发明名称 Rotor support for a gas turbine engine
摘要 A rotor support (128) includes a first ring (160) disposed around a first axis (132), a second ring (162) disposed around the first axis (132) downstream from the first ring (160), and a plurality of beams (164, 166, 168, 170, 172) extending between the first and the second rings (160, 162). Each beam (164, 166, 168, 170, 172) is configured to provide an axial stiffness, when an axial force is exerted on the first ring (160), and a radial stiffness, when a radial force is exerted on the first ring (160). Each beam (164, 166, 168, 170, 172) has a height extending parallel to a second axis (176) and a width extending parallel to a third axis (180). The beams (164, 166, 168, 170, 172) are distributed around the first ring (160) to provide a substantially uniform circumferential axial stiffness around the rotor support (128), and the height of each beam is greater than the width of each beam. Damping can be provided by the placement of a damper (130) between the rotor support (128) and the support housing (134).
申请公布号 EP1985811(A2) 申请公布日期 2008.10.29
申请号 EP20080155241 申请日期 2008.04.25
申请人 HONEYWELL INTERNATIONAL INC. 发明人 MEACHAM, WALTER L.;TALBERT, PAUL B.
分类号 F01D25/16 主分类号 F01D25/16
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