CN202836959U - 飞行器尾翼折叠旋转机构测试系统 - Google Patents
飞行器尾翼折叠旋转机构测试系统 Download PDFInfo
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- CN202836959U CN202836959U CN 201220550984 CN201220550984U CN202836959U CN 202836959 U CN202836959 U CN 202836959U CN 201220550984 CN201220550984 CN 201220550984 CN 201220550984 U CN201220550984 U CN 201220550984U CN 202836959 U CN202836959 U CN 202836959U
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Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104819816A (zh) * | 2015-05-13 | 2015-08-05 | 中国飞机强度研究所 | 一种动载荷加载系统及飞机垂尾试验系统及方法 |
CN104897355A (zh) * | 2015-06-23 | 2015-09-09 | 中国航空工业集团公司西安飞机设计研究所 | 一种折叠翼非线性颤振试验装置 |
CN105258933A (zh) * | 2015-11-06 | 2016-01-20 | 航天科工哈尔滨风华有限公司 | 一种折叠舵芯展开试验装置 |
CN106871748A (zh) * | 2017-01-11 | 2017-06-20 | 北京理工大学 | 用于弹体多角度高速旋转条件下测试弹翼展开的旋转台 |
CN106871747A (zh) * | 2017-01-11 | 2017-06-20 | 北京理工大学 | 一种弹体多角度高速旋转条件下测试弹翼展开的装置 |
CN111003204A (zh) * | 2019-12-06 | 2020-04-14 | 江西洪都航空工业集团有限责任公司 | 一种飞机平尾伺服作动机构动刚度测试系统及测试方法 |
CN111994302A (zh) * | 2020-09-08 | 2020-11-27 | 中国电子科技集团公司第四十一研究所 | 一种小型折叠翼无人机一体化地面测试平台及测试方法 |
CN113495002A (zh) * | 2020-04-03 | 2021-10-12 | 中国航发商用航空发动机有限责任公司 | 航空发动机非全环风扇叶片的旋转冲击试验装置 |
CN113848046A (zh) * | 2021-09-08 | 2021-12-28 | 湖南航天机电设备与特种材料研究所 | 用于测试折叠翼飞行器翼面展开同步性的测试装置 |
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- 2012-10-25 CN CN 201220550984 patent/CN202836959U/zh not_active Expired - Lifetime
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104819816A (zh) * | 2015-05-13 | 2015-08-05 | 中国飞机强度研究所 | 一种动载荷加载系统及飞机垂尾试验系统及方法 |
CN104819816B (zh) * | 2015-05-13 | 2017-11-03 | 中国飞机强度研究所 | 一种动载荷加载系统及飞机垂尾试验系统及方法 |
CN104897355B (zh) * | 2015-06-23 | 2017-05-17 | 中国航空工业集团公司西安飞机设计研究所 | 一种折叠翼非线性颤振试验装置 |
CN104897355A (zh) * | 2015-06-23 | 2015-09-09 | 中国航空工业集团公司西安飞机设计研究所 | 一种折叠翼非线性颤振试验装置 |
CN105258933A (zh) * | 2015-11-06 | 2016-01-20 | 航天科工哈尔滨风华有限公司 | 一种折叠舵芯展开试验装置 |
CN106871748A (zh) * | 2017-01-11 | 2017-06-20 | 北京理工大学 | 用于弹体多角度高速旋转条件下测试弹翼展开的旋转台 |
CN106871747A (zh) * | 2017-01-11 | 2017-06-20 | 北京理工大学 | 一种弹体多角度高速旋转条件下测试弹翼展开的装置 |
CN111003204A (zh) * | 2019-12-06 | 2020-04-14 | 江西洪都航空工业集团有限责任公司 | 一种飞机平尾伺服作动机构动刚度测试系统及测试方法 |
CN111003204B (zh) * | 2019-12-06 | 2022-12-02 | 江西洪都航空工业集团有限责任公司 | 一种飞机平尾伺服作动机构动刚度测试系统及测试方法 |
CN113495002A (zh) * | 2020-04-03 | 2021-10-12 | 中国航发商用航空发动机有限责任公司 | 航空发动机非全环风扇叶片的旋转冲击试验装置 |
CN111994302A (zh) * | 2020-09-08 | 2020-11-27 | 中国电子科技集团公司第四十一研究所 | 一种小型折叠翼无人机一体化地面测试平台及测试方法 |
CN111994302B (zh) * | 2020-09-08 | 2022-01-28 | 中国电子科技集团公司第四十一研究所 | 一种小型折叠翼无人机一体化地面测试平台及测试方法 |
CN113848046A (zh) * | 2021-09-08 | 2021-12-28 | 湖南航天机电设备与特种材料研究所 | 用于测试折叠翼飞行器翼面展开同步性的测试装置 |
CN113848046B (zh) * | 2021-09-08 | 2023-11-24 | 湖南航天机电设备与特种材料研究所 | 用于测试折叠翼飞行器翼面展开同步性的测试装置 |
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Assignee: Jiangxi Hongdu Technology Co.,Ltd. Assignor: JIANGXI HONGDU AVIATION INDUSTRY GROUP Co.,Ltd. Contract record no.: 2014360000189 Denomination of utility model: Test system for aircraft empennage folding and rotating mechanism Granted publication date: 20130327 License type: Exclusive License Record date: 20140714 |
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