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1. 发明申请

US20070154301A1 Device for support of an adjusting ring which encompasses at a distance a circular blade carrier 有权
标题翻译：用于支撑围绕圆形叶片载体的距离的调节环的装置
公开(公告)号：US20070154301A1
公开(公告)日：2007-07-05
申请号：US11649141
申请日：2007-01-03
申请人： Martin Hartmann , Alexandra Kupper , Walter Loch , Vadim Shevchenko
发明人： Martin Hartmann , Alexandra Kupper , Walter Loch , Vadim Shevchenko
IPC分类号： F04D29/56
CPC分类号： F04D29/563 , F01D17/162 , F05D2260/50
摘要： The invention relates to a device for support of an adjusting ring which encompasses at a distance a basically circular blade carrier, which adjusting ring is rotatable in the circumferential direction around a center axis which is identical with the blade carrier, in order to adjust radially extending blades of a ring of a turbo-engine, wherein a plurality of levers are provided between the blade carrier and the adjusting ring, which levers are distributed over the circumference, extend tangentially in each case, and which on their free ends have a rotatable roller in each case, which are rollable in the circumferential direction on the adjusting ring or on the blade carrier. According to the invention, the lever is tightly clamped on one side to disclose a wear-free and reliable device for support of an adjusting ring which encompasses at a distance a circular blade carrier.
摘要翻译：本发明涉及一种用于支撑调节环的装置，该调节环围绕基本上圆形的叶片载体包围该调节环，该调节环围绕与叶片承载件相同的中心轴在圆周方向上旋转，以便调节径向延伸涡轮发动机的环的叶片，其中多个杆设置在叶片载体和调节环之间，该杆在圆周上分布，在每种情况下相切地延伸，并且其自由端具有可旋转辊在各种情况下，其可以在调节环上或在叶片载体上在圆周方向上可滚动。根据本发明，杠杆紧紧地夹紧在一侧以公开一种无磨损和可靠的装置，用于支撑围绕圆形叶片载体的距离的调节环。

2. 发明授权

US07828516B2 Device for support of an adjusting ring which encompasses at a distance a circular blade carrier 有权
标题翻译：用于支撑围绕圆形叶片载体的距离的调节环的装置
公开(公告)号：US07828516B2
公开(公告)日：2010-11-09
申请号：US11649141
申请日：2007-01-03
申请人： Martin Hartmann , Alexandra Küpper , Walter Loch , Vadim Shevchenko
发明人： Martin Hartmann , Alexandra Küpper , Walter Loch , Vadim Shevchenko
IPC分类号： F01D17/16 , F04D29/56
CPC分类号： F04D29/563 , F01D17/162 , F05D2260/50
摘要： The invention relates to a device for support of an adjusting ring which encompasses at a distance a basically circular blade carrier, which adjusting ring is rotatable in the circumferential direction around a center axis which is identical with the blade carrier, in order to adjust radially extending blades of a ring of a turbo-engine, wherein a plurality of levers are provided between the blade carrier and the adjusting ring, which levers are distributed over the circumference, extend tangentially in each case, and which on their free ends have a rotatable roller in each case, which are rollable in the circumferential direction on the adjusting ring or on the blade carrier. According to the invention, the lever is tightly clamped on one side to disclose a wear-free and reliable device for support of an adjusting ring which encompasses at a distance a circular blade carrier.
摘要翻译：本发明涉及一种用于支撑调节环的装置，该调节环围绕基本上圆形的叶片载体包围该调节环，该调节环围绕与叶片承载件相同的中心轴在圆周方向上旋转，以便调节径向延伸涡轮发动机的环的叶片，其中多个杆设置在叶片载体和调节环之间，该杆在圆周上分布，在每种情况下相切地延伸，并且其自由端具有可旋转辊在各种情况下，其可以在调节环上或在叶片载体上在圆周方向上可滚动。根据本发明，杠杆紧紧地夹紧在一侧以公开一种无磨损和可靠的装置，用于支撑围绕圆形叶片载体的距离的调节环。

