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1.发明申请ALIGNMENT SYSTEM AND METHODOLOGY TO ACCOUNT FOR VARIATION IN A GAS TURBINE ENGINE 有权燃气轮机发动机变化的对准系统和方法公开(公告)号：US20140174088A1
公开(公告)日：2014-06-26
申请号：US13725312
申请日：2012-12-21
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Jose E. Ruberte Sanchez , Joey Wong , Mark J. Ricciardo , Russell B. Hanson
CPC classification number: F02C7/20 , A61K39/395 , A61K39/3955 , C07K16/18 , C07K16/28 , F01D25/162 , F02K1/80 , F02K3/10 , F05D2260/31 , F16B33/002 , F16B35/048 , F16B43/001
Abstract: A gas turbine engine includes a bushing that is non-round in cross-section, the bushing receivable within an aperture. A fastener passes through the bushing to retain a second component to a third component with respect to the first component.
Abstract translation: 燃气涡轮发动机包括横截面为非圆形的衬套，衬套可接收在孔内。 紧固件穿过衬套，以将第二部件相对于第一部件保持在第三部件上。
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公开(公告)号：US10570944B2
公开(公告)日：2020-02-25
申请号：US15265205
申请日：2016-09-14
Applicant: United Technologies Corporation
Inventor： Jose E. Ruberte Sanchez , Joey Wong , Mark J. Ricciardo , Russell B. Hanson
Abstract: A gas turbine engine includes a bushing that is non-round in cross-section, the bushing receivable within an aperture. A fastener passes through the bushing to retain a second component to a third component with respect to the first component.
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公开(公告)号：US20170226964A1
公开(公告)日：2017-08-10
申请号：US15265205
申请日：2016-09-14
Applicant: United Technologies Corporation
Inventor： Jose E. Ruberte Sanchez , Joey Wong , Mark J. Ricciardo , Russell B. Hanson
Abstract: A gas turbine engine includes a bushing that is non-round in cross-section, the bushing receivable within an aperture. A fastener passes through the bushing to retain a second component to a third component with respect to the first component.
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4.发明授权Alignment system and methodology to account for variation in a gas turbine engine 有权对准系统和方法来解释燃气涡轮发动机的变化公开(公告)号：US09470151B2
公开(公告)日：2016-10-18
申请号：US13725312
申请日：2012-12-21
Applicant: United Technologies Corporation
Inventor： Jose E. Ruberte Sanchez , Joey Wong , Mark J. Ricciardo , Russell B. Hanson
CPC classification number: F02C7/20 , A61K39/395 , A61K39/3955 , C07K16/18 , C07K16/28 , F01D25/162 , F02K1/80 , F02K3/10 , F05D2260/31 , F16B33/002 , F16B35/048 , F16B43/001
Abstract: A gas turbine engine includes a bushing that is non-round in cross-section, the bushing receivable within an aperture. A fastener passes through the bushing to retain a second component to a third component with respect to the first component.
Abstract translation: 燃气涡轮发动机包括横截面为非圆形的衬套，衬套可接收在孔内。 紧固件穿过衬套，以将第二部件相对于第一部件保持在第三部件上。
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