CN102501970A - 一种板式阻尼器及其制备方法 - Google Patents
一种板式阻尼器及其制备方法 Download PDFInfo
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- CN102501970A CN102501970A CN2011103621626A CN201110362162A CN102501970A CN 102501970 A CN102501970 A CN 102501970A CN 2011103621626 A CN2011103621626 A CN 2011103621626A CN 201110362162 A CN201110362162 A CN 201110362162A CN 102501970 A CN102501970 A CN 102501970A
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CN201110362162.6A CN102501970B (zh) | 2011-11-15 | 2011-11-15 | 一种板式阻尼器及其制备方法 |
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CN201110362162.6A CN102501970B (zh) | 2011-11-15 | 2011-11-15 | 一种板式阻尼器及其制备方法 |
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CN102501970A true CN102501970A (zh) | 2012-06-20 |
CN102501970B CN102501970B (zh) | 2014-12-24 |
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Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104334914A (zh) * | 2012-06-27 | 2015-02-04 | 波音公司 | 阻尼机械联动机构 |
WO2016033412A1 (en) * | 2014-08-29 | 2016-03-03 | Aktiebolaget Skf | Elastomer having tear reducing contoured edges |
EP3130537A1 (fr) | 2015-08-14 | 2017-02-15 | Airbus Helicopters | Dispositif d'amortissement, et aeronef |
CN106965927A (zh) * | 2015-11-11 | 2017-07-21 | 瑞士玛瑞恩克直升机公司 | 用于旋翼飞机的旋翼头的旋翼叶片联接装置 |
CN109592024A (zh) * | 2016-07-05 | 2019-04-09 | 金福珍 | 一种智能无人机 |
EP3575629A1 (fr) | 2018-05-31 | 2019-12-04 | Airbus Helicopters | Amortisseur hydroelastique, et aeronef |
FR3090777A1 (fr) | 2018-12-19 | 2020-06-26 | Airbus Helicopters | Amortisseur hydroelastique, rotor comportant un tel amortisseur hydroelastique et aeronef associe |
US10759529B2 (en) | 2015-11-11 | 2020-09-01 | Kopter Group Ag | Rotor blade coupling device of a rotor head for a rotorcraft |
US11161601B2 (en) | 2018-03-30 | 2021-11-02 | Airbus Helicopters | Hydro-elastic damper and an aircraft |
US12060148B2 (en) | 2022-08-16 | 2024-08-13 | Honeywell International Inc. | Ground resonance detection and warning system and method |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB787848A (en) * | 1954-10-26 | 1957-12-18 | Saunders Roe Ltd | Improvements in vibration dampers |
US7360994B2 (en) * | 2004-03-03 | 2008-04-22 | Eurocopter | Method of controlling vibration damping in a helicopter, and apparatus implementing the method |
CN102009745A (zh) * | 2010-11-19 | 2011-04-13 | 中国航空工业集团公司北京航空材料研究院 | 一种直升机旋翼板式阻尼器 |
CN202358301U (zh) * | 2011-11-15 | 2012-08-01 | 中国航空工业集团公司北京航空材料研究院 | 一种板式阻尼器 |
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2011
- 2011-11-15 CN CN201110362162.6A patent/CN102501970B/zh active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB787848A (en) * | 1954-10-26 | 1957-12-18 | Saunders Roe Ltd | Improvements in vibration dampers |
US7360994B2 (en) * | 2004-03-03 | 2008-04-22 | Eurocopter | Method of controlling vibration damping in a helicopter, and apparatus implementing the method |
CN102009745A (zh) * | 2010-11-19 | 2011-04-13 | 中国航空工业集团公司北京航空材料研究院 | 一种直升机旋翼板式阻尼器 |
CN202358301U (zh) * | 2011-11-15 | 2012-08-01 | 中国航空工业集团公司北京航空材料研究院 | 一种板式阻尼器 |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104334914A (zh) * | 2012-06-27 | 2015-02-04 | 波音公司 | 阻尼机械联动机构 |
CN104334914B (zh) * | 2012-06-27 | 2016-07-20 | 波音公司 | 阻尼机械联动机构 |
WO2016033412A1 (en) * | 2014-08-29 | 2016-03-03 | Aktiebolaget Skf | Elastomer having tear reducing contoured edges |
US10479493B2 (en) | 2015-08-14 | 2019-11-19 | Airbus Helicopters | Damper device and an aircraft |
EP3130537A1 (fr) | 2015-08-14 | 2017-02-15 | Airbus Helicopters | Dispositif d'amortissement, et aeronef |
CN106965927A (zh) * | 2015-11-11 | 2017-07-21 | 瑞士玛瑞恩克直升机公司 | 用于旋翼飞机的旋翼头的旋翼叶片联接装置 |
US10759529B2 (en) | 2015-11-11 | 2020-09-01 | Kopter Group Ag | Rotor blade coupling device of a rotor head for a rotorcraft |
CN109592024A (zh) * | 2016-07-05 | 2019-04-09 | 金福珍 | 一种智能无人机 |
US11161601B2 (en) | 2018-03-30 | 2021-11-02 | Airbus Helicopters | Hydro-elastic damper and an aircraft |
EP3575629A1 (fr) | 2018-05-31 | 2019-12-04 | Airbus Helicopters | Amortisseur hydroelastique, et aeronef |
US11518503B2 (en) | 2018-05-31 | 2022-12-06 | Airbus Helicopters | Hydroelastic damper, and an aircraft |
FR3090777A1 (fr) | 2018-12-19 | 2020-06-26 | Airbus Helicopters | Amortisseur hydroelastique, rotor comportant un tel amortisseur hydroelastique et aeronef associe |
EP3680510A1 (fr) | 2018-12-19 | 2020-07-15 | Airbus Helicopters | Amortisseur hydroélastique, rotor comportant un tel amortisseur hydroélastique et aéronef associé |
US12060148B2 (en) | 2022-08-16 | 2024-08-13 | Honeywell International Inc. | Ground resonance detection and warning system and method |
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Publication number | Publication date |
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CN102501970B (zh) | 2014-12-24 |
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Address after: No. 5 Yongxiang North Road, Haidian District, Beijing 100094 Patentee after: Beijing Aviation Materials Research Institute Co.,Ltd. Address before: No. 5 Yongxiang North Road, Haidian District, Beijing 100094 Patentee before: Beijing Aeronautical Materials Research Institute Co.,Ltd. |
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