3. 发明申请

US20090021247A1 Device for determining the angular position of a rotatable compressor stator blade 有权
标题翻译：用于确定可旋转压缩机定子叶片的角位置的装置
公开(公告)号：US20090021247A1
公开(公告)日：2009-01-22
申请号：US11895929
申请日：2007-08-28
申请人： Joachim Braun , Walter Loch , Bernd Pollack , Vadim Shevchenko , Joachim Simmchen
发明人： Joachim Braun , Walter Loch , Bernd Pollack , Vadim Shevchenko , Joachim Simmchen
IPC分类号： G01B7/30
CPC分类号： G01B11/26 , F01D17/162 , F01D21/003 , F02C7/042 , F04D29/563
摘要： The invention refers to a device for determining the angular position of a compressor stator blade, which is rotatable around its longitudinal axis and arranged in a compressor, with which is associated a measuring surface which rotates synchronously with it. For a reliable, simple and approximately error-free recording of the angular positions, the angular position of the compressor stator blade can be determined via the device in an automated manner. For this purpose, it has at least one mounting unit provided for aligned fastening of the device on the compressor, and at least one measuring and evaluating unit which comprises at least two distance sensors which each record a distance to the measuring surface which is rotatable from the reference position, as a result the angular position of the measuring surface, relative to the reference position depends upon the two recorded distances, is determined by the measuring and evaluating unit.
摘要翻译：本发明涉及一种用于确定压缩机定子叶片的角位置的装置，该压缩机定子叶片可围绕其纵向轴线旋转并且布置在压缩机中，该压缩机与其同步旋转的测量表面相关联。为了可靠，简单且近乎无差错地记录角位置，压缩机定子叶片的角位置可以通过装置自动确定。为此，其具有至少一个安装单元，用于将装置对准地紧固在压缩机上，以及至少一个测量和评估单元，其包括至少两个距离传感器，每个距离传感器记录与测量表面的距离，该距离传感器可从参考位置，因此测量表面相对于参考位置的角度位置取决于两个记录的距离，由测量和评估单元确定。

4. 发明授权

US07700907B2 Device for determining the angular position of a rotatable compressor stator blade 有权
标题翻译：用于确定可旋转压缩机定子叶片的角位置的装置
公开(公告)号：US07700907B2
公开(公告)日：2010-04-20
申请号：US11895929
申请日：2007-08-28
申请人： Joachim Braun , Walter Loch , Bernd Pollack , Vadim Shevchenko , Joachim Simmchen
发明人： Joachim Braun , Walter Loch , Bernd Pollack , Vadim Shevchenko , Joachim Simmchen
IPC分类号： G01D5/34
CPC分类号： G01B11/26 , F01D17/162 , F01D21/003 , F02C7/042 , F04D29/563
摘要： The invention refers to a device for determining the angular position of a compressor stator blade, which is rotatable around its longitudinal axis and arranged in a compressor, with which is associated a measuring surface which rotates synchronously with it. For a reliable, simple and approximately error-free recording of the angular positions, the angular position of the compressor stator blade can be determined via the device in an automated manner. For this purpose, it has at least one mounting unit provided for aligned fastening of the device on the compressor, and at least one measuring and evaluating unit which comprises at least two distance sensors which each record a distance to the measuring surface which is rotatable from the reference position, as a result the angular position of the measuring surface, relative to the reference position depends upon the two recorded distances, is determined by the measuring and evaluating unit.
摘要翻译：本发明涉及一种用于确定压缩机定子叶片的角位置的装置，该压缩机定子叶片可围绕其纵向轴线旋转并且布置在压缩机中，该压缩机与其同步旋转的测量表面相关联。为了可靠，简单且近乎无差错地记录角位置，压缩机定子叶片的角位置可以通过装置自动确定。为此，其具有至少一个安装单元，用于将装置对准地紧固在压缩机上，以及至少一个测量和评估单元，其包括至少两个距离传感器，每个距离传感器记录与测量表面的距离，该距离传感器可从参考位置，因此测量表面相对于参考位置的角度位置取决于两个记录的距离，由测量和评估单元确定。

5. 发明授权

US07455505B2 Device for the demounting of blades of a turbine or of a compressor 失效
标题翻译：用于拆卸涡轮机或压缩机的叶片的装置
公开(公告)号：US07455505B2
公开(公告)日：2008-11-25
申请号：US11176452
申请日：2005-07-07
申请人： Martin Hartmann , Werner Polanz , Sabine Rintzel , Peter Schröder , Vadim Shevchenko , Thomas-Dieter Tenrahm , Bernd Vonnemann
发明人： Martin Hartmann , Werner Polanz , Sabine Rintzel , Peter Schröder , Vadim Shevchenko , Thomas-Dieter Tenrahm , Bernd Vonnemann
IPC分类号： F03D11/00
CPC分类号： B23P6/002 , B23P19/025 , F01D5/005 , F01D5/3007 , F05D2230/60 , F05D2230/70 , Y10T29/49318
摘要： A device (10) for the demounting of blades (12), which are pushed in with a blade root (20) on a wheel disk (14) of a blade wheel (16) of a turbine or of a compressor, is designed with a support (24) which is designed to be brought to bear against at least one component of the turbine, and is designed with an actuator (28) which is coupled to the support (24) and is designed for moving the blade root (20) mechanically out of the wheel disk (14).
摘要翻译：用于拆卸叶片（12）的装置（10）被设计成具有用叶轮根部（20）推入涡轮机或压缩机的叶轮（16）的轮盘（14）上的装置（10）被设计成承受涡轮机的至少一个部件的支撑件（24），并且被设计成具有联接到所述支撑件（24）并且被设计成用于移动所述叶片根部（20）的致动器（28））机械地离开轮盘（14）。

