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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 USAFand Goodrich have developed and sled tested aninertia reel access door retrofit kit for use on ACESII seats. This access door kit allows for inertia reelreplacement while the seat is in the aircraft. AUSAF decision on a separate inertia reel access doorretrofit, versus combining it with the EnhancedDrogue retrofit, is pending. This update describesthe process used to investigate drogue optimizationand describes drogue reefing time and ratio changesallowing further improvement in MDRCperformance for all occupants. In addition, the requirements and installation details of the inertiareel access door retrofit kit will be reviewed.Expanding the accommodation characteristics forlegacy aircraft has challenged the crew escape andcockpit design community. In particular, the smalloccupant offers challenges in achieving the propersitting eye height, reaching aircraft controls, andproviding safe ejections. As part of the ACES P3IProgram, Goodrich was tasked to integrate theaccommodation enhancements from the CMPprogram with the comfort improvement programenhancements resulting in a comfortableaccommodation package for today’s ACES II. Inaddition, Goodrich/UPCO has been tasked toincorporate accommodation kit maintenanceimprovements. Existing accommodation designs,design requirements for the updatedaccommodations kit, development status, safetyimpact, and performance data are reviewed.Limb flail is recognized as a major injury concernduring high-speed ejections. The ACES P3I Programincludes research and development of passiverestraint systems to reduce limb flail injuries. Theprogram is qualifying a retrofittable variant of theF/A-22 passive leg well restraint system for use onthe F-15 and F-16 aircraft platforms. In addition,inflatable and net arm restraint technologies arebeing investigated. Special emphasis is being givento minimizing the aircraft modifications required toinstall the limb restraint systems into the aircraft.The requirements, design/qualification status, testschedule, and projected fielding timeframe for thesesystems will be reviewed as part of this update.
机译:除非装有强制稳定装置,否则在高速和低速弹出过程中,弹出座本质上是不稳定的。如今,机组人员的飞行范围已从103磅扩大到245磅,这进一步挑战了座椅的稳定性。在低速条件下,USAF ACES II座椅是迄今为止世界上最稳定的弹射座椅。通过STAPAC火箭组件,ACES II可以在零到低空速下保持稳定,并通过STAPAC和5.0英尺的hemisflo带状锥状降落伞在高速上将空气动力学稳定在空气中。作为美国/日本合作改装项目的一部分,美国空军开发了增强型锥套系统,该系统可提高高速座椅的稳定性并降低机组人员受伤的风险。 Goodrich,座椅原始设备制造商和USAF分析了ACES P3I计划下的增强型Drogue设计,并确定了雪橇测试已表明的较小改动,从而进一步降低了受伤风险,而不会对稳定性或地形间隙造成负面影响。 和古德里奇(Goodrich)已开发并测试了雪橇 用于ACES的惯性卷轴检修门改装套件 II座位。该检修门套件可用于惯性卷盘 座位在飞机上时进行更换。一种 美国空军决定另行购买惯性卷轴检修门 改造,与将其与增强型产品相结合 Drogue改造,正在等待中。此更新描述 研究锥套优化的过程 并描述锥套收礁时间和比率变化 可以进一步改善MDRC 所有乘员的表现。另外,惯性的要求和安装细节 卷轴检修门改装套件将受到审查。 扩大住宿特色 遗留飞机已向机组人员的逃生挑战, 座舱设计社区。特别是小 居住者在实现适当的生活方面面临挑战 坐着的眼睛高度,达到飞机控制,以及 提供安全的弹射。作为ACES P3I的一部分 计划中,Goodrich的任务是整合 CMP提供的住宿增强功能 舒适度改善计划 增强功能带来舒适感 适用于当今ACES II的住宿套餐。在 此外,Goodrich / UPCO的任务是 整合住宿套件维护 改进。现有的住宿设计, 更新的设计要求 住宿套件,发展状况,安全 影响和性能数据。肢体连fl被认为是主要的伤害问题 在高速弹出时。 ACES P3I计划 包括被动的研发 约束系统,以减少四肢fl伤。这 程序符合资格的 F / A-22被动腿束约束系统,用于 F-15和F-16飞机平台。此外, 充气和网臂约束技术是 正在调查中。特别强调 尽量减少对飞机的改装 将肢体约束系统安装到飞机上。 要求,设计/资格状态,测试 时间表,以及这些的预计部署时间框架 系统将作为此更新的一部分进行审查。

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