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公开(公告)号:US20150308343A1
公开(公告)日:2015-10-29
申请号:US14649161
申请日:2013-12-19
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Jonathan Ariel Scott , John J. Henderson , Ralph D. Harris
CPC classification number: F02C7/20 , F01D25/162 , F01D25/24 , F01D25/28 , F01D25/30
Abstract: A turbine exhaust case frame (100) comprises an inner ring (104), an outer ring (102), and a plurality of load-bearing struts (106). The inner ring is configured to carry a load from inner bearings. The outer ring has installation bosses (116) with downward-facing mount surfaces (120). The load-bearing struts connect the inner ring to the outer ring.
Abstract translation: 涡轮机排气箱框架(100)包括内圈(104),外圈(102)和多个承载支柱(106)。 内圈配置为承载内轴承的负载。 外环具有带有向下安装表面(120)的安装凸台(116)。 承载支柱将内圈连接到外圈。
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公开(公告)号:US10036324B2
公开(公告)日:2018-07-31
申请号:US14649161
申请日:2013-12-19
Applicant: United Technologies Corporation
Inventor: Jonathan Ariel Scott , John J. Henderson , Ralph D. Harris
CPC classification number: F02C7/20 , F01D25/162 , F01D25/24 , F01D25/28 , F01D25/30
Abstract: A turbine exhaust case frame (100) comprises an inner ring (104), an outer ring (102), and a plurality of load-bearing struts (106). The inner ring is configured to carry a load from inner bearings. The outer ring has installation bosses (116) with downward-facing mount surfaces (120). The load-bearing struts connect the inner ring to the outer ring.
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