aircraft static pressure error corrector 飞机静压误差校正器
aircraft static margin 飞机静安定性裕度
aircraft static inverter 航空静止变流器
aircraft ground static inverter 飞机地面静变电源
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.
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CCAR 23适航条例要求。
Then, the mathematics model of calculating the surface load and point load in the design of aircraft structure static load test using aircraft surface model is established.
其次结合飞机的曲面外形,建立了飞机结构静力试验设计中的分布式载荷和集中式载荷的演算数学模型。
The efficiency of a novel aircraft static inverter based on cascaded inverter is mainly rested with its DC link.
基于级联技术的新型航空静止变流器的效率主要取决于其直流变换环节。
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