公开(公告)号：US10823412B2

公开(公告)日：2020-11-03

申请号：US15477518

申请日：2017-04-03

Applicant: United Technologies Corporation

Inventor： San Quach ,  Andreas Sadil ,  Donald W. Peters

IPC: F23R3/00 ,  F01D25/14 ,  F02K1/82 ,  F02K9/97 ,  C23C2/00 ,  C23C4/02 ,  B32B3/30

Abstract: A coated panel for a gas turbine engine includes a panel having a panel inner surface and a pocket formed in the panel inner surface, the pocket having a pocket depth. A coating is applied to the pocket such that a coating edge is disposed within the pocket to enhance coating retention to the panel. A gas turbine engine includes a turbine, a combustor to supply hot combustion gases to the turbine along a gas path, and one or more coated panels located along the gas path. The one or more panels includes a panel having a panel inner surface, and a pocket formed in the panel inner surface, the pocket having a pocket depth. A coating is applied to the pocket such that a coating edge is located within the pocket to enhance coating retention to the panel.

公开(公告)号：US10422532B2

公开(公告)日：2019-09-24

申请号：US14909226

申请日：2014-07-22

Applicant: United Technologies Corporation

Inventor： Andreas Sadil ,  Jonathan M. Jause ,  Alexander Broulidakis

IPC: F23R3/60 ,  F23R3/00 ,  F02C7/16 ,  F02C7/20 ,  F02C7/24 ,  F02C7/18 ,  F23R3/10 ,  F23R3/50 ,  F16B21/16

Abstract: A turbine engine includes a compressor section, a combustor in fluid communication with the compressor section, and a turbine section in fluid communication with the combustor section. The combustor includes a combustor region defined by at least one bulkhead panel and at least one heat shielding panel inside the combustor region. The at least one heat shielding panel is connected to the bulkhead panel via at least one cooled fastener.

公开(公告)号：US20180010482A1

公开(公告)日：2018-01-11

申请号：US15207207

申请日：2016-07-11

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Donald W. Peters ,  Andreas Sadil ,  Nico M. RappoIi ,  Amarnath Ramlogan

IPC: F01D25/04 ,  F02K3/10

CPC classification number: F01D25/04 ,  F01D25/162 ,  F01D25/30 ,  F02C7/20 ,  F02C7/22 ,  F02K3/10 ,  F05D2220/323 ,  F05D2230/237 ,  F05D2260/96 ,  F16F7/116

Abstract: A tuned mass damper for reducing vibration on a component includes a shaft connector member configured to be coupled to the component and a cable termination member. The tuned mass damper also includes at least one cable coupled to the shaft connector member and to the cable termination member such that vibration of the component is transferred to the at least one cable via the shaft connector member and increased or decreased by the at least one cable.

公开(公告)号：US20160231000A1

公开(公告)日：2016-08-11

申请号：US15025685

申请日：2014-10-01

Applicant: United Technologies Corporation

Inventor： Andreas Sadil ,  Steven W. Trinks ,  Jonathan M. Jause

IPC: F23R3/28 ,  F23R3/14

Abstract: A swirler is provided for a turbine engine. The swirler includes a swirler housing and a swirler nozzle that is attached to the housing. The housing defines a first inlet and a second inlet. The housing and the nozzle form an inner passage and an outer passage. The inner passage is radially within the nozzle and coupled with the first inlet. The outer passage is radially between the housing and the nozzle and coupled with the second inlet.

Abstract translation: 为涡轮发动机提供旋流器。 旋流器包括旋流器壳体和附接到壳体的旋流器喷嘴。 壳体限定第一入口和第二入口。 壳体和喷嘴形成内部通道和外部通道。 内部通道径向地在喷嘴内并与第一入口连接。 外部通道在壳体和喷嘴之间径向地与第二入口连接。