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COMBUSTION CHAMBER ASSEMBLY WITH DIFFERENT CURVATURES FOR A COMBUSTION CHAMBER WALL AND A COMBUSTION CHAMBER SHINGLE FIXED THERETO

机译:燃烧室壁用不同曲率的燃烧室组件和固定在其上的燃烧室瓦

摘要

A combustion chamber assembly group, and a mounting method therefor, includes a combustion chamber for an engine that includes a curved combustion chamber wall extending along two spatial directions, and a combustion chamber shingle affixed at an inner side of the combustion chamber wall and having a shingle edge defining the outer contour of the shingle. For an at least sectional abutment of the shingle edge at the combustion chamber wall with a minimum clamping force in an operational state of the engine, the shingle is mounted to the combustion chamber wall in a mounting state in which the shingle at least at one section of the shingle edge has a curvature with respect to at least one of the spatial directions that differs from the curvature of the combustion chamber wall with respect to this spatial direction.
机译:燃烧室组件组及其安装方法,包括用于发动机的燃烧室,该燃烧室包括沿两个空间方向延伸的弯曲燃烧室壁,以及固定在该燃烧室壁的内侧并具有一个瓦边缘,定义瓦的外部轮廓。为了在发动机的运行状态下以最小的夹紧力使带状板边缘在燃烧室壁上至少部分地邻接,将带状板在安装状态下安装到燃烧室壁上,其中,带状板至少在一个部分处带状板边缘的曲率相对于至少一个空间方向具有曲率,该曲率与燃烧室壁相对于该空间方向的曲率不同。

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