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公开(公告)号：US10184358B2
公开(公告)日：2019-01-22
申请号：US14808573
申请日：2015-07-24
Applicant: United Technologies Corporation
Inventor： Dale William Petty
Abstract: A retractable exhaust liner segment according to an example of the present disclosure includes, among other things, at least one liner segment extending between a forward end and an aft end. The forward end of the at least one liner segment is configured to overlap an aft end of an engine structure and the aft end of the at least one liner segment is configured to overlap a forward end of an exhaust liner when in an assembled position. The at least one liner is configured such that a gap exists between the at least one liner segment and one of the engine structure and the exhaust liner when the at least one liner segment is moved along an axis in a first direction to a disassembled position. The gap closes as the at least one liner segment is moved along the axis in a second, different direction to the assembled position.
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公开(公告)号：US20160348581A1
公开(公告)日：2016-12-01
申请号：US15165245
申请日：2016-05-26
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： John D. Wiedemer , Dale William Petty , Jonathan Lemoine , Jason Arnold
Abstract: An example diffuser assembly includes a diffuser case, an annular ring, and a retaining tab that is mounted to the annular ring and has an end that engages an inner wall of the diffuser case. The engagement between the second end and the inner wall locks the retaining tab and limits movement of the annular ring along a central longitudinal axis of the diffuser case. Another example diffuser assembly includes a diffuser case, an annular ring, and a snap ring. The snap ring is situated in an annular groove of an inner wall of the diffuser case, and restricts movement of the annular ring along a central longitudinal axis of the diffuser case. A retaining tab is affixed to either the annular ring or the diffuser case, and has an end retaining the annular ring in the annular groove.
Abstract translation: 示例性扩散器组件包括扩散器壳体，环形环和保持突片，其被安装到环形环并且具有接合扩散器壳体的内壁的端部。 第二端和内壁之间的接合锁住保持片并限制环形圈沿着扩散器壳体的中心纵向轴线的移动。 另一示例性扩散器组件包括扩散器壳体，环形环和卡环。 卡环位于扩散器壳体的内壁的环形槽中，并且限制环形环沿着扩散器壳体的中心纵向轴线的运动。 保持翼片固定在环形圈或扩散器壳体上，并且具有将环形圈保持在环形槽中的端部。
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公开(公告)号：US09708933B2
公开(公告)日：2017-07-18
申请号：US14707811
申请日：2015-05-08
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Dale William Petty
IPC: F16B39/10 , F01D25/24 , F16B39/32 , G01N21/954 , F01D9/06
CPC classification number: F01D25/24 , F01D9/065 , F05D2220/32 , F05D2260/31 , F05D2260/83 , F16B39/32 , G01N21/954
Abstract: The present disclosure relates to plug assemblies within a gas turbine engine. In one embodiment, a plug assembly includes a boss which includes a shaft and a collar, a retaining element including at least two prongs, and a plug including a shank and at least one retaining feature. The at least two prongs of the retaining element are configured to retain the plug to the boss.
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公开(公告)号：US20160288208A1
公开(公告)日：2016-10-06
申请号：US15037028
申请日：2014-12-03
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Dale William Petty
CPC classification number: B22F3/1055 , B22F5/009 , B22F2003/1057 , B33Y10/00 , B33Y50/02 , B33Y80/00 , F01D5/025 , F01D25/285 , F05D2220/32 , F05D2230/30 , F05D2230/70 , G05B19/4099 , G05B2219/35134 , G05B2219/49007 , G06F2217/12 , Y02P10/295
Abstract: A method of making a tool includes creating a computer rile defining the tool in layers and building the tool using an additive manufacturing process that builds the tool on a layer-by-layer basis. The tool includes at least one of the following features: a substantially square dogleg inner end corner, a substantially completely cylindrical dogleg surface, an angled dogleg inlet, and an integral mounting point at or near one end of the body.
Abstract translation: 一种制造工具的方法包括创建一个计算机刀片，该刀片在层中定义刀具，并使用在逐层构建工具的添加剂制造工艺来构建刀具。 该工具包括以下特征中的至少一个：基本上为方形的狗腿内端拐角，基本上完全圆柱形的腿部表面，成角度的弯曲入口，以及位于身体一端处或附近的整体安装点。
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公开(公告)号：US20160010507A1
公开(公告)日：2016-01-14
申请号：US14808573
申请日：2015-07-24
Applicant: United Technologies Corporation
Inventor： Dale William Petty
IPC: F01D25/30
CPC classification number: F01D25/30 , F02K1/80 , F02K1/822 , F05D2230/70 , F05D2230/72 , F05D2250/34 , F05D2260/31 , Y02T50/675 , Y10T29/49229
Abstract: A retractable exhaust liner segment according to an example of the present disclosure includes, among other things, at least one liner segment extending between a forward end and an aft end. The forward end of the at least one liner segment is configured to overlap an aft end of an engine structure and the aft end of the at least one liner segment is configured to overlap a forward end of an exhaust liner when in an assembled position. The at least one liner is configured such that a gap exists between the at least one liner segment and one of the engine structure and the exhaust liner when the at least one liner segment is moved along an axis in a first direction to a disassembled position. The gap closes as the at least one liner segment is moved along the axis in a second, different direction to the assembled position.
