发明授权
- 专利标题: Rotating pulse detonation system for a gas turbine engine
- 专利标题(中): 燃气轮机的旋转脉冲爆震系统
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申请号: US10422314申请日: 2003-04-24
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公开(公告)号: US06931858B2公开(公告)日: 2005-08-23
- 发明人: Kattalaicheri Srinivasan Venkataramani , Lawrence Butler , Ching-Pang Lee , Harvey Michael Maclin
- 申请人: Kattalaicheri Srinivasan Venkataramani , Lawrence Butler , Ching-Pang Lee , Harvey Michael Maclin
- 申请人地址: US NY Schenectady
- 专利权人: General Electric Company
- 当前专利权人: General Electric Company
- 当前专利权人地址: US NY Schenectady
- 代理商 William Scott Andes; James P. Davidson
- 主分类号: F02C5/04
- IPC分类号: F02C5/04 ; F02C5/11 ; F02C5/12 ; F02K3/06 ; F02K7/06 ; F02K7/075 ; F23R7/00
摘要:
A pulse detonation system for a gas turbine engine having a longitudinal centerline axis extending therethrough includes a rotatable cylindrical member having a forward surface, an aft surface, and an outer circumferential surface, where a plurality of spaced detonation passages are disposed therethrough. Each detonation passage includes at least a portion having a longitudinal axis extending therethrough oriented at a circumferential angle to the longitudinal centerline axis. The pulse detonation system further includes a shaft rotatably connected to the cylindrical member and a stator configured in spaced arrangement with the forward surface of the cylindrical member and a portion of the shaft. The stator has at least one group of ports formed therein alignable with the detonation passages as the cylindrical member rotates. In this way, detonation cycles are performed in the detonation passages so that combustion gases exit the aft surface of the cylindrical member to create a torque which causes the cylindrical member to rotate. Each detonation passage further includes a first end located adjacent the forward surface of the cylindrical member and a second end located adjacent the aft surface of the cylindrical member.
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