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1. 发明申请

US20100247005A1 Sealing Segment and Sealing-Segment Arrangement 有权
标题翻译：密封段和密封段安排
公开(公告)号：US20100247005A1
公开(公告)日：2010-09-30
申请号：US12738771
申请日：2008-11-03
申请人： Emil Aschenbruck , Michael Blaswich , Jaman El Masalme , Frank Reiss
发明人： Emil Aschenbruck , Michael Blaswich , Jaman El Masalme , Frank Reiss
IPC分类号： F16C33/74 , F16C29/02 , F16C33/02 , F16C33/06 , F16J15/16 , F02C7/28
CPC分类号： F16J15/0893 , F01D9/023 , F01D11/005 , F05D2230/642 , F05D2240/11
摘要： A sealing segment for sealingly connecting two structural components parts which are movable relative to one another, with two sealing bodies which are connected to one another by a web and which can be arranged in recesses of the structural component parts in an articulated manner, and a sealing segment arrangement with a plurality of sealing segments of this type, and a flow machine with a sealing segment arrangement of this type.
摘要翻译：密封段，用于密封地连接可相对于彼此移动的两个结构部件的两个密封体，两个密封体通过腹板彼此连接并且可以铰接的方式布置在结构部件的凹部中，具有这种类型的多个密封段的密封段布置，以及具有这种类型的密封段布置的流动机。

2. 发明授权

US09182039B2 Sealing segment and sealing-segment arrangement 有权
标题翻译：密封段和密封段布置
公开(公告)号：US09182039B2
公开(公告)日：2015-11-10
申请号：US12738771
申请日：2008-11-03
申请人： Emil Aschenbruck , Michael Blaswich , Jaman El Masalme , Frank Reiss
发明人： Emil Aschenbruck , Michael Blaswich , Jaman El Masalme , Frank Reiss
IPC分类号： F16J15/08 , F01D9/02 , F01D11/00
CPC分类号： F16J15/0893 , F01D9/023 , F01D11/005 , F05D2230/642 , F05D2240/11
摘要： A sealing segment for sealingly connecting two structural components parts which are movable relative to one another, with two sealing bodies which are connected to one another by a web and which can be arranged in recesses of the structural component parts in an articulated manner, and a sealing segment arrangement with a plurality of sealing segments of this type, and a flow machine with a sealing segment arrangement of this type.
摘要翻译：密封段，用于密封地连接可相对于彼此移动的两个结构部件的两个密封体，两个密封体通过腹板彼此连接并且可以铰接的方式布置在结构部件的凹部中，具有这种类型的多个密封段的密封段布置，以及具有这种类型的密封段布置的流动机。

3. 发明授权

US09739176B2 Turbomachine 有权
公开(公告)号：US09739176B2
公开(公告)日：2017-08-22
申请号：US14520992
申请日：2014-10-22
申请人： Emil Aschenbruck , Jaman El Masalme , Michael Blaswich
发明人： Emil Aschenbruck , Jaman El Masalme , Michael Blaswich
IPC分类号： F01D9/04 , F01D25/24 , F01D9/00 , F01D9/02
CPC分类号： F01D25/246 , F01D9/00 , F01D9/02 , F01D9/041 , F01D9/042 , F05D2220/32 , F05D2240/14 , F05D2240/91
摘要： A turbomachine includes: a stator-side housing having: a plurality of stator-side guide vane supports fastened to the stator-side housing, stator-side guide vanes fastened to the stator-side guide vane supports, and axially spaced guide vane rings; and a rotor having a plurality of rotor-side moving blades. At least two guide vane supports are jointly fastened to and centered on a flange of the stator-side housing.

4. 发明授权

US07175385B2 Mounting of the rotor of a gas turbine 失效
标题翻译：安装燃气轮机的转子
公开(公告)号：US07175385B2
公开(公告)日：2007-02-13
申请号：US11007817
申请日：2004-12-08
申请人： Emil Aschenbruck , Michael Blaswich , Andreas Kleinefeldt , Ulrich Orth
发明人： Emil Aschenbruck , Michael Blaswich , Andreas Kleinefeldt , Ulrich Orth
IPC分类号： F01D25/16
CPC分类号： F01D3/00 , F01D25/16 , F02C7/06 , F05D2240/52 , F05D2240/54
摘要： The rotor (5) of a gas turbine containing a compressor part (1) and a turbine part (3) is mounted in an axial thrust bearing (19) and in two radial journal bearings (16, 17). One of the bearings is a journal bearing (16) arranged in the intake area of the compressor part (1) and the other journal bearing (17) together with the thrust bearing (19) is arranged in the area of the turbine part (3).
摘要翻译：包含压缩机部分（1）和涡轮部分（3）的燃气轮机的转子（5）安装在轴向推力轴承（19）和两个径向轴颈轴承（16,17）中。其中一个轴承是布置在压缩机部件（1）的进气区域中的轴颈轴承（16），另一个轴颈轴承（17）与止推轴承（19）一起布置在涡轮部分（3）的区域中）。

