火箭发动机端面密封静环热压工艺及故障分析

(1.西安航天发动机有限公司,陕西 西安 710100; 2.西安航天动力研究所,陕西 西安 710100)

静环; 热压工艺; 故障分析; 仿真计算; 试验验证

Hot pressing technology and fault analysis of face seal ring for rocket engine
WEI Fangsheng1, ZHUANG Suguo2, WANG Lei2, ZHANG Ya2, ZHANG Qiang2

(1.Xi'an Space Engine Company Limited, Xi'an 710100, China; 2.Xi'an Aerospace Propulsion Institute, Xi'an 710100, China)

static ring; hot pressing; fault analysis; simulation; test verification

备注

静环是端面密封的主要组成部分,石墨环热压环节是整个静环生产的核心,热压成品率直接关系端面密封的质量可靠性。结合生产工艺过程,深入分析了热压工艺机理,建立了静环热压的数学模型,明确了镶嵌应力、过盈量校核等一系列参数。在此基础上,形成了一套完备的热压工艺方法。结合某型号试车端面密封故障问题,对静环进行了仿真分析和试验验证。结果 表明,在热反浸过程端面密封受到高温作用,由于石墨材料线性膨胀系数发生变化,导致石墨环和静环座间的过盈量减小,过盈连接部位局部存在微缝隙,石墨环受高压介质挤压不均匀脱出,石墨环脱出不均匀导致石墨端面变形,产生泄漏。

Static ring is the main component of the face seal, the hot pressing of graphite ring is the core of the static ring production, the yield is directly related to the quality reliability.Based on the production process, the mechanism of hot pressing process was deeply analyzed, and the mathematical model of static ring hot pressing was established, and a series of parameter, such as the mosaic stress, the amount of interference were defined.On this basis, a complete set of hot pressing process was formed.The simulation analysis and experimental verification of the static ring were carried out based on the seal failure of a certain type of tests.Results show that in the process of hot dipping high temperature effect of face seal, the interference between graphite ring and static ring seat decreases due to the change of linear expansion coefficient of graphite material, then there are some gaps in the interference junction, graphite ring by high-pressure uneven extrusion, which leads to deformation of the graphite ring face and results in leakage.