CN102501984B - 可计算襟翼丝杠加载的轴向力的襟翼加载装置 - Google Patents
可计算襟翼丝杠加载的轴向力的襟翼加载装置 Download PDFInfo
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- CN102501984B CN102501984B CN201110318492.5A CN201110318492A CN102501984B CN 102501984 B CN102501984 B CN 102501984B CN 201110318492 A CN201110318492 A CN 201110318492A CN 102501984 B CN102501984 B CN 102501984B
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- flap
- lead screw
- servoactuator
- coupling nut
- ball pivot
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CN201110318492.5A CN102501984B (zh) | 2011-10-19 | 2011-10-19 | 可计算襟翼丝杠加载的轴向力的襟翼加载装置 |
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CN201110318492.5A CN102501984B (zh) | 2011-10-19 | 2011-10-19 | 可计算襟翼丝杠加载的轴向力的襟翼加载装置 |
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CN102501984A CN102501984A (zh) | 2012-06-20 |
CN102501984B true CN102501984B (zh) | 2016-04-06 |
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Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
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CN103043225B (zh) * | 2012-12-10 | 2016-03-30 | 中国飞机强度研究所 | 一种用于飞机结构强度试验的力控和位控结合加载系统及方法 |
CN105667766B (zh) * | 2016-02-25 | 2017-12-19 | 陕西飞机工业(集团)有限公司 | 一种双缝后退式襟翼的调整方法 |
CN107856880A (zh) * | 2017-12-04 | 2018-03-30 | 西安庆安航空试验设备有限责任公司 | 襟翼作动装置试验过程中的加载运动机构 |
CN109515748B (zh) * | 2018-12-07 | 2022-03-29 | 江西洪都航空工业集团有限责任公司 | 一种飞机襟翼非线性力加载方法 |
CN113371227B (zh) * | 2021-07-22 | 2024-04-05 | 中国商用飞机有限责任公司 | 襟翼运动机构的试验台架 |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3949957A (en) * | 1973-11-06 | 1976-04-13 | Societe Nationale Industrielle Aerospatiale | Actuating system for wing leading-edge slats |
GB1535785A (en) * | 1976-03-04 | 1978-12-13 | Hawker Siddeley Aviation Ltd | Wing leading edge flaps |
EP0230061A1 (en) * | 1986-01-24 | 1987-07-29 | The Boeing Company | Trailing edge flaps |
CN202267598U (zh) * | 2011-10-19 | 2012-06-06 | 无锡市海航电液伺服系统有限公司 | 一种可计算襟翼丝杠加载的轴向力的襟翼加载装置 |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
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JP3611294B2 (ja) * | 2000-03-08 | 2005-01-19 | 三菱重工業株式会社 | 遠心力実験装置 |
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- 2011-10-19 CN CN201110318492.5A patent/CN102501984B/zh active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3949957A (en) * | 1973-11-06 | 1976-04-13 | Societe Nationale Industrielle Aerospatiale | Actuating system for wing leading-edge slats |
GB1535785A (en) * | 1976-03-04 | 1978-12-13 | Hawker Siddeley Aviation Ltd | Wing leading edge flaps |
EP0230061A1 (en) * | 1986-01-24 | 1987-07-29 | The Boeing Company | Trailing edge flaps |
CN202267598U (zh) * | 2011-10-19 | 2012-06-06 | 无锡市海航电液伺服系统有限公司 | 一种可计算襟翼丝杠加载的轴向力的襟翼加载装置 |
Non-Patent Citations (1)
Title |
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某型飞机襟翼系统可靠性分析;孙海龙等;《空军工程大学学报》;20060831;第7卷(第4期);第8-10页 * |
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Address after: 214027 No. 11, A, 1899 Jianghai Road, New District, Jiangsu, Wuxi Applicant after: Wuxi Haihang Electrohydraulic Servo System Co., Ltd. Address before: 214027 No. 11, A, 1899 Jianghai Road, New District, Jiangsu, Wuxi Applicant before: Wuxi Haihang Electrohydraulic Servo System Co.,Ltd. |
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Address after: 214101 No. 4, Chunlei Road, Xishan District, Wuxi City, Jiangsu Province Patentee after: WUXI HAIHANG ELECTRO-HYDRAULIC SERVO SYSTEM OF LIMITED BY SHARE LTD. Address before: 214027 No. 11, A, 1899 Jianghai Road, New District, Jiangsu, Wuxi Patentee before: WUXI HAIHANG ELECTRO-HYDRAULIC SERVO SYSTEM OF LIMITED BY SHARE LTD. |
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