发明名称 Thrust balancing
摘要 A gas turbine engine having variable geometry flow controllers therein for controlling mass flow in accordance with engine operation includes a rotor with a wide variation in thrust forces thereon during different phases of engine operation countered by a variable axial load integrating device having a rotating hydraulic thrust compensating piston mounted forwardly of the rotor in association with a rotor thrust bearing and further including means for generating a centrifugal head in accordance with engine speed and wherein improved oil distribution panels are included to evenly distribute oil between the rotating piston and a nonrotating counterpiston to form a uniform depth of rotating oil automatically regulated by an integral, flow regulator having flow area therethrough varied in accordance with axial position of a thrust bearing carriage that has the variable rotor thrust loading imposed thereon.
申请公布号 US4268220(A) 申请公布日期 1981.05.19
申请号 US19790017608 申请日期 1979.03.05
申请人 GENERAL MOTORS CORPORATION 发明人 MALOTT, RICHARD C.
分类号 F01D3/04;F01D25/16;(IPC1-7):F01D3/04 主分类号 F01D3/04
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