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公开(公告)号：US20190277579A1
公开(公告)日：2019-09-12
申请号：US15914042
申请日：2018-03-07
Applicant: United Technologies Corporation
Inventor： Michael A. Disori , William P. Stillman , Adam J. Diener , Alexander Broulidakis , David J. Hyland , Jeremy Styborski
IPC: F28F3/02
Abstract: A heat exchanger includes a plate portion including a top surface, bottom surface, a leading edge, a trailing edge and a plurality of internal passages extending between an inlet and an outlet. A fin portion extends outward from one of the top surface and the bottom surface. The fin portion and the leading edge of the plate portion define a leading edge contour. A cast plate for a heat exchanger and a method are also disclosed.
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公开(公告)号：US20190277571A1
公开(公告)日：2019-09-12
申请号：US15914055
申请日：2018-03-07
Applicant: United Technologies Corporation
Inventor： Michael A. Disori , William P. Stillman , Adam J. Diener , Alexander Broulidakis , David J. Hyland , Jeremy Styborski
Abstract: A plate fin heat exchanger includes a first cast plate assembly includes at least two plate portions separated by at least one cooling channel. Each of the two plate portions include a plurality of internal passages extending between a corresponding plurality of inlets and outlets. A common inlet perimeter surrounds the plurality of inlets from each of the two plate portions and an outlet perimeter surrounds the plurality of outlets from each of the two plate portions. An inlet manifold is attached at an inlet joint to the inlet perimeter. An outlet manifold is attached at an outlet joint to the outlet perimeter. A method is also disclosed.
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公开(公告)号：US10392974B2
公开(公告)日：2019-08-27
申请号：US14612469
申请日：2015-02-03
Applicant: United Technologies Corporation
Inventor： Joshua Daniel Winn , Alexander Broulidakis , Paul K. Sanchez , Anthony P. Cherolis , Joseph J. Sedor , Christopher Treat
Abstract: A fastener assembly includes a first component that includes a bushing opening. A second component includes a fastener opening. A threaded bushing is at least partially located within the bushing opening. A fastener extends through the fastener opening and engages the bushing.
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公开(公告)号：US10060631B2
公开(公告)日：2018-08-28
申请号：US14911158
申请日：2014-08-29
Applicant: United Technologies Corporation
Inventor： Christopher B. Lyons , Alexander W. Williams , Alexander Broulidakis
IPC: F23R3/00 , F23R3/60 , F02C3/14 , F01D25/16 , F01D25/24 , F01D9/04 , F02C7/20 , F23R3/04 , F04D29/54
CPC classification number: F23R3/60 , F01D9/041 , F01D25/162 , F01D25/24 , F01D25/243 , F02C3/14 , F02C7/20 , F04D29/54 , F04D29/542 , F23R3/04 , Y02T50/671 , Y02T50/675
Abstract: A hybrid diffuser case for a gas turbine engine includes an outer diffuser case wall that extends downstream from an annular outer pre-diffuser case shroud. An inner diffuser case wall extends downstream from an annular inner pre-diffuser case shroud. A multiple of struts extend between the annular outer pre-diffuser case shroud and the annular inner pre-diffuser case shroud.
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Patent Agency Ranking
公开(公告)号：US10036503B2
公开(公告)日：2018-07-31
申请号：US14685118
申请日：2015-04-13
Applicant: United Technologies Corporation
Inventor： Anthony P. Cherolis , Alexander Broulidakis , Matthew A. Hough , Jonathan Lemoine , Christopher Treat
IPC: F16L55/00 , F01D9/06 , F16L21/035
CPC classification number: F16L55/00 , F01D9/065 , F05D2240/58 , F05D2300/43 , F16L21/035
Abstract: Aspects of the disclosure are directed to a tube of an engine of an aircraft configured to transfer a fluid, a boss of the engine, and a shim coupled to at least one of the tube and the boss that is configured to maintain a gap between the tube and the boss when the engine is assembled.
