![Heat transfer system and method for turbine engine using heat pipes](/ep/2008/02/06/EP1884628A2/abs.jpg.150x150.jpg)
基本信息:
- 专利标题: Heat transfer system and method for turbine engine using heat pipes
- 专利标题(中):Wärmeübertragungssystemund -verfahrenfürTurbinenmotorenüberWärmerohre
- 申请号:EP07112983.7 申请日:2007-07-24
- 公开(公告)号:EP1884628A2 公开(公告)日:2008-02-06
- 发明人: Venkataramani, Kattalaicheri Srinivasan , Moniz, Thomas Ory , Stephenson, Justin Paul
- 申请人: The General Electric Company
- 申请人地址: 1 River Road Schenectady NY 12345 US
- 专利权人: The General Electric Company
- 当前专利权人: The General Electric Company
- 当前专利权人地址: 1 River Road Schenectady NY 12345 US
- 代理机构: Illingworth-Law, William Illingworth
- 优先权: US460791 20060728
- 主分类号: F01D25/08
- IPC分类号: F01D25/08 ; F01D9/06 ; F01D5/08
摘要:
A heat transfer system is provided for a turbine engine of the type including an annular casing (10) with an array of thermally conductive, generally radially-extending strut members disposed therein. The heat transfer system includes at least one arcuate heat pipe (36) disposed in contact with an outer surface of the casing within fore-and-aft limits of the axial extent of the strut members. The heat pipe (36) is thermally coupled to a heat source, such that heat from the heat source can be transferred through the heat pipe (36) and the casing (10) to the strut members.
摘要(中):
提供了一种用于这种类型的涡轮发动机的传热系统,该涡轮发动机包括具有布置在其中的导热的大致径向延伸的支柱构件阵列的环形壳体(10)。 传热系统包括至少一个弓形热管(36),其布置成与支柱构件的轴向范围的前后限制的壳体的外表面接触。 热管(36)热耦合到热源,使得来自热源的热量可以通过热管(36)和壳体(10)传递到支柱构件。
公开/授权文献:
IPC结构图谱:
F | 机械工程;照明;加热;武器;爆破 |
--F01 | 一般机器或发动机;一般的发动机装置;蒸汽机 |
----F01D | 非变容式机器或发动机,如汽轮机 |
------F01D25/00 | 不包含在其他各组或与其无关的部件、零件或附件 |
--------F01D25/08 | .冷却(一般的机器或发动机的冷却入F01P);加热;隔热 |