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1. 发明授权

US09920770B2 Flow machine 有权
公开(公告)号：US09920770B2
公开(公告)日：2018-03-20
申请号：US14881233
申请日：2015-10-13
申请人： Carsten Bennewa , Hildegard Ebbing , Emil Aschenbruck
发明人： Carsten Bennewa , Hildegard Ebbing , Emil Aschenbruck
IPC分类号： F04D29/54 , F04D29/10 , F04D29/52 , F04D29/053 , F04D29/056 , F04D19/00 , F01D11/00 , F01D9/02 , F01D25/16 , F01D25/24 , F04D29/12 , F04D29/62 , F04D29/64
CPC分类号： F04D29/54 , F01D11/003 , F04D29/122 , F04D29/624 , F04D29/644 , F05D2230/642
摘要： A flow machine with a rotor-side shaft includes: a stator-side housing in which the rotor-side shaft is mounted; a seal bushing configured to seal a gap between the stator-side housing and the rotor-side shaft; a retaining bolt configured to center the seal bushing at the stator-side housing in a heat-resilient manner; and a clamp configured to fix the seal bushing in a positively engaging manner at the stator-side housing while ensuring a radial displaceability of the seal bushing relative to the stator-side housing.

2. 发明申请

US20160130962A1 FLOW MACHINE 有权
标题翻译：流动机
公开(公告)号：US20160130962A1
公开(公告)日：2016-05-12
申请号：US14881233
申请日：2015-10-13
申请人： Carsten BENNEWA , Hildegard EBBING , Emil ASCHENBRUCK
发明人： Carsten BENNEWA , Hildegard EBBING , Emil ASCHENBRUCK
IPC分类号： F01D11/00 , F01D25/24 , F01D25/16 , F04D29/54 , F04D29/053 , F04D29/056 , F04D29/10 , F04D29/52 , F01D9/02 , F04D19/00
CPC分类号： F04D29/54 , F01D11/003 , F04D29/122 , F04D29/624 , F04D29/644 , F05D2230/642
摘要： A flow machine with a rotor-side shaft includes: a stator-side housing in which the rotor-side shaft is mounted; a seal bushing configured to seal a gap between the stator-side housing and the rotor-side shaft; a retaining bolt configured to center the seal bushing at the stator-side housing in a heat-resilient manner; and a clamp configured to fix the seal bushing in a positively engaging manner at the stator-side housing while ensuring a radial displaceability of the seal bushing relative to the stator-side housing.
摘要翻译：具有转子侧轴的流动机包括：转子侧轴安装在其中的定子侧壳体; 密封衬套，其构造成密封所述定子侧壳体和所述转子侧轴之间的间隙; 保持螺栓，其构造成以热弹性方式使所述密封衬套定位在所述定子侧壳体处; 以及夹具，被配置为将密封衬套以正向接合的方式固定在定子侧壳体上，同时确保密封衬套相对于定子侧壳体的径向位移。

3. 发明授权

US06832891B2 Device for sealing turbomachines 失效
标题翻译：密封涡轮机的装置
公开(公告)号：US06832891B2
公开(公告)日：2004-12-21
申请号：US10268422
申请日：2002-10-10
申请人： Emil Aschenbruck , Hildegard Ebbing , Andreas Kleinefeldt , Klaus Dieter Mohr
发明人： Emil Aschenbruck , Hildegard Ebbing , Andreas Kleinefeldt , Klaus Dieter Mohr
IPC分类号： F01D1100
CPC分类号： F01D11/001 , F01D11/025
摘要： A device for sealing between the guide vanes (1) and the rotor (17) of turbomachines, especially gas turbines has inner rings (3) suspended on the vane footing (14) of the guide vanes (1) in a thermally elastic manner with soldered honeycomb seal (4) and labyrinth tips (5) arranged on the rotor (17). First flow channels, which are connected to the cavities (21) of the cooled guide vanes (1), through which said cavities cooling air flows, are led through the vane footings (14). The first flow channels are connected to at least one of second flow channels led through the inner ring (3) to the vicinity of the honeycomb seal (4). The second flow channels open into at least one of third flow channels that are open at the rear edge of the inner ring (3) or are led to an annular groove (10) open toward the honeycomb seal (4) on the underside of the inner ring (3).
摘要翻译：一种用于在导叶（1）和涡轮机（特别是燃气轮机）的转子（17）之间进行密封的装置，其具有以热弹性方式悬挂在导叶（1）的叶片基脚（14）上的内环（3）焊接的蜂窝状密封件（4）和布置在转子（17）上的迷宫尖端（5）。连接到冷却的导向叶片（1）的空腔（21）的第一流动通道（冷却空气流过的空腔）被引导通过叶片基座（14）。第一流动通道连接到通过内环（3）引导到蜂窝密封件（4）附近的至少一个第二流动通道。第二流动通道打开到在内圈（3）的后边缘处开口的第三流动通道中的至少一个，或者被引导到朝向蜂窝状密封件（4）的下侧的开口的环形槽（10）内圈（3）。