5. 发明申请

US20050129506A1 Mounting of the rotor of a gas turbine 失效
标题翻译：安装燃气轮机的转子
公开(公告)号：US20050129506A1
公开(公告)日：2005-06-16
申请号：US11007817
申请日：2004-12-08
申请人： Emil Aschenbruck , Michael Blaswich , Andreas Kleinefeldt , Ulrich Orth
发明人： Emil Aschenbruck , Michael Blaswich , Andreas Kleinefeldt , Ulrich Orth
IPC分类号： F01D25/16 , F01D3/00 , F02C7/06 , F16C35/02
CPC分类号： F01D3/00 , F01D25/16 , F02C7/06 , F05D2240/52 , F05D2240/54
摘要： The rotor (5) of a gas turbine containing a compressor part (1) and a turbine part (3) is mounted in an axial thrust bearing (19) and in two radial journal bearings (16, 17). One of the bearings is a journal bearing (16) arranged in the intake area of the compressor part (1) and the other journal bearing (17) together with the thrust bearing (19) is arranged in the area of the turbine part (3).
摘要翻译：包含压缩机部分（1）和涡轮部分（3）的燃气轮机的转子（5）安装在轴向推力轴承（19）和两个径向轴颈轴承（16,17）中。其中一个轴承是布置在压缩机部件（1）的进气区域中的轴颈轴承（16），另一个轴颈轴承（17）与止推轴承（19）一起布置在涡轮部分（3）的区域中）。

6. 发明授权

US08727718B2 Turbine rotor for a gas turbine 有权
标题翻译：用于燃气轮机的涡轮转子
公开(公告)号：US08727718B2
公开(公告)日：2014-05-20
申请号：US12864039
申请日：2008-11-03
申请人： Emil Aschenbruck , Ralf Müller , Michael Blaswich
发明人： Emil Aschenbruck , Ralf Müller , Michael Blaswich
IPC分类号： F01D5/30 , F01D5/06
CPC分类号： F01D5/066
摘要： A turbine rotor (1) for a gas turbine with a one-piece compressor housing (11) or a compressor housing (11) which is divided in a first plane, a one-piece turbine housing (12) connected to the compressor housing (11) or a turbine housing (12) which is divided in a second plane different from the first plane comprises a compressor area which includes at least two compressor disks (2.1-2.5) and a turbine area which includes at least one turbine disk (13.1, 13.2). The compressor disks and turbine disks are clamped together by a tie rod arrangement which includes at least one tie rod (6) which has a first fastening area, a second fastening area for clamping at least two compressor disks between the first fastening area and the second fastening area, and a third fastening area for clamping at least one turbine disk.
摘要翻译：一种用于燃气轮机的涡轮转子（1），其具有一体式压缩机壳体（11）或分为第一平面的压缩机壳体（11），连接到压缩机壳体的一体式涡轮机壳体（12）分隔在不同于第一平面的第二平面中的涡轮壳体（12）包括压缩机区域，其包括至少两个压缩机盘（2.1-2.5）和涡轮区域，该涡轮机区域包括至少一个涡轮盘（13.1 ，13.2）。压缩机盘和涡轮盘通过拉杆装置夹紧在一起，所述拉杆装置包括至少一个具有第一紧固区域的拉杆（6），用于在第一紧固区域和第二紧固区域之间夹紧至少两个压缩机盘的第二紧固区域紧固区域和用于夹持至少一个涡轮盘的第三紧固区域。

7. 发明申请

US20110038718A1 Fluid Flow Machine 审中-公开
标题翻译：流体流动机
公开(公告)号：US20110038718A1
公开(公告)日：2011-02-17
申请号：US12841317
申请日：2010-07-22
申请人： Emil Aschenbruck , Michael Blaswich
发明人： Emil Aschenbruck , Michael Blaswich
IPC分类号： F01D11/08
CPC分类号： F16J15/3288 , F01D11/001 , F01D11/003 , F01D11/02 , F05D2240/56
摘要： A fluid flow machine has a stator, a rotor which is supported so as to be rotatable relative to the stator, and a brush seal which seals a gap formed between the stator and rotor in a radial direction to prevent the passage of fluid. The brush seal has a brush holder and a plurality of sealing bristles, each of which has a first end that is fastened to the brush holder and a second end that contacts a sealing surface. The sealing surface is rotationally displaceable relative to the second ends of the respective sealing bristles. The sealing surface is formed by a circumferential surface of an intermediate sleeve which is arranged between the stator and rotor and which radially divides the gap.
摘要翻译：流体流动机具有定子，以相对于定子可转动的方式被支撑的转子以及在径向上密封形成在定子与转子之间的间隙的刷密封件，以防止流体通过。刷子密封件具有刷子保持器和多个密封刷毛，每个密封刷毛具有紧固到刷子保持器的第一端和与密封表面接触的第二端。密封表面相对于相应密封刷毛的第二端旋转移位。密封面是由定子和转子之间的中间套筒的圆周表面形成的，并且将间隙径向分开。

