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1.发明申请公开(公告)号：US20050100445A1
公开(公告)日：2005-05-12
申请号：US10936487
申请日：2004-09-09
CPC分类号： F01D25/285 , B23P6/002 , B23P19/025 , B25B27/023 , F01D5/005 , F01D5/323 , F05D2230/70
摘要： A rotor blade (1) for a flow machine includes an aerodynamic blade (2) and a foot (3). The foot (3) has an anchoring section (5) on a side facing away from the blade (2). A rotor (4) of the flow machine has an axial anchoring groove (6) which is complementary to the anchoring section (5). The anchoring section (5) can be inserted axially into the anchoring groove (6) in order to radially attach the rotor blade (1) to the rotor (4). At least one pulling-off contour (7) is formed on the foot (3), via which an axial pulling-off force can be introduced into the rotor blade (1), which is attached to the rotor (4) with the aid of a pulling-off tool (15) which is complementary to this pulling-off contour (7).
摘要翻译： 用于流动机器的转子叶片（1）包括空气动力学叶片（2）和脚部（3）。 脚（3）在远离叶片（2）的一侧具有锚定部分（5）。 流动机的转子（4）具有与锚定部分（5）互补的轴向锚定槽（6）。 锚定部分（5）可以轴向地插入到锚定槽（6）中，以将转子叶片（1）径向地附接到转子（4）。 至少一个脱落轮廓（7）形成在脚部（3）上，通过该至少一个牵引轮廓可以将轴向牵引力引入到转子叶片（1）中，该转子叶片（1）借助于辅助 与所述脱离轮廓（7）互补的拉脱工具（15）。
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2.发明授权公开(公告)号：US07128537B2
公开(公告)日：2006-10-31
申请号：US10936487
申请日：2004-09-09
IPC分类号： F01D5/30
CPC分类号： F01D25/285 , B23P6/002 , B23P19/025 , B25B27/023 , F01D5/005 , F01D5/323 , F05D2230/70
摘要： A rotor blade (1) for a flow machine includes an aerodynamic blade (2) and a foot (3). The foot (3) has an anchoring section (5) on a side facing away from the blade (2). A rotor (4) of the flow machine has an axial anchoring groove (6) which is complementary to the anchoring section (5). The anchoring section (5) can be inserted axially into the anchoring groove (6) in order to radially attach the rotor blade (1) to the rotor (4). At least one pulling-off contour (7) is formed on the foot (3), via which an axial pulling-off force can be introduced into the rotor blade (1), which is attached to the rotor (4) with the aid of a pulling-off tool (15) which is complementary to this pulling-off contour (7).
摘要翻译： 用于流动机器的转子叶片（1）包括空气动力学叶片（2）和脚部（3）。 脚（3）在远离叶片（2）的一侧具有锚定部分（5）。 流动机的转子（4）具有与锚定部分（5）互补的轴向锚定槽（6）。 锚定部分（5）可以轴向地插入到锚定槽（6）中，以将转子叶片（1）径向地附接到转子（4）。 至少一个脱落轮廓（7）形成在脚部（3）上，通过该至少一个牵引轮廓可以将轴向牵引力引入到转子叶片（1）中，该转子叶片（1）借助于辅助 与所述脱离轮廓（7）互补的拉脱工具（15）。
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公开(公告)号：US07665957B2
公开(公告)日：2010-02-23
申请号：US11859963
申请日：2007-09-24
IPC分类号： F01D25/26
CPC分类号： F01D25/246 , F01D11/005 , F01D11/24
摘要： A heat shield arrangement for local separation of a flow channel within a turbine engine, with respect to a stator housing radially surrounding the flow channel is provided. The heat shield includes two axially opposite joining contours which are each engageable with two components which are axially adjacent along the flow channel. Each provides a complementary reception contour for the joining contours. At least one of the reception contours has an axial clearance, in which the associated joining contour is axially displaceably mounted. At least one seal is provided between the axially displaceable joining contour and the reception contour. The seal is mounted movably within the reception contour or the joining contour in such a way that the seal is deflectable against a surface region of the reception contour or of the joining contour.
摘要翻译： 提供了一种用于在涡轮发动机内部相对于径向围绕流动通道的定子壳体局部分离涡流发动机的隔热罩装置。 隔热罩包括两个轴向相对的接合轮廓，每个轮廓可与沿着流动通道轴向相邻的两个部件接合。 每个为接合轮廓提供互补的接收轮廓。 接收轮廓中的至少一个具有轴向间隙，其中相关联的接合轮廓轴向可移动地安装。 在可轴向移动的接合轮廓和接收轮廓之间提供至少一个密封件。 密封件可移动地安装在接收轮廓或接合轮廓内，使得密封件可抵靠接收轮廓或接合轮廓的表面区域偏转。
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公开(公告)号：US08137069B2
公开(公告)日：2012-03-20
申请号：US12638580
申请日：2009-12-15
IPC分类号： F01D5/18
CPC分类号： F01D5/187 , F01D5/147 , F05D2230/21 , F05D2250/185 , Y10T29/49336 , Y10T29/49988
摘要： A cast turbine blade is disclosed and includes an internal cooling passage that passes (e.g., zig-zags or meanders) through the blade from an inlet in the blade root to an outlet in the blade tip. The cooling passage can have a zone at a bend that is at a distance which is remote from the inlet of the cooling passage when the distance from the inlet is measured around the passage, but that is closer to the inlet when the distance from the inlet is measured in a straight line. During casting of the blade, the cooling passage can be defined by a core or cores having a leachable material, the cores being removed after casting by a chemical leaching process. A supplementary passage is also provided for connecting the remote zone to the inlet during the leaching process. The supplementary passage can likewise be defined by a leachable core, or it may be machined into the blade after casting. During the service life of the blade, a plug can be used to obturate the supplementary passage to prevent leakage of cooling air from the cooling passage through the supplementary passage.
