首页> 外国专利> TURBOMACHINE CENTRIFUGAL COMPRESSOR COVER COVER ATTACHMENT METHOD, COMPRESSOR COVER OF IMPLEMENTATION AND COMPRESSOR ASSEMBLY PROVIDED WITH SUCH COVER

TURBOMACHINE CENTRIFUGAL COMPRESSOR COVER COVER ATTACHMENT METHOD, COMPRESSOR COVER OF IMPLEMENTATION AND COMPRESSOR ASSEMBLY PROVIDED WITH SUCH COVER

机译:透平机离心压缩机盖的安装方法,执行器的压缩机盖和带有这种盖的压缩机组件

摘要

The present invention aims to allow centrifugal compressor cover displacement so that the clearance between the cover and the compressor wheel blades remains substantially constant and as low as possible. To do this, the invention proposes a type of attachment configuration in the middle of the lid having an elastically deformable portion. A cover has a concave envelope (50) having an inner face (51) arranged at a distance from the compressor (12) equipped with a wheel (22) provided with fins (20) by a fastener (8). The fastener (8) has a junction end (83) in the middle of the casing (50), and another end (82) fixed to a casing (6) of the turbomachine (1). The fastener (8) comprises an axially symmetrical diaphragm (80) of generally frusto-conical configuration having an arm profile (8b) coupled to the attachment end (82) to the casing (6) by a double-elbow joint (8c, 8d). , 8e) of right angles and obtuse at rest. The distance between the inner face (51) of the envelope (50) and the upper edges (21) of the fins (20) is able to be kept constant in operation with a minimum clearance setting.
机译:本发明的目的是允许离心式压缩机盖移位,从而使得盖与压缩机叶轮叶片之间的间隙保持基本恒定并且尽可能小。为此,本发明提出了一种在盖的中间具有弹性可变形部分的附接构造。盖具有凹入的外壳(50),该凹入的外壳(50)具有内表面(51),该内表面(51)布置成与压缩机(12)相距一定距离,该压缩机(12)配备有通过紧固件(8)设置有翅片(20)的轮(22)。紧固件(8)在壳体(50)的中央具有接合端(83),并且另一端(82)固定在涡轮机(1)的壳体(6)上。紧固件(8)包括大体上为截头圆锥形构造的轴向对称隔膜(80),该隔膜具有臂轮廓(8b),该臂轮廓通过双肘关节(8c,8d)联接至附接端(82)至壳体(6)。 )。 ,8e)成直角,静止时钝角。外壳(50)的内表面(51)和散热片(20)的上边缘(21)之间的距离在操作中能够以最小的间隙设置保持恒定。

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