6. 发明申请

US20110268580A1 Axially segmented guide vane mount for a gas turbine 有权
标题翻译：用于燃气轮机的轴向分段导叶架
公开(公告)号：US20110268580A1
公开(公告)日：2011-11-03
申请号：US13127295
申请日：2009-09-10
申请人： Roderich Bryk , Sascha Dungs , Martin Hartmann , Uwe Kahlstorf , Karl Klein , Oliver Lüsebrink , Mirko Milazar , Nicolas Savilius , Oliver Schneider , Shilun Sheng , Vadim Shevchenko , Gerhard Simon , Norbert Thamm
发明人： Roderich Bryk , Sascha Dungs , Martin Hartmann , Uwe Kahlstorf , Karl Klein , Oliver Lüsebrink , Mirko Milazar , Nicolas Savilius , Oliver Schneider , Shilun Sheng , Vadim Shevchenko , Gerhard Simon , Norbert Thamm
IPC分类号： F04D29/00
CPC分类号： F01D9/041 , F01D25/246
摘要： A stator blade carrier for a gas turbine is provided. The stator blade carrier includes a plurality of axial segments. At least one axial segment is designed as a tubular lattice structure. This allows a simpler design technically and a more flexible adaptation to the temperature profile present on the stator blade carrier to maintain operational safety.
摘要翻译：提供了一种用于燃气轮机的定子叶片载体。定子叶片载体包括多个轴向段。至少一个轴向段被设计为管状晶格结构。这允许在技术上更简单的设计和更灵活地适应定子叶片载体上存在的温度分布，以保持操作安全性。

7. 发明授权

US08870526B2 Axially segmented guide vane mount for a gas turbine 有权
标题翻译：用于燃气轮机的轴向分段导叶架
公开(公告)号：US08870526B2
公开(公告)日：2014-10-28
申请号：US13127295
申请日：2009-09-10
申请人： Roderich Bryk , Sascha Dungs , Martin Hartmann , Uwe Kahlstorf , Karl Klein , Oliver Lüsebrink , Mirko Milazar , Nicolas Savilius , Oliver Schneider , Shilun Sheng , Vadim Shevchenko , Gerhard Simon , Norbert Thamm
发明人： Roderich Bryk , Sascha Dungs , Martin Hartmann , Uwe Kahlstorf , Karl Klein , Oliver Lüsebrink , Mirko Milazar , Nicolas Savilius , Oliver Schneider , Shilun Sheng , Vadim Shevchenko , Gerhard Simon , Norbert Thamm
IPC分类号： F01D25/24 , F01D9/04
CPC分类号： F01D9/041 , F01D25/246
摘要： A stator blade carrier for a gas turbine is provided. The stator blade carrier includes a plurality of axial segments. At least one axial segment is designed as a tubular lattice structure. This allows a simpler design technically and a more flexible adaptation to the temperature profile present on the stator blade carrier to maintain operational safety.
摘要翻译：提供了一种用于燃气轮机的定子叶片载体。定子叶片载体包括多个轴向段。至少一个轴向段被设计为管状晶格结构。这允许在技术上更简单的设计和更灵活地适应定子叶片载体上存在的温度分布，以保持操作安全性。

