发明名称 Gas turbine with small blade clearance - consists of two=part pendulum housing with carrier plates and elastic membranes
摘要 The gas turbine has an intake housing (11) with a rotor slide unit. This consists of a two-part pendulum housing (1) for the axial bearing (2), two ring-shaped carrier plates (7,8), and two elastic membranes (3,4). The carrier plates are fastened to the intake housing, and carry the pressure cases (5,6). Defined contact faces (9,10) are located between pendulum housing and intake housing. Carrier plates and pressure cases are welded together gas-proof. USE/ADVANTAGE - Gas turbine with small blade clearance has device for adjustment of optimum rotor position during stationary and non-stationary operational conditions, to improve blade tolerance.
申请公布号 DE4223495(A1) 申请公布日期 1994.01.20
申请号 DE19924223495 申请日期 1992.07.17
申请人 ASEA BROWN BOVERI AG, BADEN, AARGAU, CH 发明人 BOLLEN, JAKOBUS, 7890 WALDSHUT, DE;SCHMID, TRAUGOTT, 5430 WETTINGEN, CH
分类号 F01D3/04;F01D25/16;F02C7/06;(IPC1-7):F02C7/06;F01D21/04 主分类号 F01D3/04
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