公开(公告)号：US5545010A

公开(公告)日：1996-08-13

申请号：US60625

申请日：1993-05-13

Applicant: Philip J. Cederwall ,  Garrett P. Prins ,  Vern V. Leuven

Inventor： Philip J. Cederwall ,  Garrett P. Prins ,  Vern V. Leuven

IPC: F01D5/02 ,  F04D29/66 ,  F16F15/32 ,  F01D25/04

CPC classification number: F01D5/027 ,  F04D29/662 ,  F16F15/32

Abstract: Trim balancing of rotating components in the past has increased manufacturing cost. In many past applications, the time and energy required to trim balance rotating components required partial disassembly of an outer case or structure member. The present trim balancing system allows the gas turbine engine to be balanced with the outer case in situ. Access to a rotating component from the exterior of the case is made possible by a compressor air flow path and a pair of holes. The balancing can be accomplished by adding or removing weights or plugs to a band assembled on the rotating component.

Abstract translation: 过去的旋转部件的修整平衡增加了制造成本。 在许多以往的应用中，修整平衡旋转部件所需的时间和精力需要外壳或结构件的部分拆卸。 本修整平衡系统允许燃气涡轮发动机与外壳原位平衡。 通过压缩机空气流动路径和一对孔可以从壳体的外部进入旋转部件。 平衡可以通过向组装在旋转部件上的带上添加或移除重物或塞子来实现。