首页> 外文OA文献 >Factors Contributing to Pilot Valve Fuel Seal Extrusion in Orbiter PRCS Thrusters
【2h】

Factors Contributing to Pilot Valve Fuel Seal Extrusion in Orbiter PRCS Thrusters

机译:轨道飞行器PRCS推进器中先导阀油封挤压的因素

摘要

Extrusion of the polytetrafluoroethylene (PTFE) pilot seal used in the monomethylhydrazine (fuel) valve of the Orbiter Primary Reaction Control System (PRCS) thrusters has been implicated in numerous on-orbit thruster failures and on-ground valve failures. Two extrusion mechanisms have been proposed, one or both may be occurring. The first mechanism is attributed to thermal expansion mismatch between adjacent PTFE and metal parts used in the fuel valve, and is referred to as thermal extrusion. The second mechanism is attributed to nitrogen tetroxide (oxidizer) leakage from the adjacent oxidizer valve on the same thruster during ground turnaround, and is referred to as oxidizer-induced extrusion. Model calculations of PTFE pilot seal in an exact pilot valve configuration show that extrusion can be caused by differential thermal expansion, without the intervening influence of oxidizer. Experimental data on semitrapped PTFE and TFM (modified PTFE) specimens simulating a fuel pilot valve configuration show that thermal extrusion 1) is incremental and irreversible, 2) increases with the size of the thermal excursion, 3) decreases with successive thermal cycling, and 4) is accompanied by gap formation. Both PTFE and TFM exhibit a higher affinity for oxidizer than fuel. The property changes associated with oxidizer uptake may explain why oxidizer seals do not exhibit extrusion. Impression replicas of fuel pilot seals removed from the Orbiter fleet show two types of extrusion: extrusion of the entire seal (loaded extrusion), or extrusion of non-sealing surface (unloaded extrusion). Both extrusion types may arise from differences in service history, rather than in failure mechanism. The plausibility oxidizer-induced extrusion was evaluated. Preliminary calculations suggest that enough energy, heat, or gas may be liberated under certain operational scenarios to cause catastrophic extrusion. However, given the lack of supporting data, conclusions implicating oxidizer leakage as a factor in extrusion must be made with caution.
机译:轨道器主反应控制系统(PRCS)推进器的单甲基肼(燃料)阀中使用的聚四氟乙烯(PTFE)先导密封件的挤出与许多在轨推进器故障和地面阀门故障有关。已经提出了两种挤出机制,一种或两种都可能发生。第一种机制归因于相邻的PTFE与燃料阀中使用的金属零件之间的热膨胀失配,被称为热挤压。第二种机制归因于地面转向过程中同一推进器上相邻氧化剂阀的四氧化氮(氧化剂)泄漏,被称为氧化剂诱发的挤出。在精确的先导阀配置中的PTFE先导密封件的模型计算表明,挤出可以由热膨胀差异引起,而没有氧化剂的干预。半圈式PTFE和TFM(改性PTFE)样品的模拟燃料先导阀配置的实验数据表明,热挤压1)是增量且不可逆的; 2)随着热偏移量的增加而增加; 3)随着连续的热循环而减少; 4 )伴随着间隙的形成。 PTFE和TFM对氧化剂的亲和力都比燃料高。与氧化剂吸收有关的性质变化可以解释为什么氧化剂密封件不显示挤出。从Orbiter机群中取出的燃料引燃密封件的印象复制品显示两种挤压类型:整个密封件的挤压(带负载的挤压)或非密封表面的挤压(无负载的挤压)。两种挤压类型都可能是由于维修历史的差异而不是由于失效机理而引起的。评价了似真性氧化剂诱导的挤出。初步计算表明,在某些操作方案下,可能会释放出足够的能量,热量或气体,从而导致灾难性的挤压。但是,由于缺乏支持数据,必须谨慎地得出将氧化剂泄漏作为挤出因素的结论。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号