8. 发明申请

US20060039790A1 Device for the demounting of blades of a turbine or of a compressor 失效
标题翻译：用于拆卸涡轮机或压缩机的叶片的装置
公开(公告)号：US20060039790A1
公开(公告)日：2006-02-23
申请号：US11176452
申请日：2005-07-07
申请人： Martin Hartmann , Werner Polanz , Sabine Rintzel , Peter Schroder , Vadim Shevchenko , Thomas-Dieter Tenrahm , Bernd Vonnemann
发明人： Martin Hartmann , Werner Polanz , Sabine Rintzel , Peter Schroder , Vadim Shevchenko , Thomas-Dieter Tenrahm , Bernd Vonnemann
IPC分类号： F01D5/30
CPC分类号： B23P6/002 , B23P19/025 , F01D5/005 , F01D5/3007 , F05D2230/60 , F05D2230/70 , Y10T29/49318
摘要： A device (10) for the demounting of blades (12), which are pushed in with a blade root (20) on a wheel disk (14) of a blade wheel (16) of a turbine or of a compressor, is designed with a supporting means (24) which is designed to be brought to bear against at least one component of the turbine, and is designed with an actuator means (28) which is coupled to the supporting means (24) and is designed for moving the blade root (20) mechanically out of the wheel disk (14).
摘要翻译：用于拆卸叶片（12）的装置（10）被设计成具有用叶轮根部（20）推入涡轮机或压缩机的叶轮（16）的轮盘（14）上的装置（10）被设计成承受涡轮机的至少一个部件的支撑装置（24），并且被设计成具有联接到支撑装置（24）的致动器装置（28），并被设计成用于使叶片根部（20）机械地离开轮盘（14）。

9. 发明申请

US20130216359A1 COMPRESSOR 审中-公开
标题翻译：压缩机
公开(公告)号：US20130216359A1
公开(公告)日：2013-08-22
申请号：US13808117
申请日：2011-07-07
申请人： Thomas Brandenburg , Daniel Ecke , Markus Hofmann , Torsten Matthias , Bernward Mertens , Frank Mildner , Markus Paus , Achim Schirrmacher , Vadim Shevchenko , Uwe Sieber , Hubertus Michael Wigger
发明人： Thomas Brandenburg , Daniel Ecke , Markus Hofmann , Torsten Matthias , Bernward Mertens , Frank Mildner , Markus Paus , Achim Schirrmacher , Vadim Shevchenko , Uwe Sieber , Hubertus Michael Wigger
IPC分类号： F01D9/04
CPC分类号： F01D9/041 , F01D17/162 , F04D29/563
摘要： An axial compressor is provided. The compressor has an annular flow channel, in which adjustable blades of a blade ring that extend through the flow channel are rotatably mounted. Each blade has a lug on the rotor-side of the vane for mounting an inner ring. In order to provide a wear-free, self-centering inner ring, the ring is designed as a split ring with two opposing ends and a spring element for spreading the split ring.
摘要翻译：提供轴流式压缩机。压缩机具有环形流动通道，其中延伸穿过流动通道的叶片环的可调叶片可旋转地安装。每个叶片在叶片的转子侧具有用于安装内圈的凸耳。为了提供无磨损，自定心的内圈，环被设计为具有两个相对端的开口环和用于扩展开口环的弹簧元件。

10. 发明申请

US20110236184A1 Axial Compressor for a Gas Turbine Having Passive Radial Gap Control 审中-公开
标题翻译：用于具有被动径向间隙控制的燃气轮机的轴向压缩机
公开(公告)号：US20110236184A1
公开(公告)日：2011-09-29
申请号：US13132126
申请日：2009-11-18
申请人： Francois Benkler , Karl Klein , Torsten Matthias , Achim Schirrmacher , Oliver Schneider , Vadim Shevchenko
发明人： Francois Benkler , Karl Klein , Torsten Matthias , Achim Schirrmacher , Oliver Schneider , Vadim Shevchenko
IPC分类号： F01D25/26
CPC分类号： F01D11/001 , F01D11/005 , F01D11/025 , F05D2230/90 , F05D2300/5021 , F05D2300/50211
摘要： An axial compressor for a gas turbine having passive radial gap control is provided. The axial compressor includes a guide vane support on which guide vanes are fastened so as to be arranged in a ring, wherein the vane tips of the guide vanes lie opposite a wall section. Thermal insulation is attached to the wall section in the section lying opposite the vane tips in order to equalize the expansion behavior of the guide vane support and the wall section, which by themselves react thermally in different manners, wherein the terminal insulation is matched in the heat input delay effect thereof to the wall section and to the guide vane support in such a way that the thermal expansion behavior of the guide vane support and the wall section is at least equalized over time during transient operation of the axial compressor.
摘要翻译：提供一种用于具有被动径向间隙控制的燃气轮机的轴向压缩机。轴流式压缩机包括导向叶片支撑件，导向叶片紧固在该导向叶片支架上，以便布置成环形，其中导向叶片的叶片顶端与壁部分相对。隔热件安装在与叶片尖端相对的部分中的壁部分上，以便均衡引导叶片支撑件和壁部分的膨胀特性，壁部分本身以不同的方式热反应，其中端子绝缘体在导热叶片支撑件和导向叶片支撑件的热输入延迟效应使得导向叶片支撑件和壁部分的热膨胀特性在轴向压缩机的瞬时操作期间至少相当于时间均衡。

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