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公开(公告)号：US10690475B2
公开(公告)日：2020-06-23
申请号：US15440946
申请日：2017-02-23
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Eli Cole Warren , Joon K. Kim
IPC: G01B7/14 , F04D29/52 , F04D29/00 , F04D27/00 , F01D17/04 , F01D17/06 , F01D21/00 , F01D17/08 , F01D17/02
Abstract: Disclosed is a probe including a housing; a plurality of axially stacked caps disposed within the housing, the plurality of stacked caps including an inner cap and an outer cap, a probe sensor fixedly disposed between the inner cap and an axial bottom of the housing, and an electronic lead connected to the probe sensor and axially extending through the plurality of caps to an exterior of the probe.
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公开(公告)号：US20200088606A1
公开(公告)日：2020-03-19
申请号：US16132128
申请日：2018-09-14
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Eli Cole Warren , Michael F. Sabol , Alan E. Ingram , Michael J. Saitta , Darren M. Wind , Steven D. Mitchell , Sebastian Martinez , Kevin Andrew Ford , Patrick M. Harrington
Abstract: A low profile un-lensed non-intrusive stress measurement system probe may comprise a housing comprising a first channel and an optical face, a first hypotube disposed within the first channel and coupled at a sensing aperture in the optical face, and a plurality of optical fibers disposed within the first hypotube, wherein the first hypotube executes a bend between 45° and 90° within the housing.
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公开(公告)号：US10429168B2
公开(公告)日：2019-10-01
申请号：US15376021
申请日：2016-12-12
Applicant: United Technologies Corporation
Inventor： Eli Cole Warren
Abstract: A method for installing a probe assembly in a case of a gas turbine engine the method including installing a first portion of the probe assembly within a first section of the case, and installing a second portion of the probe assembly within a second section of the case. A case assembly within a gas turbine engine the case assembly including a case in at least one of a compressor and a turbine, and a probe assembly. The probe assembly including a first portion positioned within a bore of the case, and a second portion positioned within an inset of the case, the bore having a smaller diameter than the inset.
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公开(公告)号：US10317315B2
公开(公告)日：2019-06-11
申请号：US15412572
申请日：2017-01-23
Applicant: United Technologies Corporation
Inventor： Eli Cole Warren , Nicholas R. Leslie
Abstract: A probe assembly for a gas turbine engine is disclosed. The probe assembly may include a probe, and a fastener to retain the probe within a case of the gas turbine engine, the fastener including a sealing arrangement with a heat shield of the gas turbine engine.
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公开(公告)号：US20170160070A1
公开(公告)日：2017-06-08
申请号：US15376021
申请日：2016-12-12
Applicant: United Technologies Corporation
Inventor： Eli Cole Warren
CPC classification number: G01B7/14 , F01D11/20 , F01D17/06 , F01D21/003 , F05D2240/11 , F05D2260/97 , G01D11/30
Abstract: A method for installing a probe assembly in a case of a gas turbine engine is disclosed. The method may include installing a first portion of the probe assembly within a first section of the case, and installing a second portion of the probe assembly within a second section of the case. A case assembly within a gas turbine engine is also disclosed. The case assembly may include a case in at least one of a compressor and a turbine, and a probe assembly. The probe assembly may include a first portion positioned within a bore of the case, and a second portion positioned within an inset of the case, the bore having a smaller diameter than the inset.
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Patent Agency Ranking
公开(公告)号：US09551632B2
公开(公告)日：2017-01-24
申请号：US14107771
申请日：2013-12-16
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Eli Cole Warren , Nicholas R. Leslie
CPC classification number: G01M15/14 , F01D11/20 , F01D17/02 , F01D21/003 , F01D25/24 , F01D25/285 , F05D2220/32 , Y10T29/4932 , Y10T403/3993
Abstract: A probe assembly for a gas turbine engine is disclosed. The probe assembly may include a probe, and a fastener to retain the probe within a case of the gas turbine engine, the fastener including a sealing arrangement with a heat shield of the gas turbine engine.
