect, F-64053 Pau, France
[3] Turbomeca Grp SAFRAN, F-64511 Bordes, France
关键词
Thermoelectric generator; Power generation; Numerical simulation; Low Mach number; Helipcopter conical nozzle; Waste heat recovery; SIMULATION; DESIGN; MODEL;
D O I
10.1016/j.jpowsour.2010.12.015
中图分类号
O64 [物理化学(理论化学)、化学物理学];
学科分类号
070304 ; 081704 ;
摘要
This paper investigates the electric power extractable from an helicopter conical nozzle equipped with thermoelectrical modules. The thermoelectric nozzle is heated by the final exhaust gas from helicopter turbine and cooled by oil. A computer model has been developed to simulate the performance of the thermoelectric system. Results were obtained for various operating conditions showing that the electrical power produced in real operating conditions is significant but currently insufficient if we consider the weight-to-power ratio. The numerical model is also used to optimize the electric power showing a good potential for the future. (C) 2010 Elsevier BM. All rights reserved.
引用
收藏
页码:4026 / 4032
页数:7
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