Abstract translation: 根据本公开的示例的可伸缩排气衬套段包括在前端和后端之间延伸的至少一个衬垫段。 所述至少一个衬套段的前端构造成与发动机结构的后端重叠，并且所述至少一个衬套段的后端构造成在组装位置时与排气衬套的前端重叠。 所述至少一个衬套构造成使得当所述至少一个衬垫段沿着沿第一方向的轴线移动到拆卸位置时，所述至少一个衬套段与所述发动机结构和所述排气衬套中的一个之间存在间隙。 当至少一个衬垫段沿着轴线在朝向组装位置的第二不同方向上移动时，间隙闭合。
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Patent Agency Ranking
公开(公告)号：US20140223919A1
公开(公告)日：2014-08-14
申请号：US14172183
申请日：2014-02-04
Applicant: United Technologies Corporation
Inventor： Dale William Petty
IPC: F01D25/28
CPC classification number: F02K1/82 , F05D2260/38 , F05D2300/175 , F05D2300/176 , F05D2300/501 , Y02T50/672 , Y10T29/49947
Abstract: A gas turbine engine exhaust system includes a liner extending along an axial direction and a radial direction and circumscribing a combustion plenum, a high pressure plenum circumscribing the liner along the radial direction, a structural component circumscribing the high pressure plenum along the radial direction, and a leaf spring fastener arranged within the high pressure plenum. The leaf spring fastener is arranged between the liner and the structural component.
Abstract translation: 一种燃气涡轮发动机排气系统，包括沿着轴向和径向延伸并且围绕燃烧室的衬套，沿着径向限定衬套的高压增压室，沿着径向限定高压气室的结构部件，以及 布置在高压集气室内的板簧紧固件。 板簧紧固件布置在衬垫和结构部件之间。
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公开(公告)号：US20200149475A1
公开(公告)日：2020-05-14
申请号：US16595883
申请日：2019-10-08
Applicant: United Technologies Corporation
Inventor： Dale William Petty , Karl D. Blume , Joseph T. Caprario , Steven J. Bauer
Abstract: A disclosed gas turbine engine includes a compressor section, a combustor section, a first turbine section and a second turbine section. An outer case structure for the gas turbine engine includes a single-piece case structure with a turbine case portion and a transition case portion. The transition case portion is integrally formed with the turbine case portion as a single part module. A combustor case houses the combustor and an aft turbine case supports the low pressure turbine. The outer case includes a forward end attachable to the combustor case and an aft end attachable to the aft turbine.
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公开(公告)号：US20150345337A1
公开(公告)日：2015-12-03
申请号：US14759769
申请日：2013-01-21
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Dale William Petty , James P. Allore , Joseph T. Caprario , Steven J. Bauer
CPC classification number: F01D25/28 , F01D25/162 , F01D25/24 , F05D2230/64 , Y10T29/49828
Abstract: A turbine housing section includes a radially inner case centered on a first axis, and a radially outer case spaced radially outwardly of the inner case, and centered on a second axis. The first and second axes are offset relative to each other. A plurality of tie rods include a threaded nut received on a tie rod, with the plurality of tie rods connecting the inner and outer cases. The plurality of tie rods are spaced circumferentially about both of the first and second axes, and extend for distinct lengths between the inner and outer cases such that the inner and outer cases are held at a position wherein the first and second axes are offset
Abstract translation: 涡轮机壳体部分包括以第一轴线为中心的径向内部壳体，以及径向外部壳体，其位于内部壳体的径向外侧并且以第二轴线为中心。 第一和第二轴相对于彼此偏移。 多个拉杆包括容纳在拉杆上的螺纹螺母，多个拉杆连接内壳和外壳。 多个拉杆围绕第一和第二轴线周向间隔开，并且在内壳体和外壳体之间延伸不同长度，使得内壳体和外壳体保持在第一和第二轴线偏移的位置
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公开(公告)号：US10982565B2
公开(公告)日：2021-04-20
申请号：US14759769
申请日：2013-01-21
Applicant: United Technologies Corporation
Inventor： Dale William Petty , James P. Allore , Joseph T. Caprario , Steven J. Bauer
Abstract: A turbine housing section includes a radially inner case centered on a first axis, and a radially outer case spaced radially outwardly of the inner case, and centered on a second axis. The first and second axes are offset relative to each other. A plurality of tie rods include a threaded nut received on a tie rod, with the plurality of tie rods connecting the inner and outer cases. The plurality of tie rods are spaced circumferentially about both of the first and second axes, and extend for distinct lengths between the inner and outer cases such that the inner and outer cases are held at a position wherein the first and second axes are offset.
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公开(公告)号：US10808612B2
公开(公告)日：2020-10-20
申请号：US15165245
申请日：2016-05-26
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： John D. Wiedemer , Dale William Petty , Jonathan Lemoine , Jason Arnold
Abstract: An example diffuser assembly includes a diffuser case, an annular ring, and a retaining tab that is mounted to the annular ring and has an end that engages an inner wall of the diffuser case. The engagement between the second end and the inner wall locks the retaining tab and limits movement of the annular ring along a central longitudinal axis of the diffuser case. Another example diffuser assembly includes a diffuser case, an annular ring, and a snap ring. The snap ring is situated in an annular groove of an inner wall of the diffuser case, and restricts movement of the annular ring along a central longitudinal axis of the diffuser case. A retaining tab is affixed to either the annular ring or the diffuser case, and has an end retaining the annular ring in the annular groove.
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