公开(公告)号：US20150292341A1

公开(公告)日：2015-10-15

申请号：US14680292

申请日：2015-04-07

Applicant: ALSTOM Technology Ltd

Inventor： Robert PRZYBYL ,  Oliver Jeseph Taheny ,  Giovanni Cataldi

IPC: F01D9/04 ,  F04D29/54 ,  F01D25/26

CPC classification number: F01D9/04 ,  F01D9/041 ,  F01D9/042 ,  F01D11/005 ,  F01D11/18 ,  F01D25/246 ,  F01D25/265 ,  F04D29/541 ,  F05D2220/31 ,  F05D2220/32 ,  F05D2230/90 ,  F05D2240/12 ,  F05D2240/14 ,  F05D2300/171 ,  F05D2300/502 ,  F05D2300/50212

Abstract: A vane carrier is provided for a compressor or a turbine section of an axial turbo machine, especially one of a gas turbine, steam turbine, compressor, expander, comprises least a first and second functional means. The first functional means is a cylinder made of a material with a coefficient of thermal expansion (CTE) below 1.3×10−5 [1/K]. The cylinder is provided for carrying a plurality of vanes on its inner side. The second functional means is a support structure made of a material different to and less expensive than the material of said first functional means. The support structure is provided for defining an axial and lateral position of the first functional means within an outer casing of the axial turbo machine.

Abstract translation: 提供了一种用于轴流涡轮机的压缩机或涡轮机部分的叶片载体，特别是燃气轮机，蒸汽轮机，压缩机，膨胀机中的一个，包括至少一个第一和第二功能装置。 第一功能装置是由热膨胀系数（CTE）低于1.3×10-5 [1 / K]的材料制成的圆筒。 气缸被设置用于在其内侧上承载多个叶片。 第二功能装置是由与所述第一功能装置的材料不同并且便宜的材料制成的支撑结构。 提供支撑结构用于在轴向涡轮增压机的外壳内限定第一功能装置的轴向和横向位置。

公开(公告)号：US20150010389A1

公开(公告)日：2015-01-08

申请号：US14317643

申请日：2014-06-27

Applicant: ALSTOM Technology Ltd

Inventor： Armin BUSEKROS ,  Robert PRZYBYL ,  Gregory JEUNET-MANCY

IPC: F01D25/26

CPC classification number: F01D25/26 ,  F01D25/12 ,  F01D25/14 ,  F01D25/243

Abstract: The invention relates to a pressure casing, which includes a plurality of casing shells which are connected in a pressure-tight manner in a parting plane by means of a flange. The casing shells are pressed together with sealing effect in the parting plane in the region of the flange by means of at least one threaded bolt which extends in a through hole through the flange perpendicularly to the parting plane. Reduced temperature differences between the flange and the connecting bolts of the flanged joint are achieved by the at least one threaded bolt being charged with a heat transfer medium over a part of its length. The heat transfer medium is supplied via holes extending through the flange.

Abstract translation: 压力壳体技术领域本发明涉及一种压力壳体，其包括多个壳体壳体，所述壳体壳体通过凸缘在分离平面中以压力方式连接。 壳体壳体通过至少一个螺纹孔在法兰区域的分型平面中被压在一起，该螺栓在通孔中垂直于分型平面延伸穿过凸缘。 法兰和法兰接头的连接螺栓之间的温度差降低是通过至少一个螺栓在其长度的一部分上装有传热介质来实现的。 传热介质通过延伸穿过凸缘的孔提供。