Abstract translation: 公开了一种用于燃气涡轮发动机的探针组件。 探针组件可以包括探针和将探针保持在燃气涡轮发动机的壳体内的紧固件，该紧固件包括具有燃气涡轮发动机的隔热罩的密封装置。
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公开(公告)号：US09518850B2
公开(公告)日：2016-12-13
申请号：US14015191
申请日：2013-08-30
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Eli Cole Warren
CPC classification number: G01B7/14 , F01D11/20 , F01D17/06 , F01D21/003 , F05D2240/11 , F05D2260/97 , G01D11/30
Abstract: A method for installing a probe assembly in a case of a gas turbine engine is disclosed. The method may include installing a first portion of the probe assembly within a first section of the case, and installing a second portion of the probe assembly within a second section of the case. A case assembly within a gas turbine engine is also disclosed. The case assembly may include a case in at least one of a compressor and a turbine, and a probe assembly. The probe assembly may include a first portion positioned within a bore of the case, and a second portion positioned within an inset of the case, the bore having a smaller diameter than the inset.
Abstract translation: 公开了一种用于在燃气涡轮发动机的情况下安装探针组件的方法。 该方法可以包括将探针组件的第一部分安装在壳体的第一部分内，以及将探针组件的第二部分安装在壳体的第二部分内。 还公开了一种燃气涡轮发动机内的壳体组件。 壳体组件可以包括在压缩机和涡轮机中的至少一个以及探头组件中的壳体。 探针组件可以包括定位在壳体的孔内的第一部分和位于壳体的插入件内的第二部分，孔具有比插入物更小的直径。
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公开(公告)号：US09228448B2
公开(公告)日：2016-01-05
申请号：US14480752
申请日：2014-09-09
Applicant: United Technologies Corporation
Inventor： Darren M. Wind , Mark A. Davidson , Eli Cole Warren
CPC classification number: F01D21/003 , F05D2270/80
Abstract: A turbine section according to an exemplary aspect of the present disclosure includes, among other things, an airfoil including an edge and a probe positioned a distance from the airfoil. The probe is configured to detect radiation emitted from a radiation source. A sensor is operatively coupled to the probe and is configured to generate a signal utilized to determine when the edge of the airfoil extends into a line-of-sight between the probe and the radiation source.
Abstract translation: 根据本公开的示例性方面的涡轮机部分包括除了别的以外的翼型件，其包括边缘和位于距离翼型一定距离的探头。 探针被配置为检测从辐射源发射的辐射。 传感器可操作地耦合到探针，并被配置为产生用于确定翼型的边缘何时延伸到探测器和辐射源之间的视线内的信号。
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公开(公告)号：US09181818B2
公开(公告)日：2015-11-10
申请号：US13626099
申请日：2012-09-25
Applicant: United Technologies Corporation
Inventor： Eli Cole Warren
CPC classification number: G01D5/353 , F01D17/02 , F05D2300/50212 , G01D11/30 , Y10T29/49229
Abstract: A disclosed probe assembly includes a sensor member and an outer holder including a main bore for the sensor member, the outer holder including a first coefficient of thermal expansion. The sensor member is held within a sensor bore of an inner holder. The inner holder is held within the main bore of the outer holder by an interference fit. The inner holder includes a second coefficient of thermal expansion greater than the first coefficient of thermal expansion. Expansion of the inner holder is constrained by the outer holder to maintain the sensor member within the probe bore of the inner holder at elevated temperatures.
Abstract translation: 公开的探针组件包括传感器构件和包括用于传感器构件的主孔的外保持器，外保持器包括第一热膨胀系数。 传感器构件保持在内部保持器的传感器孔内。 内保持器通过过盈配合保持在外保持器的主孔内。 内部支架包括大于第一热膨胀系数的第二热膨胀系数。 内部支架的膨胀受到外保持器约束，以将传感器构件保持在内部保持器的探针孔内处于升高的温度。
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公开(公告)号：US20150083919A1
公开(公告)日：2015-03-26
申请号：US14480752
申请日：2014-09-09
Applicant: United Technologies Corporation
Inventor： Darren M. Wind , Mark A. Davidson , Eli Cole Warren
IPC: G01B11/14
CPC classification number: F01D21/003 , F05D2270/80
Abstract: A turbine section according to an exemplary aspect of the present disclosure includes, among other things, an airfoil including an edge and a probe positioned a distance from the airfoil. The probe is configured to detect radiation emitted from a radiation source. A sensor is operatively coupled to the probe and is configured to generate a signal utilized to determine when the edge of the airfoil extends into a line-of-sight between the probe and the radiation source.
Abstract translation: 根据本公开的示例性方面的涡轮机部分包括除了别的以外的翼型件，其包括边缘和位于距离翼型一定距离的探头。 探针被配置为检测从辐射源发射的辐射。 传感器可操作地耦合到探针，并被配置为产生用于确定翼型的边缘何时延伸到探测器和辐射源之间的视线内的信号。
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