发明授权
US4460311A Apparatus for minimizing and maintaining constant the blade tip
clearance of axial-flow turbines in gas turbine engines
失效
用于最小化和保持燃气涡轮发动机中轴流涡轮机的叶片顶端间隙恒定的装置
- 专利标题: Apparatus for minimizing and maintaining constant the blade tip clearance of axial-flow turbines in gas turbine engines
- 专利标题(中): 用于最小化和保持燃气涡轮发动机中轴流涡轮机的叶片顶端间隙恒定的装置
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申请号: US265849申请日: 1981-05-21
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公开(公告)号: US4460311A公开(公告)日: 1984-07-17
- 发明人: Klaus Trappmann , Wolfgang Kruger
- 申请人: Klaus Trappmann , Wolfgang Kruger
- 申请人地址: DEX Munich
- 专利权人: MTU Motogren-Und Turbinen-Union
- 当前专利权人: MTU Motogren-Und Turbinen-Union
- 当前专利权人地址: DEX Munich
- 优先权: DEX3019920 19800524
- 主分类号: F01D11/08
- IPC分类号: F01D11/08 ; F01D5/20 ; F01D11/12 ; F01D11/24 ; F01D25/14
摘要:
Apparatus and method for minimizing and maintaining substantially constant the effective blade tip clearance between the outer free ends of rotor blades and an adjacent casing shroud of an axial-flow turbine of a gas turbine engine. The casing shroud includes a portion facing the hot gas stream and the outer rotor blade ends and a packing of high heat-resistance, high erosion-resistance ceramic elements secured to the shroud via a metal ring to face the blade tips. A heat insulator is interposed between the packing and the metal ring. A perforated conduit is mounted outside the metal ring for blowing cooling fluid against the metal ring on the side thereof remote from the insulator for equalizing the expansion of the metal ring to that of the turbine wheel. The ceramic packing includes projections facing the outer ends of the blades which are tapered so that they are easily broken off when coming into contact with the blades during running-in of the apparatus.
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