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公开(公告)号：US11466700B2
公开(公告)日：2022-10-11
申请号：US15445240
申请日：2017-02-28
摘要： A turbine engine for an aircraft can includes a casing. The casing can be a fan casing surrounding a fan assembly for drawing air into the turbine engine. The fan casing can have a peripheral wall. A surface cooler can be provided in the turbine engine confronting the peripheral wall of the fan casing. The surface cooler can have a mounting bracket for mounting the surface cooler to the fan casing.
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公开(公告)号：US10393147B2
公开(公告)日：2019-08-27
申请号：US14807046
申请日：2015-07-23
IPC分类号： F04D29/58 , F28F9/007 , F01D25/28 , B64D29/00 , F02C7/04 , F02C7/32 , F04D29/60 , B64D33/02 , F02K3/06 , F02C7/14 , F04D19/00 , F04D29/02 , F04D29/40 , F04D29/66 , B64D33/08
摘要： A fan casing assembly for a turbine engine including a fan casing having a peripheral wall, a surface cooler having a first surface confronting the peripheral wall and forward and aft projections, which are radially spaced from the first surface and located between the peripheral wall and the first surface, and a mounting bracket to mount the surface cooler to the fan casing and a method of mounting a surface cooler to a fan casing of a turbine engine.
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公开(公告)号：US20180238238A1
公开(公告)日：2018-08-23
申请号：US15440551
申请日：2017-02-23
CPC分类号： F02C7/18 , B21D53/022 , F02K3/06 , F02K3/115 , F05D2220/323 , F05D2230/10 , F05D2260/22141 , F05D2260/232 , F05D2300/173 , F28D1/06 , F28D2021/0026 , F28F1/16 , F28F1/26 , F28F2255/00 , Y02T50/676
摘要： A method of forming fins in a heat exchanger includes using a stacked slit saw with multiple saw blades to simultaneously cut multiple fins into a metal body of the heat exchanger, with each fin having a body extending from an upper surface of the metal body and terminating in a tip.
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4.发明申请公开(公告)号：US20170023017A1
公开(公告)日：2017-01-26
申请号：US14807046
申请日：2015-07-23
CPC分类号： F04D29/582 , B64D29/00 , B64D33/02 , B64D33/08 , B64D2033/024 , F01D25/28 , F02C7/04 , F02C7/14 , F02C7/32 , F02K3/06 , F04D19/002 , F04D29/02 , F04D29/403 , F04D29/60 , F04D29/661 , F05D2260/213 , F28F9/007 , F28F9/0075 , Y02T50/676
摘要： A fan casing assembly for a turbine engine including a fan casing having a peripheral wall, a surface cooler having a first surface confronting the peripheral wall and forward and aft projections, which are radially spaced from the first surface and located between the peripheral wall and the first surface, and a mounting bracket to mount the surface cooler to the fan casing and a method of mounting a surface cooler to a fan casing of a turbine engine.
摘要翻译： 一种用于涡轮发动机的风扇壳体组件，其包括具有周壁的风扇壳体，表面冷却器，其具有面向周壁的第一表面和与第一表面径向间隔开并位于周壁和 第一表面和用于将表面冷却器安装到风扇壳体的安装支架以及将表面冷却器安装到涡轮发动机的风扇壳体的方法。
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公开(公告)号：US11143105B2
公开(公告)日：2021-10-12
申请号：US16225063
申请日：2018-12-19
摘要： A fan casing assembly for a turbine engine including a fan casing having a peripheral wall, a surface cooler having a first surface confronting the peripheral wall and a mounting assembly having a lower portion generally retained between the first surface of the annular surface cooler and the peripheral wall and having a floating body extending through the set of fan casing fastener openings and an upper portion located radially exterior of the annular fan casing and operably coupled to the lower portion.
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公开(公告)号：US10514005B2
公开(公告)日：2019-12-24
申请号：US15441888
申请日：2017-02-24
发明人： Bernard Albert Luschek , David William Millward , Joseph Richard Schmitt , Daniel Scott McCann , Derek Thomas Dreischarf
摘要： A turbine engine with a casing including opposing surfaces and a manifold opening passing through the surfaces. A surface cooler is provided adjacent one of the surfaces. A cooler manifold passes through the manifold opening. A seal is provided between the surface cooler and the casing. At least one bolt is used to secure the surface cooler to the casing with the seal in between.
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公开(公告)号：US11766747B2
公开(公告)日：2023-09-26
申请号：US17835593
申请日：2022-06-08
IPC分类号： B23P6/00 , F01D25/14 , F01D25/24 , F01D25/28 , B22F5/00 , F02K3/06 , B22F10/25 , B33Y80/00 , B33Y10/00 , B22F10/66
CPC分类号： B23P6/007 , B22F5/009 , B22F10/25 , F01D25/14 , F01D25/24 , F01D25/28 , F02K3/06 , B22F10/66 , B33Y10/00 , B33Y80/00 , F05D2230/22 , F05D2230/31 , F05D2230/80 , F05D2260/213 , F05D2260/22141
摘要： A surface cooler configured to be operably coupled to an aircraft fan casing includes a body having a first surface configured to confront the aircraft fan casing and a second surface opposite the first surface, multiple fluid passages located within the body, and a set of fins located on at least the second surface of the body.
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公开(公告)号：US11377976B2
公开(公告)日：2022-07-05
申请号：US16225096
申请日：2018-12-19
IPC分类号： F01D25/14 , F01D25/24 , F01D25/28 , B22F5/00 , B23P6/00 , F02K3/06 , B22F10/20 , B33Y80/00 , B33Y10/00
摘要： A surface cooler configured to be operably coupled to an aircraft fan casing and having a first surface configured to confront a peripheral wall of an aircraft fan casing and a second surface opposite the first surface, a set of fluid passages internal to the body and a set of fins located on at least a portion of the second surface of the body.
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公开(公告)号：US10428834B2
公开(公告)日：2019-10-01
申请号：US15157648
申请日：2016-05-18
发明人： Derek Thomas Dreischarf , Bernard Albert Luschek , Dennis Alan McQueen , Daniel Scott McCann , Anthony Lynn Lighthill
摘要： A fan casing assembly for a turbine engine including a casing having an annular fan cooler. The annular fan cooler includes first and second connection assemblies to fix movement of the fan cooler during engine operation, while permitting circumferential thermal growth of the fan cooler without suffering from high cycle fatigue.
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公开(公告)号：US20180238640A1
公开(公告)日：2018-08-23
申请号：US15440626
申请日：2017-02-23
CPC分类号： F28F3/048 , F02C7/14 , F04D29/522 , F04D29/526 , F04D29/582 , F05D2230/20 , F05D2260/213 , F05D2260/98 , F28D7/005 , F28D2021/0021 , F28D2021/0026 , F28F1/26 , F28F21/084
摘要： A method of forming fins in a heat exchanger having a metal body by skiving the metal body to form a first fin in a first orientation, and skiving the metal body again to form a second fin in a second orientation while straightening the first fin into a third orientation.
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