发明名称 TURBINE CYLINDER WITH A DEVICE TO ADJUST THE TIP CLEARANCE BETWEEN THE TURBINE BLADES AND THE CYLINDER
摘要 A housing for a turbojet engine compressor is disclosed having inner and outer housing portions which may radially expand or contract as the compressor rotor wheel blades expand or contract, so as to maintain a minimum clearance between the housing and the rotor blade tips. A heat transfer manifold is applied about the outer periphery of the outer housing portion to rapidly expand the housing during transient operating conditions of the engine.
申请公布号 DE3661750(D1) 申请公布日期 1989.02.16
申请号 DE19863661750 申请日期 1986.02.11
申请人 SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION, "S.N.E.C.M.A." 发明人 LARDELLIER, ALAIN MARIE JOSEPH
分类号 F01D11/08;F01D25/24;(IPC1-7):F01D11/08;F01D9/04 主分类号 F01D11/08
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