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公开(公告)号：US11921490B2
公开(公告)日：2024-03-05
申请号：US16743528
申请日：2020-01-15
Applicant: United Technologies Corporation
Inventor： Steven W. Burd
IPC: G05B19/4099 , B22F5/00 , B22F7/06 , B22F10/25 , B22F10/28 , B29C64/386 , B29C64/40 , B33Y10/00 , B33Y50/00 , B33Y50/02
CPC classification number: G05B19/4099 , B22F5/009 , B22F7/062 , B22F10/28 , B29C64/386 , B29C64/40 , B33Y10/00 , B33Y50/00 , B22F10/25 , B33Y50/02 , G05B2219/35134 , G05B2219/49007 , G05B2219/49014 , Y02P10/25
Abstract: An additive manufacturing method includes segmenting a CAD file of a component along a build interface to define at least a first component segment and a second component segment, each of the first component segment and the second component segment sized to fit within an additive manufacturing build chamber; additive manufacturing the first component segment and the second component segment within the build chamber; and bonding the first component segment and the second component segment to form the component.
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公开(公告)号：US20190106993A1
公开(公告)日：2019-04-11
申请号：US16210322
申请日：2018-12-05
Applicant: United Technologies Corporation
Inventor： Steven W. Burd
IPC: F01D5/18 , B22F5/10 , B29C64/153
Abstract: An apparatus includes a component built by layer-by-layer additive manufacturing. An external structure is located on an external surface of the component. An internal structure is positioned within the component and is integrally formed to the external structure. The internal structure is made of a matrix structure, honeycomb structure, or lattice structure. The internal structure provides structural support, vibration dampening, heat transfer, energy absorption, fluid flow, or piping for the component.
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3.发明申请公开(公告)号：US20180231250A1
公开(公告)日：2018-08-16
申请号：US15348639
申请日：2016-11-10
Applicant: United Technologies Corporation
Inventor： Steven W. Burd
CPC classification number: F23M5/04 , F01D9/023 , F23M5/085 , F23R3/002 , F23R3/06 , F23R3/50 , F23R3/60 , F23R2900/03041 , F23R2900/03042 , F23R2900/03044
Abstract: A combustor for a gas turbine engine including a forward liner panel mounted to a support shell via a multiple of studs, the forward liner panel including an aft non-linear circumferential edge and an aft liner panel mounted to the support shell via a multiple of studs, the aft liner panel including a forward non-linear circumferential edge that is complementary to the aft non-linear circumferential edge.
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公开(公告)号：US09404656B2
公开(公告)日：2016-08-02
申请号：US13717232
申请日：2012-12-17
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Steven W. Burd
CPC classification number: F23R3/28 , F05D2260/14 , F23R3/10 , F23R3/12 , F23R3/14 , F23R3/286 , Y02T50/675
Abstract: In accordance with one aspect of the disclosure, a swirler is disclosed. The swirler may include an outer shroud and inner shroud. The inner shroud may be positioned radially inside the outer shroud. At least one of the outer shroud and inner shroud may have a major diameter which is larger than a minor diameter such that the shrouds define an oblong shape. The swirler may further include a plurality of vanes which may be positioned between the inner and outer shrouds.
Abstract translation: 根据本公开的一个方面，公开了一种旋流器。 旋流器可以包括外护罩和内护罩。 内护罩可以位于外护罩的径向内侧。 外护罩和内护罩中的至少一个可以具有大于小直径的大直径，使得护罩限定长方形。 旋流器还可以包括可以位于内护罩和外护罩之间的多个叶片。
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5.发明申请COMBUSTOR DILUTION HOLE ACTIVE HEAT TRANSFER CONTROL APPARATUS AND SYSTEM 审中-公开COMBUSTOR DILUTION HOLE主动换热控制装置和系统公开(公告)号：US20160178199A1
公开(公告)日：2016-06-23
申请号：US14862332
申请日：2015-09-23
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Steven W. Burd
CPC classification number: F23R3/06 , F02C6/08 , F02C7/18 , F23R3/002 , Y02T50/675
Abstract: Systems and methods are described herein whereby an air jet is configured to manipulate local aerodynamics and/or boundary layer flows associated with a dilution hole. A gas turbine component including a combustor panel, a dilution hole located within the combustor panel and an air jet located within the combustor panel positioned in close proximity to the dilution hole is described. The dilution hole is configured to produce a flow of cooling fluid. An air flow from the air jet is configured to deflect secondary flows produced within a combustor. The air jet is located close enough to a leading edge of the dilution hole such that the air flow from the air jet manipulates a pressure gradient of the dilution hole.
