| 飞机全机悬空静力试验技术 |
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| 引用本文： | 彭刚.飞机全机悬空静力试验技术[J].洪都科技,2009(4):34-43. |
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| 作者姓名： | 彭刚 |
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| 作者单位： | 洪都航空工业集团 |
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| 摘 要： | 新飞机研制必须经全机悬空静力试验验证其结构的强度是否满足强度规范和CCAR23适航条例要求。本文针对飞机全机悬空静力试验的技术方法和试验误差分析进行了简要介绍。
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| 关 键 词： | 结构重量 全机平衡 误差分析 |
Suspended Static Test of Aircraft |
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| Peng Gang.Suspended Static Test of Aircraft[J].Hongdu Science and Technology,2009(4):34-43. |
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| Authors: | Peng Gang |
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| Institution: | Peng Gang (Hongdu Aviation Industry Group) |
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| Abstract: | During the design of a new aircraft, the suspended static test must be carried out to test whether its structure can satisfy the need of strength specification and CCAR23 air worthiness test. I shall give a brief introduction of aircraft suspended static test method and deviation analysis in this paper. |
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| Keywords: | Structural weight Balance of entire aircraft Deviation analysis |
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