Aircraft Acceleration Sensitive Inertia Reel Lock.

机译：飞机加速敏感惯性卷轴锁。

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摘要

The Navy has designed, built and tested an aircraft acceleration sensitive inertia reel lock for crewmember positioning and restraint during eyeballs out (-gx) accelerations such as during an aircraft flat spin. The design is simple and retrofittable to many ejection seats. Centrifuge tests at NADC indicate the locking device performs effectively and reliably. (Author)

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Zenobi, T. J.;
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年度 1982
页码 1-11
总页数 11
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Locking fastener devices; Restraint; Ejection seats; High acceleration; Performance(Engineering); Naval aircraft; Centrifuges; Performance tests; Centrifugal force; Inertia; Flight crews; Control systems; Aircraft seats; Experimental design; Reels; Straps; Release mechanisms; Spinning(Motion); Flight maneuvers; Aviation safety;

机译：锁定紧固件装置;约束;弹射座椅;高加速度;性能（工程）;海军飞机;离心机;性能测试;离心力;惯性;飞行机组;控制系统;飞机座椅;实验设计;卷轴;带子;释放机构;旋转（动议）;飞行演习;航空安全;

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8. Aircraft Acceleration Sensitive Inertia Reel Lock. [R] . Zenobi, T. J. 1982

机译：飞机加速敏感惯性卷轴锁。

Aircraft Acceleration Sensitive Inertia Reel Lock.

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