本文選題：氣囊 + 緩沖�。� 參考：《包裝工程》2017年11期

【摘要】：目的總結當前著陸緩沖氣囊的國內(nèi)外研究現(xiàn)狀。方法介紹不同緩沖氣囊的工作原理與優(yōu)缺點,總結解析與有限元2種氣囊性能的計算方法與性能參數(shù)優(yōu)化方法的研究現(xiàn)狀,以及氣囊技術研究的發(fā)展方向。結果分析了各類緩沖氣囊與性能參數(shù)計算方法的優(yōu)缺點,總結了氣囊技術待解決的問題。結論提高緩沖氣囊的氣壓主動控制技術與著陸姿態(tài)控制技術可進一步提高氣囊性能。
[Abstract]:Objective to summarize the current research status of landing cushion airbag at home and abroad. Methods the working principle, advantages and disadvantages of different cushioning airbags were introduced, and the current research status of the analytical and finite element methods for calculating the performance of airbags and the optimization methods of performance parameters were summarized, as well as the development trend of airbag technology. Results the advantages and disadvantages of various cushioning airbags and performance parameters were analyzed, and the problems to be solved were summarized. Conclusion the air pressure active control technology and landing attitude control technology can further improve the performance of the airbag.
【作者單位】： 軍械工程學院;軍械技術研究所;
【分類號】：TB485.1
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本文編號：1822718