Abstract translation: 这里描述了系统和方法，其中空气喷射被配置为操纵与稀释孔相关联的局部空气动力学和/或边界层流。 描述了一种燃气轮机部件，其包括燃烧器板，位于燃烧器板内的稀释孔和位于靠近稀释孔定位的燃烧器板内的空气喷射。 稀释孔构造成产生冷却流体流。 来自空气射流的空气流被配置成偏转在燃烧器内产生的二次流。 空气射流位置足够靠近稀释孔的前缘，使得来自空气射流的气流操纵稀释孔的压力梯度。
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Patent Agency Ranking
公开(公告)号：US20160144434A1
公开(公告)日：2016-05-26
申请号：US14903479
申请日：2014-07-01
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Steven W. Burd
CPC classification number: B22F7/08 , B22F3/1055 , B22F5/04 , B29C64/153 , B29C64/165 , B29C64/40 , B29D99/0025 , B29K2105/251 , B29L2009/00 , B29L2031/08 , B33Y10/00 , B33Y30/00 , Y02P10/295
Abstract: An additive manufacturing system includes a support structure defining a cavity. A movable platform is contained within the cavity, and is capable of moving along a build direction within the cavity. The movable platform is shaped to receive and hold a substrate that includes at least a portion of a finished part. The movable platform, in combination with the substrate, defines a working surface for building a finished product via additive manufacturing.
Abstract translation: 添加剂制造系统包括限定空腔的支撑结构。 可移动平台被容纳在空腔内，并且能够沿着空腔内的构建方向移动。 活动平台被成形为容纳和保持包括成品部分的至少一部分的基底。 可移动平台与基底结合，限定了通过添加剂制造来建造成品的工作表面。
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公开(公告)号：US20160108745A1
公开(公告)日：2016-04-21
申请号：US14893229
申请日：2014-05-22
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Steven W. Burd , Meggan Harris , John T. Ols , William G. Askey
CPC classification number: F01D5/3069 , B22D25/02 , B23P15/006 , F01D5/02 , F01D5/12 , F01D5/3023 , F01D5/3061 , F01D5/34 , F01D9/044 , F01D25/24 , F01D25/30 , F05D2220/32 , F05D2230/21 , F05D2230/232 , F05D2230/25 , F05D2230/60 , F05D2240/24
Abstract: A unitary one-piece hub has first and second rings and a midsection arranged between the first and second rings. The midsection includes a plurality of windows configured to receive a plurality of cross members. The windows include a lip configured to surround the cross members. A gas turbine engine and a method of providing a hub for a gas turbine engine are also disclosed.
Abstract translation: 一体式单件式轮毂具有第一和第二环和布置在第一和第二环之间的中间部分。 中央部分包括被配置为接收多个横向构件的多个窗口。 窗户包括被配置为围绕横梁的唇部。 还公开了一种燃气涡轮发动机和提供燃气轮机的轮毂的方法。
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8.发明申请公开(公告)号：US20150369059A1
公开(公告)日：2015-12-24
申请号：US14764842
申请日：2013-01-30
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Steven W. Burd , Rickey P. Mercer
CPC classification number: F01D5/288 , B23P2700/06 , C23C4/12 , C23C4/18 , F01D5/005 , F01D5/186 , F05D2260/202 , Y02T50/676
Abstract: A method of coating a component having a multiple of cooling holes including removing at least a portion of a prior coating from a component; mapping a location of each of the multiple of cooling holes to generate a map of cooling holes; applying a coat to the component; adjusting the map of cooling holes to account for said coat to generate a adjusted map of cooling holes; and re-drilling the multiple of cooling holes in response to the adjusted map of cooling holes.
Abstract translation: 一种涂覆具有多个冷却孔的部件的方法，包括从组件除去至少一部分现有涂层; 映射多个冷却孔中的每一个的位置以产生冷却孔的图; 将涂层施加到部件上; 调整冷却孔的图以考虑所述涂层以产生调整的冷却孔的图; 并响应于调整好的冷却孔图来重新钻出多个冷却孔。
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公开(公告)号：US20150354460A1
公开(公告)日：2015-12-10
申请号：US14759774
申请日：2013-11-06
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Steven W. Burd
IPC: F02C7/266
CPC classification number: F02C7/266 , F23C99/001 , F23N2027/36 , F23R3/002 , F23R2900/00009
Abstract: An ignition system for a combustor of a gas turbine engine is disclosed. The ignition system may include an igniter operatively associated with the combustor, and an electrode operatively associated with the combustor and spaced from the igniter, wherein an electrical potential is created between the igniter and the electrode to produce an electric arc therebetween.
Abstract translation: 公开了一种用于燃气涡轮发动机的燃烧器的点火系统。 点火系统可以包括与燃烧器可操作地相关联的点火器和与燃烧器操作地相关联并与点火器间隔开的电极，其中在点火器和电极之间产生电位以在它们之间产生电弧。
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10.发明申请公开(公告)号：US20140255158A1
公开(公告)日：2014-09-11
申请号：US13725229
申请日：2012-12-21
Applicant: United Technologies Corporation
Inventor： Steven W. Burd , Alan C. Barron
Abstract: A method of coating a component having a multiple of cooling holes includes removing at least a portion of a prior coating; directing a gas through at least one of the multiple of cooling holes; and applying a coat layer while directing the gas through at least one of the
Abstract translation: 涂覆具有多个冷却孔的部件的方法包括去除至少一部分现有涂层; 引导气体通过多个冷却孔中的至少一个; 并且在引导气体通过所述气体中的至少一个的同时施加涂层
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