CN201107166Y - 直升机桨叶标定装置 - Google Patents
直升机桨叶标定装置 Download PDFInfo
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- CN201107166Y CN201107166Y CNU2007201815984U CN200720181598U CN201107166Y CN 201107166 Y CN201107166 Y CN 201107166Y CN U2007201815984 U CNU2007201815984 U CN U2007201815984U CN 200720181598 U CN200720181598 U CN 200720181598U CN 201107166 Y CN201107166 Y CN 201107166Y
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Application Number | Priority Date | Filing Date | Title |
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CNU2007201815984U CN201107166Y (zh) | 2007-10-19 | 2007-10-19 | 直升机桨叶标定装置 |
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CNU2007201815984U CN201107166Y (zh) | 2007-10-19 | 2007-10-19 | 直升机桨叶标定装置 |
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CN201107166Y true CN201107166Y (zh) | 2008-08-27 |
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CNU2007201815984U Expired - Lifetime CN201107166Y (zh) | 2007-10-19 | 2007-10-19 | 直升机桨叶标定装置 |
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Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102539127A (zh) * | 2010-12-31 | 2012-07-04 | 中国直升机设计研究所 | 一种桨叶标定标准载荷施加装置 |
CN104697766A (zh) * | 2014-08-26 | 2015-06-10 | 中国直升机设计研究所 | 一种双向铰支座装置 |
CN106767373A (zh) * | 2016-11-24 | 2017-05-31 | 兰州飞行控制有限责任公司 | 一种角位移舵机机械传动间隙测量方法 |
CN107014421A (zh) * | 2017-04-19 | 2017-08-04 | 吉林宇恒光电仪器有限责任公司 | 基于双向黑白比的光电编码器码盘不均匀误差检测方法 |
CN108225692A (zh) * | 2017-12-01 | 2018-06-29 | 中国直升机设计研究所 | 一种测量桨叶整体扭转刚度试验方法 |
CN110657917A (zh) * | 2019-09-29 | 2020-01-07 | 中国直升机设计研究所 | 一种无级变角标测装置 |
CN112432746A (zh) * | 2020-10-21 | 2021-03-02 | 中国人民解放军总参谋部第六十研究所 | 一种确定直升机桨叶挥摆载荷耦合程度的方法 |
-
2007
- 2007-10-19 CN CNU2007201815984U patent/CN201107166Y/zh not_active Expired - Lifetime
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102539127A (zh) * | 2010-12-31 | 2012-07-04 | 中国直升机设计研究所 | 一种桨叶标定标准载荷施加装置 |
CN102539127B (zh) * | 2010-12-31 | 2014-10-22 | 中国直升机设计研究所 | 一种桨叶标定标准载荷施加装置 |
CN104697766A (zh) * | 2014-08-26 | 2015-06-10 | 中国直升机设计研究所 | 一种双向铰支座装置 |
CN106767373A (zh) * | 2016-11-24 | 2017-05-31 | 兰州飞行控制有限责任公司 | 一种角位移舵机机械传动间隙测量方法 |
CN107014421A (zh) * | 2017-04-19 | 2017-08-04 | 吉林宇恒光电仪器有限责任公司 | 基于双向黑白比的光电编码器码盘不均匀误差检测方法 |
CN107014421B (zh) * | 2017-04-19 | 2023-04-28 | 吉林宇恒光电仪器有限责任公司 | 基于双向黑白比的光电编码器码盘不均匀误差检测方法 |
CN108225692A (zh) * | 2017-12-01 | 2018-06-29 | 中国直升机设计研究所 | 一种测量桨叶整体扭转刚度试验方法 |
CN110657917A (zh) * | 2019-09-29 | 2020-01-07 | 中国直升机设计研究所 | 一种无级变角标测装置 |
CN112432746A (zh) * | 2020-10-21 | 2021-03-02 | 中国人民解放军总参谋部第六十研究所 | 一种确定直升机桨叶挥摆载荷耦合程度的方法 |
CN112432746B (zh) * | 2020-10-21 | 2022-11-11 | 中国人民解放军总参谋部第六十研究所 | 一种确定直升机桨叶挥摆载荷耦合程度的方法 |
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Legal Events
Date | Code | Title | Description |
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C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
EE01 | Entry into force of recordation of patent licensing contract |
Assignee: China Aviation Science and technology industry Limited by Share Ltd Assignor: China Helicopter Research and Development Institute Contract record no.: 2010110000118 Denomination of utility model: Helicopter paddle calibration apparatus Granted publication date: 20080827 License type: Exclusive License Record date: 20100811 |
|
EE01 | Entry into force of recordation of patent licensing contract |
Assignee: China Aviation Science and technology industry Limited by Share Ltd Assignor: China Helicopter Research and Development Institute Contract record no.: 2010110000118 Denomination of utility model: Helicopter paddle calibration apparatus Granted publication date: 20080827 License type: Exclusive License Record date: 20100811 |
|
LICC | Enforcement, change and cancellation of record of contracts on the licence for exploitation of a patent or utility model | ||
CX01 | Expiry of patent term |
Granted publication date: 20080827 |
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CX01 | Expiry of patent term |