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公开(公告)号：US20160298472A1
公开(公告)日：2016-10-13
申请号：US14685118
申请日：2015-04-13
Applicant: United Technologies Corporation
Inventor： Anthony P. Cherolis , Alexander Broulidakis , Matthew A. Hough , Jonathan Lemoine , Christopher Treat
CPC classification number: F16L55/00 , F01D9/065 , F05D2240/58 , F05D2300/43 , F16L21/035
Abstract: Aspects of the disclosure are directed to a tube of an engine of an aircraft configured to transfer a fluid, a boss of the engine, and a shim coupled to at least one of the tube and the boss that is configured to maintain a gap between the tube and the boss when the engine is assembled.
Abstract translation: 本公开的方面针对被配置为传送流体，发动机的凸台和联接到管和凸起中的至少一个的垫片的飞行器的发动机的管，所述垫被配置为保持间隙 管和发动机组装时的老板。
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公开(公告)号：US20160222827A1
公开(公告)日：2016-08-04
申请号：US14612469
申请日：2015-02-03
Applicant: United Technologies Corporation
Inventor： Joshua Daniel Winn , Alexander Broulidakis , Paul K. Sanchez , Anthony P. Cherolis , Joseph J. Sedor , Christopher Treat
CPC classification number: F01D25/28 , F01D5/02 , F01D9/065 , F01D25/12 , F01D25/162 , F01D25/26 , F02C7/12 , F05D2220/32 , F05D2220/3213 , F05D2240/24 , F05D2260/20 , F05D2260/31 , Y02T50/676
Abstract: A fastener assembly includes a first component that includes a bushing opening. A second component includes a fastener opening. A threaded bushing is at least partially located within the bushing opening. A fastener extends through the fastener opening and engages the bushing.
Abstract translation: 紧固件组件包括包括衬套开口的第一部件。 第二部件包括紧固件开口。 螺纹衬套至少部分地位于衬套开口内。 紧固件延伸穿过紧固件开口并接合衬套。
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公开(公告)号：US20160195275A1
公开(公告)日：2016-07-07
申请号：US14911158
申请日：2014-08-29
Applicant: United Technologies Corporation
Inventor： Christopher B. Lyons , Alexander W. Williams , Alexander Broulidakis
CPC classification number: F23R3/60 , F01D9/041 , F01D25/162 , F01D25/24 , F01D25/243 , F02C3/14 , F02C7/20 , F04D29/54 , F04D29/542 , F23R3/04 , Y02T50/671 , Y02T50/675
Abstract: A hybrid diffuser case for a gas turbine engine includes an outer diffuser case wall that extends downstream from an annular outer pre-diffuser case shroud. An inner diffuser case wall extends downstream from an annular inner pre-diffuser case shroud. A multiple of struts extend between the annular outer pre-diffuser case shroud and the annular inner pre-diffuser case shroud.
Abstract translation: 用于燃气涡轮发动机的混合式扩散器壳体包括从环形外部预扩散器壳体护罩的下游延伸的外部扩散器壳体壁。 内部扩散器壳壁从环形内部预扩散器壳体护罩的下游延伸。 多个支柱在环形外部预扩散器壳体护罩和环形内部预扩散器壳体护罩之间延伸。
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公开(公告)号：US20160186997A1
公开(公告)日：2016-06-30
申请号：US14909226
申请日：2014-07-22
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Andreas Sadil , Jonathan M. Jause , Alexander Broulidakis
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.
Abstract translation: 涡轮发动机包括压缩机部分，与压缩机部分流体连通的燃烧器以及与燃烧器部分流体连通的涡轮部分。 燃烧器包括由燃烧器区域内的至少一个隔板和至少一个隔热板限定的燃烧器区域。 至少一个热屏蔽板通过至少一个冷却紧固件连接到隔板面板。
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