4. 发明授权

US06568902B2 Device for cooling a component subject to temperature stress of nonuniform intensity 失效
公开(公告)号：US06568902B2
公开(公告)日：2003-05-27
申请号：US09898174
申请日：2001-07-03
申请人： Emil Aschenbruck , Hildegard Ebbing , Klaus Dieter Mohr
发明人： Emil Aschenbruck , Hildegard Ebbing , Klaus Dieter Mohr
IPC分类号： F01D2512
CPC分类号： F01D25/12 , F01D9/023 , F01D11/24 , F05D2260/201
摘要： A symmetrical component of a turbine unit, whose wall is exposed to a hot medium on one side and is subject to nonuniform thermal stress over the circumference, is cooled by a flow of cooling air being guided along the other side of the component. A ring (5) is provided with slots (7) or other openings for the passage of the cooling air. The ring (5) protrudes into the flow of the cooling air. The overall cross section of the slots (7) that are arranged in the sections of the ring (5) that are adjacent to the areas of the component that are subject to the higher stress is larger than the overall cross section of the slots (7) that are arranged in the sections of the ring (5) that are adjacent to the areas of the component that are subject to a lower stress.

5. 发明授权

US6155777A Removal of cooling air on the housing side of a diffuser of a compressor stage of gas turbines 失效
标题翻译：拆除燃气轮机压缩机级的扩散器壳体侧的冷却空气
公开(公告)号：US6155777A
公开(公告)日：2000-12-05
申请号：US256575
申请日：1999-02-24
申请人： Emil Aschenbruck , Hildegard Ebbing , Hans Otto Jeske , Ulrich Orth , Harald Schonenborn
发明人： Emil Aschenbruck , Hildegard Ebbing , Hans Otto Jeske , Ulrich Orth , Harald Schonenborn
IPC分类号： F02C7/18 , F04D29/44 , F04D29/54 , F01D9/06
CPC分类号： F04D29/682 , F04D29/444 , F05D2250/52 , Y10S415/914
摘要： The removal of cooling air from the diffuser part of a radial end stage of a compressor of a gas turbine is provided. Compressed air is removed via a cooling air discharge (10) from a radial compressor stage, which comprises a rotor disk (2) and a bladed diffuser (20). The removal of cooling air may be brought about such that the cooling air is removed on one side through openings (6) on the housing side (20.1) of the diffuser (20) and is fed through cooling air channels (10) to the parts in contact with hot gas, including the outer wall of the bifurcated tube (17). The compressed air is guided to the diffuser outside (20.2) through cooling air holes (19) in the diffuser blade (3).
摘要翻译：提供了从燃气轮机的压缩机的径向末端级的扩散器部分去除冷却空气。通过冷却空气排出口（10）从径向压缩机级除去压缩空气，其包括转子盘（2）和叶片式扩散器（20）。冷却空气的除去可以使得冷却空气在一侧通过扩散器（20）的壳体侧（20.1）上的开口（6）被移除，并且通过冷却空气通道（10）被供给到部件与包括分叉管（17）的外壁的热气体接触。压缩空气通过扩散器叶片（3）中的冷却空气孔（19）被引导到扩散器外部（20.2）。

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