The invention belongs to the technical field of aircraft design, and particularly relates to an ultra-long cabin door adjusting structure and method for a transport plane, which mainly comprise cabin door initial centering adjustment, cabin door gap and jump adjustment and adjustment of a closed position centering guide device. And the hatch can be ensured to be positioned on the symmetric line of the airplane.
本申请属于飞机设计技术领域,特别涉及一种运输机超长型舱门调整结构以及调整方法,主要划分为舱门初始对中调整、舱门间隙和阶差调整及关闭位对中导向装置的调整。能够保证舱门阶差、间隙满足要求且能够保证舱门位于飞机对称线上。
Transporter super-long cabin door adjusting structure and adjusting method
一种运输机超长型舱门调整结构以及调整方法
2025-02-18
Patent
Electronic Resource
Chinese
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