8. 发明申请

US20100290911A1 Turbine Rotor for a Gas Turbine 有权
标题翻译：涡轮转子用于燃气轮机
公开(公告)号：US20100290911A1
公开(公告)日：2010-11-18
申请号：US12864039
申请日：2008-11-03
申请人： Emil Aschenbruck , Ralf Müller , Michael Blaswich
发明人： Emil Aschenbruck , Ralf Müller , Michael Blaswich
IPC分类号： F01D5/06 , F01D5/30 , B23P15/04
CPC分类号： F01D5/066
摘要： A turbine rotor (1) for a gas turbine with a one-piece compressor housing (11) or a compressor housing (11) which is divided in a first plane, a one-piece turbine housing (12) connected to the compressor housing (11) or a turbine housing (12) which is divided in a second plane different from the first plane comprises a compressor area which includes at least two compressor disks (2.1-2.5) and a turbine area which includes at least one turbine disk (13.1, 13.2). The compressor disks and turbine disks are clamped together by a tie rod arrangement which includes at least one tie rod (6) which has a first fastening area, a second fastening area for clamping at least two compressor disks between the first fastening area and the second fastening area, and a third fastening area for clamping at least one turbine disk.
摘要翻译：一种用于燃气轮机的涡轮转子（1），其具有一体式压缩机壳体（11）或分为第一平面的压缩机壳体（11），连接到压缩机壳体的一体式涡轮机壳体（12）分隔在不同于第一平面的第二平面中的涡轮壳体（12）包括压缩机区域，其包括至少两个压缩机盘（2.1-2.5）和涡轮区域，该涡轮机区域包括至少一个涡轮盘（13.1 ，13.2）。压缩机盘和涡轮盘通过拉杆装置夹紧在一起，拉杆装置包括至少一个具有第一紧固区域的拉杆（6），用于在第一紧固区域和第二紧固区域之间夹紧至少两个压缩机盘的第二紧固区域紧固区域和用于夹持至少一个涡轮盘的第三紧固区域。

9. 发明授权

US08784064B2 Multi-component bladed rotor for a turbomachine 有权
标题翻译：用于涡轮机的多组分叶片式转子
公开(公告)号：US08784064B2
公开(公告)日：2014-07-22
申请号：US12812862
申请日：2008-12-11
申请人： Emil Aschenbruck , Michael Blaswich , Andreas Kleinefeldt , William F. Cline
发明人： Emil Aschenbruck , Michael Blaswich , Andreas Kleinefeldt , William F. Cline
IPC分类号： F01D5/30
CPC分类号： F01D5/3038 , F01D5/06 , F01D5/066 , F01D5/3069 , F05D2240/20 , F05D2260/30 , F05D2260/36
摘要： A multipart bladed rotor (1) for a flow machine, particularly a gas turbine or steam turbine or an axial compressor, has at least two disks (2) whose front sides, which face one another, are connected to one another, particularly by positive engagement, in a separating plane (7) so as to be fixed with respect to rotation relative to one another, wherein a groove (10) for receiving a blade root (14) of at least one rotor blade is formed in the separating plane.
摘要翻译：用于流动机械，特别是燃气涡轮机或汽轮机或轴向压缩机的多部分叶片转子（1）具有至少两个彼此面对的前侧彼此连接的盘（2），特别是正的接合在分离平面（7）中，以相对于彼此相对于旋转而固定，其中用于接收至少一个转子叶片的叶根（14）的凹槽（10）形成在分离平面中。

10. 发明申请

US20110052371A1 Multi-Component Bladed Rotor for a Turbomachine 有权
标题翻译：用于涡轮机的多组分叶片转子
公开(公告)号：US20110052371A1
公开(公告)日：2011-03-03
申请号：US12812862
申请日：2008-12-11
申请人： Emil Aschenbruck , Michael Blaswich , Andreas Kleinefeldt , William F. Cline
发明人： Emil Aschenbruck , Michael Blaswich , Andreas Kleinefeldt , William F. Cline
IPC分类号： F04D25/16 , F01D5/30
CPC分类号： F01D5/3038 , F01D5/06 , F01D5/066 , F01D5/3069 , F05D2240/20 , F05D2260/30 , F05D2260/36
摘要： A multipart bladed rotor (1) for a flow machine, particularly a gas turbine or steam turbine or an axial compressor, has at least two disks (2) whose front sides, which face one another, are connected to one another, particularly by positive engagement, in a separating plane (7) so as to be fixed with respect to rotation relative to one another, wherein a groove (10) for receiving a blade root (14) of at least one rotor blade is formed in the separating plane.
摘要翻译：用于流动机械，特别是燃气涡轮机或汽轮机或轴向压缩机的多部分叶片转子（1）具有至少两个彼此面对的前侧彼此连接的盘（2），特别是正的接合在分离平面（7）中，以相对于彼此相对于旋转而固定，其中用于接收至少一个转子叶片的叶根（14）的凹槽（10）形成在分离平面中。

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