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公开(公告)号：US20170241842A1
公开(公告)日：2017-08-24
申请号：US15588890
申请日：2017-05-08
Applicant: Rosemount Aerospace Inc.
Inventor： Matthew J. T. Gmach , Robert E. Sable , John T. Otto , Scott Wigen
CPC classification number: G01K1/22 , G01K13/00 , G01K13/028
Abstract: A temperature sensor includes a sensor body and a wedge extension. The sensor body extends from a sensor base to an opposed sensor tip along a longitudinal axis. The sensor body has a leading edge and opposed trailing edge. The sensor body also has an interior flow passage with an inlet for fluid communication of fluid into the interior flow passage and an outlet for exhausting fluid out from the interior flow passage. The wedge extension is on the sensor body between the sensor tip and the sensor base on the leading edge of the sensor body.
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Patent Agency Ranking
公开(公告)号：US09689755B2
公开(公告)日：2017-06-27
申请号：US14191800
申请日：2014-02-27
Applicant: Rosemount Aerospace Inc.
Inventor： Matthew J. T. Gmach , Robert E. Sable , John T. Otto , Scott Wigen
CPC classification number: G01K1/22 , G01K13/00 , G01K13/028
Abstract: A temperature sensor includes a sensor body and a wedge extension. The sensor body extends from a sensor base to an opposed sensor tip along a longitudinal axis. The sensor body has a leading edge and opposed trailing edge. The sensor body also has an interior flow passage with an inlet for fluid communication of fluid into the interior flow passage and an outlet for exhausting fluid out from the interior flow passage. The wedge extension is on the sensor body between the sensor tip and the sensor base on the leading edge of the sensor body.
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公开(公告)号：US09488534B2
公开(公告)日：2016-11-08
申请号：US14189885
申请日：2014-02-25
Applicant: Rosemount Aerospace Inc.
Inventor： Scott Wigen , Matthew J. T. Gmach , Robert E. Sable , John T. Otto
CPC classification number: G01K13/028
Abstract: A total air temperature sensor includes a supercritical airfoil body extending from an airfoil base to an opposed airfoil tip along a longitudinal axis. The supercritical airfoil body defines an interior flow passage with an inlet for fluid communication of fluid into the interior flow passage and an outlet for exhausting fluid out from the interior flow passage. A temperature probe is mounted within the interior flow passage for measuring temperature of flow through the interior flow passage to determine total air temperature.
Abstract translation: 总空气温度传感器包括超临界翼型体，其从翼型基部沿着纵向轴线延伸到相对的翼型端头。 超临界翼型体限定了内部流动通道，其具有用于使流体流体连通到内部流动通道中的入口和用于从内部流动通道排出流体的出口。 温度探针安装在内部流动通道内，用于测量通过内部流动通道的流动的温度，以确定总的空气温度。
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公开(公告)号：US20150110154A1
公开(公告)日：2015-04-23
申请号：US14191800
申请日：2014-02-27
Applicant: Rosemount Aerospace Inc.
Inventor： Matthew J. T. Gmach , Robert E. Sable , John T. Otto , Scott Wigen
IPC: G01K13/00
CPC classification number: G01K1/22 , G01K13/00 , G01K13/028
Abstract: A temperature sensor includes a sensor body and a wedge extension. The sensor body extends from a sensor base to an opposed sensor tip along a longitudinal axis. The sensor body has a leading edge and opposed trailing edge. The sensor body also has an interior flow passage with an inlet for fluid communication of fluid into the interior flow passage and an outlet for exhausting fluid out from the interior flow passage. The wedge extension is on the sensor body between the sensor tip and the sensor base on the leading edge of the sensor body.
Abstract translation: 温度传感器包括传感器主体和楔形延伸部。 传感器主体沿着纵向轴线从传感器基座延伸到相对的传感器尖端。 传感器主体具有前缘和相对的后缘。 传感器体还具有内部流动通道，其具有用于将流体流体连通到内部流动通道中的入口和用于从内部流动通道排出流体的出口。 楔形延伸部位于传感器顶端与传感器主体前缘的传感器底座之间的传感器本体上。
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公开(公告)号：US10006813B2
公开(公告)日：2018-06-26
申请号：US15588890
申请日：2017-05-08
Applicant: Rosemount Aerospace Inc.
Inventor： Matthew J. T. Gmach , Robert E. Sable , John T. Otto , Scott Wigen
CPC classification number: G01K1/22 , G01K13/00 , G01K13/028
Abstract: A temperature sensor includes a sensor body and a wedge extension. The sensor body extends from a sensor base to an opposed sensor tip along a longitudinal axis. The sensor body has a leading edge and opposed trailing edge. The sensor body also has an interior flow passage with an inlet for fluid communication of fluid into the interior flow passage and an outlet for exhausting fluid out from the interior flow passage. The wedge extension is on the sensor body between the sensor tip and the sensor base on the leading edge of the sensor body.
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公开(公告)号：US20150063414A1
公开(公告)日：2015-03-05
申请号：US14189885
申请日：2014-02-25
Applicant: Rosemount Aerospace Inc.
Inventor： Scott Wigen , Matthew J.T. Gmach , Robert E. Sable , John T. Otto
IPC: G01K13/02
CPC classification number: G01K13/028
Abstract: A total air temperature sensor includes a supercritical airfoil body extending from an airfoil base to an opposed airfoil tip along a longitudinal axis. The supercritical airfoil body defines an interior flow passage with an inlet for fluid communication of fluid into the interior flow passage and an outlet for exhausting fluid out from the interior flow passage. A temperature probe is mounted within the interior flow passage for measuring temperature of flow through the interior flow passage to determine total air temperature.
Abstract translation: 总空气温度传感器包括超临界翼型体，其从翼型基部沿着纵向轴线延伸到相对的翼型端头。 超临界翼型体限定了内部流动通道，其具有用于使流体流体连通到内部流动通道中的入口和用于从内部流动通道排出流体的出口。 温度探针安装在内部流动通道内，用于测量通过内部流动通道的流动的温度，以确定总的空气温度。
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