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 PDF

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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
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Canada
Prior art keywords
drive shaft
torque
tail rotor
rotor drive
measuring
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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
Application number
CA2802172A
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English (en)
Other versions
CA2802172C (fr
Inventor
Joseph W. Wendelsdorf
Keith Hale
Walter West Riley
Charles Eric Covington
Brian E. Tucker
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Bell Helicopter Textron Inc
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Bell Helicopter Textron Inc
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Publication date
Priority claimed from US13/722,005 external-priority patent/US8909453B2/en
Application filed by Bell Helicopter Textron Inc filed Critical Bell Helicopter Textron Inc
Publication of CA2802172A1 publication Critical patent/CA2802172A1/fr
Application granted granted Critical
Publication of CA2802172C publication Critical patent/CA2802172C/fr
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  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
  • Force Measurement Appropriate To Specific Purposes (AREA)
CA2802172A 2012-01-12 2013-01-10 Methode de mesure et de monitorage du couple dans un systeme d'entrainement de giravion Active CA2802172C (fr)

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

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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

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CA (1) CA2802172C (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
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

Cited By (5)

* Cited by examiner, † Cited by third party
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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