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 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|