JP2014119451A - 乗り物用の大気温度センサ配設および大気温度を測定する方法 - Google Patents
乗り物用の大気温度センサ配設および大気温度を測定する方法 Download PDFInfo
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- JP2014119451A JP2014119451A JP2013255522A JP2013255522A JP2014119451A JP 2014119451 A JP2014119451 A JP 2014119451A JP 2013255522 A JP2013255522 A JP 2013255522A JP 2013255522 A JP2013255522 A JP 2013255522A JP 2014119451 A JP2014119451 A JP 2014119451A
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- temperature sensor
- inlet
- vehicle
- sensor arrangement
- atmospheric temperature
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
- G01K13/00—Thermometers specially adapted for specific purposes
- G01K13/02—Thermometers specially adapted for specific purposes for measuring temperature of moving fluids or granular materials capable of flow
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
- G01K13/00—Thermometers specially adapted for specific purposes
- G01K13/02—Thermometers specially adapted for specific purposes for measuring temperature of moving fluids or granular materials capable of flow
- G01K13/028—Thermometers specially adapted for specific purposes for measuring temperature of moving fluids or granular materials capable of flow for use in total air temperature [TAT] probes
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Measuring Temperature Or Quantity Of Heat (AREA)
Abstract
【解決手段】 乗り物用の大気温度センサ配設は、ベース部分、入口、および出口を有する温度センサ筐体を含む。粒子状物質を入口気流から分離するために入口から出口まで延在する、連続的に曲線を成す壁によって画定される主流路も含まれる。温度センサ筐体の内部空洞内に配置される温度センサもさらに含まれる。
【選択図】 図3
Description
32…大気温度センサ筐体
34…ベース部分
38…主流
40…入口気流
42…粒子状物質
44…主流路
46…空洞入口
48…空洞
50…温度センサ
52…出口
54…連続的に曲線を成す壁
56…軸
Claims (15)
- 乗り物用の大気温度センサ配設であって、
ベース部分、入口、および出口を有する温度センサ筐体と、
粒子状物質を入口気流から分離するために前記入口から前記出口まで延在する、連続的に曲線を成す壁によって画定される主流路と、
前記温度センサ筐体の内部空洞内に配置される温度センサと、
を備えた、大気温度センサ配設。 - 前記入口は、円形断面を備える、請求項1に記載の大気温度センサ配設。
- 前記入口は、楕円形断面を備える、請求項1に記載の大気温度センサ配設。
- 前記入口は、第1の断面積を備え、前記出口は、第2の断面積を備え、前記第1の断面積は、前記第2の断面積よりも大きい、請求項1に記載の大気温度センサ配設。
- 前記ベース部分は、前記乗り物に固定される、請求項1に記載の大気温度センサ配設。
- 前記乗り物は、航空機である、請求項1に記載の大気温度センサ配設。
- 前記主流路は、前記入口に近接して実質的に対称である、請求項1に記載の大気温度センサ配設。
- 分離された前記粒子状物質は、水、氷、および粉塵のうちの少なくとも1つを含む、請求項1に記載の大気温度センサ配設。
- 前記空洞は、円形断面を有する、請求項1に記載の大気温度センサ配設。
- 乗り物に近接した大気温度を測定するための方法であって、
主流を吸い込んで温度センサ筐体の入口に入れることと、
連続的に曲線を成す壁によって画定される主流路を通して前記主流を流すことと、
前記主流が前記主流路を通過するときに、粒子状物質を入口気流から分離することと、
前記粒子状物質を前記温度センサ筐体から出口を通して排出することと、
前記温度センサ筐体の内部位置の空洞内に配置される温度センサを用いて前記入口気流の温度を測定することと、
を備えた、方法。 - 前記入口気流を前記空洞に送ることをさらに備えた、請求項10に記載の方法。
- 前記入口と前記出口との間の前記主流路に沿って配置される空洞入口を介して、前記入口気流を前記空洞に送ることをさらに備えた、請求項11に記載の方法。
- 前記温度センサ筐体を前記乗り物に固定することをさらに備えた、請求項10に記載の方法。
- 前記乗り物は、航空機である、請求項13に記載の方法。
- 前記粒子状物質は、水、氷、および粉塵のうちの少なくとも1つを備えた、請求項10に記載の方法。
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/713,661 US9829395B2 (en) | 2012-12-13 | 2012-12-13 | Air temperature sensor arrangement for a vehicle and method of measuring air temperature |
US13/713,661 | 2012-12-13 |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2014119451A true JP2014119451A (ja) | 2014-06-30 |
JP6218585B2 JP6218585B2 (ja) | 2017-10-25 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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JP2013255522A Active JP6218585B2 (ja) | 2012-12-13 | 2013-12-11 | 乗り物用の大気温度センサ配設および大気温度を測定する方法 |
Country Status (6)
Country | Link |
---|---|
US (1) | US9829395B2 (ja) |
EP (1) | EP2743660B1 (ja) |
JP (1) | JP6218585B2 (ja) |
CN (1) | CN103884452B (ja) |
BR (1) | BR102013032063A2 (ja) |
CA (1) | CA2836171C (ja) |
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ES2837851T3 (es) * | 2014-04-11 | 2021-07-01 | Bundesrepublik Deutschland Vertreten Durch Das Bmvi Dieses Vertreten Durch Den Deutschen Wetterdiens | Aparato de medición de vapor de agua |
US20160238456A1 (en) * | 2015-02-12 | 2016-08-18 | Rosemount Aerospace Inc. | Air temperature sensor and fabrication |
CA2944106A1 (en) | 2015-12-10 | 2017-06-10 | Rosemount Aerospace Inc. | Air data probe with elliptical cross section |
CN105841841A (zh) * | 2016-04-07 | 2016-08-10 | 中国航空工业集团公司西安飞机设计研究所 | 一种飞机表面温度检测系统 |
US10422702B2 (en) * | 2017-06-08 | 2019-09-24 | Rosemount Aerospace Inc. | Total air temperature probe with reduced icing sensor flow passage geometry |
US10852203B2 (en) | 2018-06-15 | 2020-12-01 | Rosemount Aerospace Inc. | Total air temperature probe with concave flow path transitions to outlet |
US11125770B2 (en) * | 2018-12-06 | 2021-09-21 | Rosemount Aerospace Inc. | Acoustic air data sensor and system |
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2013
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- 2013-12-11 JP JP2013255522A patent/JP6218585B2/ja active Active
- 2013-12-12 BR BR102013032063A patent/BR102013032063A2/pt not_active Application Discontinuation
- 2013-12-13 CN CN201310684173.5A patent/CN103884452B/zh active Active
- 2013-12-13 EP EP13197137.6A patent/EP2743660B1/en active Active
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Also Published As
Publication number | Publication date |
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CA2836171C (en) | 2021-07-27 |
US20140169401A1 (en) | 2014-06-19 |
EP2743660B1 (en) | 2016-09-28 |
JP6218585B2 (ja) | 2017-10-25 |
US9829395B2 (en) | 2017-11-28 |
CN103884452B (zh) | 2020-04-14 |
CA2836171A1 (en) | 2014-06-13 |
CN103884452A (zh) | 2014-06-25 |
BR102013032063A2 (pt) | 2015-12-08 |
EP2743660A1 (en) | 2014-06-18 |
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