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公开(公告)号：EP3030753B1
公开(公告)日：2018-12-26
申请号：EP14835036.6
申请日：2014-07-18
Applicant: United Technologies Corporation
Inventor： BUDNICK, Matthew , CHUONG, Conway
CPC classification number: F01D11/005 , F01D11/001 , F01D15/10 , F01D25/24 , F02C7/28 , F05D2220/30 , F05D2220/76 , F05D2240/55
Abstract: A gas turbine engine includes an engine static structure. A fairing is supported relative to the engine static structure and configured to provide a flow path surface of a flow path extending in an axial direction. A seal plate has first and second ends radially spaced from one another with respect to the axial direction. The first end is operatively secured to the engine static structure. The second end is configured to seal relative to the fairing. The seal plate includes a portion between the first and second ends that extends substantially in the axial direction and configured to permit the second end to move away from the fairing in the axial direction relative to the first end in response to thermal growth.
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公开(公告)号：EP3296520A3
公开(公告)日：2018-05-30
申请号：EP17175782.6
申请日：2017-06-13
Applicant: United Technologies Corporation
Inventor： CHUONG, Conway
IPC: F01D11/02
CPC classification number: F01D11/025 , F05D2220/323 , F05D2230/60 , F05D2240/55 , F05D2240/60
Abstract: An assembly (20) includes a plurality of seal shoes (76) arranged about an axial centerline (22) in an annular array. The assembly (20) also includes a seal base (74) and a plurality of spring elements (78). The seal base (74) circumscribes the annular array of the seal shoes (76). A threaded base aperture (84) extends axially through the seal base (74). Each of the spring elements (78) is radially between and connects a respective one of the seal shoes (76) with the seal base (74). The spring elements (78) are formed integral with the seal base (74) and the seal shoes (76) as a unitary body.
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公开(公告)号：EP3290647A1
公开(公告)日：2018-03-07
申请号：EP17179191.6
申请日：2017-06-30
Applicant: United Technologies Corporation
Inventor： CHUONG, Conway , WILSON, Ross , WONG, Joey , PETERS, Christopher J.
Abstract: A seal sub-assembly (500) may comprise a spacer (212), at least one secondary seal (208, 210), and a secondary seal cover (206). At least a portion of the at least one secondary seal (208, 210) are located axially between the spacer (212) and the secondary seal cover (206). The spacer (212) is attached to the secondary seal cover (206). The spacer (212) may comprise a first flange (510) and a second flange (520). The at least one secondary seal (208, 210) may be located axially in line with and radially inward from the first flange (510). At least a portion of the secondary seal cover (206) may be located axially in line with and radially inward from the second flange (520).
Abstract translation: 密封子组件（500）可以包括间隔件（212），至少一个辅助密封件（208,210）和辅助密封件盖（206）。 至少一个辅助密封件（208,210）的至少一部分轴向地位于间隔件（212）和辅助密封盖（206）之间。 间隔件（212）附接到二级密封盖（206）。 间隔件（212）可以包括第一凸缘（510）和第二凸缘（520）。 所述至少一个辅助密封件（208,210）可以与所述第一凸缘（510）轴向对齐并从所述第一凸缘（510）径向向内定位。 第二密封盖（206）的至少一部分可以与第二凸缘（520）轴向对齐并从第二凸缘（520）径向向内定位。
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公开(公告)号：EP2938833B1
公开(公告)日：2017-11-01
申请号：EP13876268.7
申请日：2013-12-16
Applicant: United Technologies Corporation
Inventor： CHUONG, Conway , SCOTT, Jonathan Ariel , BUDNICK, Matthew
CPC classification number: F02C7/20 , F01D25/162 , F01D25/28 , F05D2250/42
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公开(公告)号：EP2938838B1
公开(公告)日：2017-07-05
申请号：EP13868633.2
申请日：2013-12-17
Applicant: United Technologies Corporation
Inventor： CHUONG, Conway , BUDNICK, Matthew
CPC classification number: F02C7/28 , F01D11/005 , F01D25/28 , F01D25/30
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Patent Agency Ranking
公开(公告)号：EP2938842A2
公开(公告)日：2015-11-04
申请号：EP13876419.6
申请日：2013-12-16
Applicant: United Technologies Corporation
Inventor： CHUONG, Conway , BUDNICK, Matthew
CPC classification number: F01D25/246 , F01D25/162 , F05D2260/201 , Y02T50/675
Abstract: An assembly includes a gas turbine engine component and a plate. The plate is spaced from a surface of the component and generally conforms to the shape of the surface. The plate and component form a passageway that allows for passage of a secondary gas flow between the component and the plate.
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公开(公告)号：EP2938833A2
公开(公告)日：2015-11-04
申请号：EP13876268.7
申请日：2013-12-16
Applicant: United Technologies Corporation
Inventor： CHUONG, Conway , SCOTT, Jonathan Ariel , BUDNICK, Matthew
CPC classification number: F02C7/20 , F01D25/162 , F01D25/28 , F05D2250/42
Abstract: An assembly for a gas turbine engine includes a frame, a mount, and a fairing. The mount is attached to the frame and the fairing is connected to the mount. The fairing and mount have mating anti-deflection features that engage to prevent circumferential movement of the fairing relative to the frame.
Abstract translation: 用于燃气涡轮发动机的组件包括框架，安装件和整流罩。 安装架连接到框架，整流罩连接到安装座。 整流罩和安装座具有接合防偏转特征，其接合以防止整流罩相对于框架的圆周运动。
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公开(公告)号：EP3653845A3
公开(公告)日：2020-08-19
申请号：EP19198029.1
申请日：2019-09-18
Applicant: United Technologies Corporation
Inventor： CHUONG, Conway , WONG, Joey
Abstract: A seal ring (216) for a non-contact seal (214) may comprise an annular body comprising a first side surface (304), a second side surface, an outer surface (306), and an inner surface (308), and a plurality of window openings (240) disposed in the annular body. The plurality of window openings (240) may be configured to provide access to the seal (214) for installation of a melting member (250) to secure the seal shoes (232) in an outboard direction during installation.
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公开(公告)号：EP3431837B1
公开(公告)日：2020-08-05
申请号：EP18172485.7
申请日：2018-05-15
Applicant: United Technologies Corporation
Inventor： CHUONG, Conway , WILSON, Ross
IPC: F16J15/44
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公开(公告)号：EP3249168B1
公开(公告)日：2020-01-15
申请号：EP17172269.7
申请日：2017-05-22
Applicant: United Technologies Corporation
Inventor： WHITE, Kevin W. , CHUONG, Conway
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