公开(公告)号：US10240793B2

公开(公告)日：2019-03-26

申请号：US14900935

申请日：2014-04-22

Applicant: United Technologies Corporation

Inventor： Kevin Joseph Low

IPC: F23R3/28 ,  F02C7/22

Abstract: A manifold fitting receiving radial and axial manifolds and providing two radial outlets is disclosed. The manifold fitting, when used in conjunction with a fuel injector and a combustor for a gas turbine engine, reduces the radial footprint of the fuel injector and thereby allows for a more compact engine. Additionally, the manifold fitting eliminates parts, reducing weight in the process, as compared to prior art fittings. Such reductions in size, parts count, and weight are particularly beneficial for aircraft applications.

公开(公告)号：US09511388B2

公开(公告)日：2016-12-06

申请号：US13723542

申请日：2012-12-21

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Brian S. Tryon ,  Kevin Joseph Low ,  James P. Bangerter ,  Russell A. Beers ,  Alexander W. Williams

IPC: B23P17/00 ,  B23P25/00 ,  B23P6/00 ,  B05C13/00 ,  B05C13/02 ,  B05B13/02 ,  C23C16/00 ,  C23C4/00 ,  B22D19/00 ,  C23C4/12

CPC classification number: B05B13/0285 ,  B05C13/02 ,  B22D19/00 ,  C23C4/12 ,  Y10T29/49234

Abstract: A method for coating a turbine engine component comprises the steps of: providing a turbine engine component having at least one sacrificial attachment on a first side; grasping the turbine engine component via the at least one sacrificial attachment to position a first surface of the turbine engine component relative to a source of coating material; and applying a coating to said first side.

Abstract translation: 用于涂覆涡轮发动机部件的方法包括以下步骤：提供在第一侧上具有至少一个牺牲附件的涡轮发动机部件; 通过所述至少一个牺牲附件来抓住所述涡轮发动机部件，以相对于涂料源定位所述涡轮发动机部件的第一表面; 以及向所述第一侧施加涂层。

公开(公告)号：US09447972B2

公开(公告)日：2016-09-20

申请号：US13686303

申请日：2012-11-27

Applicant: United Technologies Corporation

Inventor： Jonathan M. Jause ,  Kevin Joseph Low ,  David Kwoka

IPC: F02C7/28 ,  F23R3/00 ,  F02C7/20 ,  F02C7/12 ,  F02C7/26 ,  F02C7/24 ,  F23R3/04

Abstract: A cooled combustor seal having a plurality of channels enabling cooling air to pass from outside of a combustion chamber to cool an area inside the combustion chamber around the seal is disclosed. The channels may be provided through a slider, a housing, and/or a washer of the combustor seal. One set of channels or multiple of sets of channels may be provided in the combustor seal. Each of these sets of channels may be in the slider, housing, or washer. The cooled combustor seal may be used in conjunction with an igniter to purge a cavity between the seal and the igniter.

公开(公告)号：US20160017755A1

公开(公告)日：2016-01-21

申请号：US14759700

申请日：2013-01-29

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Kevin Joseph Low

IPC: F01D25/28 ,  F01N3/20 ,  F01D25/24 ,  F02C3/04

CPC classification number: F01D25/28 ,  F01D25/24 ,  F01D25/243 ,  F01N3/20 ,  F02C3/04 ,  F05D2220/32 ,  F05D2240/35 ,  F05D2240/90

Abstract: An assembly for a gas turbine engine is disclosed. The gas turbine engine may have a combustor, a diffuser, and a tangential onboard injector. The assembly may include a common joint between the combustor, the diffuser, and the tangential onboard injector.

Abstract translation: 公开了一种用于燃气涡轮发动机的组件。 燃气涡轮发动机可以具有燃烧器，扩散器和切向板载喷射器。 组件可以包括燃烧器，扩散器和切向板载喷射器之间的公共接头。

公开(公告)号：US20150241067A1

公开(公告)日：2015-08-27

申请号：US14429087

申请日：2013-03-15

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Jonathan M. Jause ,  Kevin Joseph Low ,  Dennis John Duhamel

IPC: F23R3/60 ,  F02C7/20 ,  F02C3/04

CPC classification number: F23R3/60 ,  F01D5/082 ,  F01D25/243 ,  F02C3/04 ,  F02C7/12 ,  F02C7/20 ,  F05D2220/32 ,  F05D2230/60 ,  F05D2240/55 ,  F05D2260/30 ,  F05D2260/31 ,  F23R3/50 ,  F23R2900/00017 ,  Y02T50/676 ,  Y10T29/49346

Abstract: A combustor assembly for a gas turbine engine includes a combustor shell, a TOBI, a case, and a joint for securing the combustor shell, TOBI and case together. The joint has a combustor flange integral to the combustor shell. A TOBI flange is integral to the TOBI and a case flange is integral to the case. The combustor flange, the TOBI flange and the case flange are secured together.

Abstract translation: 用于燃气涡轮发动机的燃烧器组件包括燃烧器壳体，TOBI，壳体和用于将燃烧器壳体，TOBI和壳体固定在一起的接头。 接头具有与燃烧器壳体成一体的燃烧器凸缘。 TOBI法兰与TOBI是一体的，外壳法兰与箱体是一体的。 燃烧器法兰，TOBI法兰和外壳法兰固定在一起。

公开(公告)号：US20140144148A1

公开(公告)日：2014-05-29

申请号：US13686303

申请日：2012-11-27

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Jonathan M. Jause ,  Kevin Joseph Low ,  David Kwoka

IPC: F02C7/28

CPC classification number: F23R3/002 ,  F02C7/12 ,  F02C7/20 ,  F02C7/24 ,  F02C7/26 ,  F02C7/28 ,  F23R3/04 ,  F23R2900/00012

Abstract: A cooled combustor seal having a plurality of channels enabling cooling air to pass from outside of a combustion chamber to cool an area inside the combustion chamber around the seal is disclosed. The channels may be provided through a slider, a housing, and/or a washer of the combustor seal. One set of channels or multiple of sets of channels may be provided in the combustor seal. Each of these sets of channels may be in the slider, housing, or washer. The cooled combustor seal may be used in conjunction with an igniter to purge a cavity between the seal and the igniter.

Abstract translation: 公开了一种冷却的燃烧器密封件，其具有多个通道，使得冷却空气能够从燃烧室的外部通过以冷却围绕密封件的燃烧室内的区域。 通道可以通过燃烧器密封件的滑块，壳体和/或垫圈来提供。 可以在燃烧器密封件中设置一组通道或多组通道。 这些通道组中的每一个可以在滑块，壳体或垫圈中。 冷却的燃烧器密封件可以与点火器一起使用以清除密封件和点火器之间的空腔。