CA2802172A1 - Methode de mesure et de monitorage du couple dans un systeme d'entrainement de giravion - Google Patents
Methode de mesure et de monitorage du couple dans un systeme d'entrainement de giravion Download PDFInfo
- Publication number
- CA2802172A1 CA2802172A1 CA2802172A CA2802172A CA2802172A1 CA 2802172 A1 CA2802172 A1 CA 2802172A1 CA 2802172 A CA2802172 A CA 2802172A CA 2802172 A CA2802172 A CA 2802172A CA 2802172 A1 CA2802172 A1 CA 2802172A1
- Authority
- CA
- Canada
- Prior art keywords
- drive shaft
- torque
- tail rotor
- rotor drive
- measuring
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
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- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
- Force Measurement Appropriate To Specific Purposes (AREA)
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201261585983P | 2012-01-12 | 2012-01-12 | |
US61/585,983 | 2012-01-12 | ||
US13/722,005 | 2012-12-20 | ||
US13/722,005 US8909453B2 (en) | 2012-01-12 | 2012-12-20 | System and method of measuring and monitoring torque in a rotorcraft drive system |
Publications (2)
Publication Number | Publication Date |
---|---|
CA2802172A1 true CA2802172A1 (fr) | 2013-07-12 |
CA2802172C CA2802172C (fr) | 2016-05-31 |
Family
ID=47501010
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA2802172A Active CA2802172C (fr) | 2012-01-12 | 2013-01-10 | Methode de mesure et de monitorage du couple dans un systeme d'entrainement de giravion |
Country Status (1)
Country | Link |
---|---|
CA (1) | CA2802172C (fr) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109141859A (zh) * | 2018-09-28 | 2019-01-04 | 南京航空航天大学 | 一种直升机环量尾梁实验测试装置 |
CN109625320A (zh) * | 2018-12-28 | 2019-04-16 | 中国兵器工业计算机应用技术研究所 | 一种旋翼传动系统的磨合测试及扭矩测试装置、方法 |
CN110589019A (zh) * | 2019-09-09 | 2019-12-20 | 中国航空工业集团公司北京长城航空测控技术研究所 | 一种起落架高速收放试验的力加载方法及加载装置 |
-
2013
- 2013-01-10 CA CA2802172A patent/CA2802172C/fr active Active
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109141859A (zh) * | 2018-09-28 | 2019-01-04 | 南京航空航天大学 | 一种直升机环量尾梁实验测试装置 |
CN109625320A (zh) * | 2018-12-28 | 2019-04-16 | 中国兵器工业计算机应用技术研究所 | 一种旋翼传动系统的磨合测试及扭矩测试装置、方法 |
CN109625320B (zh) * | 2018-12-28 | 2022-04-05 | 中国兵器工业计算机应用技术研究所 | 一种旋翼传动系统的磨合测试及扭矩测试装置、方法 |
CN110589019A (zh) * | 2019-09-09 | 2019-12-20 | 中国航空工业集团公司北京长城航空测控技术研究所 | 一种起落架高速收放试验的力加载方法及加载装置 |
CN110589019B (zh) * | 2019-09-09 | 2021-07-13 | 中国航空工业集团公司北京长城航空测控技术研究所 | 一种起落架高速收放试验的力加载方法及加载装置 |
Also Published As
Publication number | Publication date |
---|---|
CA2802172C (fr) | 2016-05-31 |
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