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ACES II Pre-Planned Product Improvement (P3I) Program Update

机译:ACES II预先计划的产品改进(P3I)计划更新

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Ejection seats are inherently unstable during high and low speed ejections unless positive stabilization devices are incorporated. Today's expanded 103 to 245 pound aircrew size range further challenges seat stability. The USAF ACES II seat is by far the most stable ejection seat in the world under low speed conditions. The ACES II is stabilized at zero to low airspeed with the STAPAC rocket assembly, and is aerodynamically stabilized at high speed by the STAPAC and a 5.0 ft. hemisflo ribbon drogue parachute. The USAF developed the Enhanced Drogue System, as part of the US/Japan Cooperative Modification Project, which improves high-speed seat stability and reduces the aircrew injury risk. Goodrich, the seat OEM, and the USAF analyzed the Enhanced Drogue design under the ACES P3I Program and identified minor modifications that sled testing has shown further reduces the risk of injury without negatively impacting stability or terrain clearance.Concurrent with the drogue modification, the USAF and Goodrich have developed and sled tested an inertia reel access door retrofit kit for use on ACES II seats. This access door kit allows for inertia reel replacement while the seat is in the aircraft. A USAF decision on a separate inertia reel access door retrofit, versus combining it with the Enhanced Drogue retrofit, is pending. This update describes the process used to investigate drogue optimization and describes drogue reefing time and ratio changes allowing further improvement in MDRC performance for all occupants. In addition, the requirements and installation details of the inertia reel access door retrofit kit will be reviewed. Expanding the accommodation characteristics for legacy aircraft has challenged the crew escape and cockpit design community. In particular, the small occupant offers challenges in achieving the proper sitting eye height, reaching aircraft controls, and providing safe ejections. As part of the ACES P3I Program, Goodrich was tasked to integrate the accommodation enhancements from the CMP program with the comfort improvement program enhancements resulting in a comfortable accommodation package for today’s ACES II. In addition, Goodrich/UPCO has been tasked to incorporate accommodation kit maintenance improvements. Existing accommodation designs, design requirements for the updated accommodations kit, development status, safety impact, and performance data are reviewed.Limb flail is recognized as a major injury concern during high-speed ejections. The ACES P3I Program includes research and development of passive restraint systems to reduce limb flail injuries. The program is qualifying a retrofittable variant of the F/A-22 passive leg well restraint system for use on the F-15 and F-16 aircraft platforms. In addition, inflatable and net arm restraint technologies are being investigated. Special emphasis is being given to minimizing the aircraft modifications required to install the limb restraint systems into the aircraft. The requirements, design/qualification status, test schedule, and projected fielding timeframe for these systems will be reviewed as part of this update.
机译:除非掺入正稳定装置,否则喷射座在高速喷射期间固有地是不稳定的。今天扩大了103至245英镑的机组尺寸范围进一步挑战座椅稳定性。 USAF ACES II座位在低速条件下,世界上最稳定的喷射座位。 ACES II以零稳定为低空速与Stapac火箭组件,并且通过STAPAC和5.0英尺高的高速空气动力学稳定。Hemisflo带滴par降落伞。美国空军开发了增强型滴度系统,作为美国/日本合作改造项目的一部分,这提高了高速座椅稳定性并降低了机组损伤风险。在ACEP3I计划下,Coodrich,座椅OEM和USAF分析了增强的滴灌设计,并确定了SLED测试显示的次要修改,进一步降低了损伤的风险,而不会产生负面影响或地形清除。与USAF的滴灌修改进行负面影响和Goodrich已经开发出和雪橇测试了惯性卷轴进入门改装套件,用于ACES II座椅。该检修门套件允许坐在飞机中的惯性卷轴替代品。对单独的惯性卷轴接入门改造的USAF决定与增强的滴灌改装相结合,是待处理的。此更新描述了用于调查滴注优化的过程,并描述了滴注的时间和比率变化,从而进一步改善了所有乘员的MDRC性能。此外,将审查惯性卷轴接入门改造套件的要求和安装细节。扩大遗产飞机的住宿特点挑战了船员逃生和驾驶舱设计社区。特别是,小型乘员在实现适当的坐着眼睛高度,到达飞机控制和提供安全弹射方面提供挑战。作为ACES P3I计划的一部分,Goodrich是任务的,以将CMP程序的容纳增强功能与当今ACE II的舒适住宿套件集成了舒适性改进程序增强功能。此外,Goodrich / Upco已被任务合并住宿套件维护改进。现有的住宿设计,更新的住宿套件,开发状态,安全影响和性能数据的设计要求..LIMB牌照被认为是在高速喷射期间的主要伤害问题。 ACES P3i计划包括被动克制系统的研发,以减少肢体尾部伤害。该计划是符合F-15和F-16飞机平台上使用的F / A-22无源腿部粗限制的改造变体。此外,正在研究充气和净臂束缚技术。可以特别强调最小化将肢体约束系统安装到飞机中所需的飞机修改。这些系统的要求,设计/资格状态,测试计划和预计的Fielding TimeFrame将被视为此更新的一部分。

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