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 simp... 展开
| 作者 | Zenobi, T. J. | ||
|---|---|---|---|
| 原报告号 | ADA1267392 | 总页数 | 11 |
| 主办者 | Non Paid ADAS | ||
| 报告分类号 | [51C - Aircraft] | ||
| 报告类别/文献类型 | AD / NTIS科技报告 | ||
| 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 | ||
