Intermediate compressor case for gas turbine engines
    1.
    发明授权
    Intermediate compressor case for gas turbine engines 失效
    燃气轮机发动机中级压缩机箱

    公开(公告)号:US3907455A

    公开(公告)日:1975-09-23

    申请号:US44040774

    申请日:1974-02-07

    CPC classification number: F04D29/403

    Abstract: In a multistage split compressor wherein the low pressure compressor has a plurality of stages on one rotor and the high pressure compressor has a plurality of stages on another rotor, the low pressure compressor is removable as a unit from the high pressure compressor by making the intermediate case in two pieces, one integral with the low pressure compressor case with an associated bearing for the low pressure rotor and the other integral with the high pressure compressor case also with an associated bearing for the high pressure rotor. By having these two pieces removably secured together, the associated compressor cases may be separated by removal of the attachment devices holding the cases together, and each case carries with it the associated bearing for the enclosed rotor.

    Abstract translation: 在多级压缩机中,低压压缩机在一个转子上具有多个级,而高压压缩机在另一个转子上具有多个级,低压压缩机可作为一个单元从高压压缩机中取出, 壳体分为两个部分,一个与低压压缩机壳体一体,其具有用于低压转子的相关轴承,另一个与高压压缩机壳体集成,还具有用于高压转子的相关联的轴承。 通过将这两个部件可拆卸地固定在一起,相关的压缩机壳体可以通过移除将壳体保持在一起的附接装置而分开,并且每个壳体都带有用于封闭转子的相关轴承。

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