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公开(公告)号：US20150345330A1
公开(公告)日：2015-12-03
申请号：US14655833
申请日：2013-12-19
CPC分类号： F01D25/145 , F01D25/162 , F01D25/24 , F05D2220/32 , F05D2230/232 , F05D2230/60 , F05D2240/15 , F05D2260/231 , Y10T29/49321
摘要： An assembly for a gas turbine engine includes a first casing, a fairing, and a multi-piece heat shield assembly. The fairing is disposed adjacent the first casing. The multi-piece heat shield assembly includes a first shield mounted to the first casing and extending between the first casing and the fairing, and a second shield mounted to the fairing and extending between the fairing and the first casing.
摘要翻译： 用于燃气涡轮发动机的组件包括第一壳体，整流罩和多件式隔热罩组件。 整流罩邻近第一壳体设置。 多件式隔热罩组件包括安装到第一壳体并在第一壳体和整流罩之间延伸的第一屏蔽件，以及安装到整流罩并在整流罩和第一壳体之间延伸的第二屏蔽件。
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公开(公告)号：US10294819B2
公开(公告)日：2019-05-21
申请号：US14655833
申请日：2013-12-19
摘要： An assembly for a gas turbine engine includes a first casing, a fairing, and a multi-piece heat shield assembly. The fairing is disposed adjacent the first casing. The multi-piece heat shield assembly includes a first shield mounted to the first casing and extending between the first casing and the fairing, and a second shield mounted to the fairing and extending between the fairing and the first casing.
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公开(公告)号：US20190249568A1
公开(公告)日：2019-08-15
申请号：US16389193
申请日：2019-04-19
CPC分类号： F01D25/145 , F01D25/162 , F01D25/24 , F05D2220/32 , F05D2230/232 , F05D2230/60 , F05D2240/15 , F05D2260/231 , Y10T29/49321
摘要： An assembly for a gas turbine engine includes a first casing, a second casing, and struts extending from the first casing to support the second casing. The assembly further includes a fairing and a multi-piece heat shield assembly. The fairing is disposed between the first casing and the second casing and around each of the struts. The multi-piece heat shield assembly includes a first shield extending between the first casing and the fairing, and a second shield extending between the fairing and the first casing. The multi-piece heat shield assembly further includes a third shield extending between the fairing and the second casing, and fourth and fifth heat shields extending from the third heat shield between the fairing and each of the struts.
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公开(公告)号：US10941674B2
公开(公告)日：2021-03-09
申请号：US16389193
申请日：2019-04-19
摘要： An assembly for a gas turbine engine includes a first casing, a second casing, and struts extending from the first casing to support the second casing. The assembly further includes a fairing and a multi-piece heat shield assembly. The fairing is disposed between the first casing and the second casing and around each of the struts. The multi-piece heat shield assembly includes a first shield extending between the first casing and the fairing, and a second shield extending between the fairing and the first casing. The multi-piece heat shield assembly further includes a third shield extending between the fairing and the second casing, and fourth and fifth heat shields extending from the third heat shield between the fairing and each of the struts.
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5.发明授权公开(公告)号：US10436447B2
公开(公告)日：2019-10-08
申请号：US15224935
申请日：2016-08-01
发明人： Javier N. Johnson , Chris Bates , Eric Beach , Jorge I. Farah
摘要： An augmentor vane assembly of a gas turbine engine with an additively manufactured augmentor vane, the additively manufactured augmentor vane having a vane wall with integral longitudinal wall passages formed therein, at least one of the integral longitudinal wall passages including at least one entrance aperture and at least one exit aperture, the at least one exit aperture transverse to the integral longitudinal wall passage.
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公开(公告)号：US20180030842A1
公开(公告)日：2018-02-01
申请号：US15292835
申请日：2016-10-13
发明人： Javier N. Johnson , Chris Bates , Eric Beach , Jorge I. Farah , Caleb N. Cross
CPC分类号： F01D9/041 , B22F3/1055 , B22F5/00 , B22F5/009 , B22F5/04 , B33Y10/00 , F01D9/065 , F02C7/222 , F02K3/10 , F05D2220/323 , F05D2230/22 , F05D2230/31 , F05D2260/20 , F23R3/20
摘要： An aerospace component includes an augmentor vane and a fuel line additively manufactured within the augmentor vane. A method of manufacture including additively manufacturing an augmentor vane wall that forms an internal volume therein; and additively manufacturing a fuel line within the augmentor vane and extends through the internal volume.
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公开(公告)号：US10337341B2
公开(公告)日：2019-07-02
申请号：US15292835
申请日：2016-10-13
发明人： Javier N. Johnson , Chris Bates , Eric Beach , Jorge I. Farah , Caleb N. Cross
摘要： An augmentor vane assembly includes an additively manufactured augmentor vane and a fuel line additively manufactured within the augmentor vane. A method of manufacture including additively manufacturing an augmentor vane having a wall that forms an internal volume therein; and additively manufacturing a fuel line within the augmentor vane that extends through the internal volume.
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公开(公告)号：US20180031241A1
公开(公告)日：2018-02-01
申请号：US15224935
申请日：2016-08-01
发明人： Javier N. Johnson , Chris Bates , Eric Beach , Jorge I. Farah
CPC分类号： F23R3/20 , B33Y10/00 , B33Y80/00 , F01D5/185 , F01D9/041 , F01D9/06 , F02K3/10 , F05D2220/32 , F05D2230/12 , F05D2230/20 , F05D2230/22 , F05D2230/31 , F05D2230/53 , F05D2240/12 , F05D2260/20 , F05D2260/232 , F05D2300/17 , F23R3/286
摘要： An aerospace component includes a wall with an integral longitudinal wall passage formed therein, the integral longitudinal wall passage including at least one entrance apertures and at least one exit aperture, the exit aperture transverse to the integral longitudinal wall passage. The aerospace component may be additively manufactured.
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