摘要翻译： 公开了一种铸造涡轮机叶片，并且包括内部冷却通道，该内部冷却通道（例如，锯齿形或曲折形）通过叶片从叶片根部中的入口到叶片尖端中的出口。 冷却通道可以具有弯曲处的区域，该区域距离冷却通道的入口远离入口处的距离，当距通道的距离被测量时，距离入口的距离更靠近入口 以直线测量。 在铸造叶片期间，冷却通道可由具有可浸出材料的芯或芯组成，芯通过化学浸出工艺浇铸后除去。 还提供了补充通道，用于在浸出过程中将远程区域连接到入口。 辅助通道同样可以由可浸出的芯部限定，也可以在铸造后被加工成刀片。 在叶片的使用寿命期间，可以使用塞子来堵塞补充通道，以防止冷却空气从冷却通道通过补充通道泄漏。
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公开(公告)号：US20100047062A1
公开(公告)日：2010-02-25
申请号：US12579464
申请日：2009-10-15
IPC分类号： F01D5/08
CPC分类号： F01D11/08 , F05D2240/11 , F05D2240/57 , F05D2260/201 , F05D2260/22141
摘要： A stator heat shield (6) for a gas turbine (1) includes an outside (11) which in the installed state faces a hot gas path (9) of the gas turbine (1), and an inside (12) facing away from the outside (11). A plurality of ribs (13) are formed on the inside (12) and extend axially in the installed state with regard to an axis of rotation (8) of a rotor (3) of the gas turbine (1) and, in the circumferential direction, are spaced a distance apart from one another. At least one baffle plate (14) is arranged on the inside (12) and is in contact with the ribs (13). At least one groove (16) is designed in an end face (15) bordering the stator heat shield (6) in the circumferential direction, into which at least one sealing element (18) can be inserted. A plurality of bores (19) are included, each opening at a distance from the groove (16) in the direction of the outside (11) at the inside (12) at one end and on the end face (15) at the other end and arranged a distance apart from one another in the axial direction.
摘要翻译： 一种用于燃气轮机（1）的定子隔热罩（6）包括：外部（11），其处于安装状态，面对燃气轮机（1）的热气路径（9）;以及内部（12） 外面（11）。 多个肋（13）形成在内侧（12）上，并且相对于燃气轮机（1）的转子（3）的旋转轴线（8）在安装状态下轴向延伸，并且在周向 方向彼此隔开一段距离。 至少一个挡板（14）设置在内部（12）上并与肋（13）接触。 至少一个凹槽（16）被设计在沿圆周方向邻接定子隔热罩（6）的端面（15）中，至少一个密封元件（18）可插入该凹槽中。 包括多个孔（19），每个孔在一端处在一个端部处和在另一端的端面（15）处沿着外部（11）的方向在一个距离槽（16）处一定距离处 并且在轴向方向上彼此分开设置一段距离。
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公开(公告)号：US20080260524A1
公开(公告)日：2008-10-23
申请号：US11859963
申请日：2007-09-24
IPC分类号： F01D25/12
CPC分类号： F01D25/246 , F01D11/005 , F01D11/24
摘要： A heat shield arrangement for local separation of a flow channel within a turbine engine, with respect to a stator housing radially surrounding the flow channel is provided. The heat shield includes two axially opposite joining contours which are each engageable with two components which are axially adjacent along the flow channel. Each provides a complementary reception contour for the joining contours. At least one of the reception contours has an axial clearance, in which the associated joining contour is axially displaceably mounted. At least one seal is provided between the axially displaceable joining contour and the reception contour. The seal is mounted movably within the reception contour or the joining contour in such a way that the seal is deflectable against a surface region of the reception contour or of the joining contour.
摘要翻译： 提供了一种用于在涡轮发动机内部相对于径向围绕流动通道的定子壳体局部分离涡流发动机的隔热罩装置。 隔热罩包括两个轴向相对的接合轮廓，每个轮廓可与沿着流动通道轴向相邻的两个部件接合。 每个为接合轮廓提供互补的接收轮廓。 接收轮廓中的至少一个具有轴向间隙，其中相关联的接合轮廓轴向可移动地安装。 在可轴向移动的接合轮廓和接收轮廓之间提供至少一个密封件。 密封件可移动地安装在接收轮廓或接合轮廓内，使得密封件可抵靠接收轮廓或接合轮廓的表面区域偏转。
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公开(公告)号：US07997856B2
公开(公告)日：2011-08-16
申请号：US12579464
申请日：2009-10-15
IPC分类号： F01D5/08
CPC分类号： F01D11/08 , F05D2240/11 , F05D2240/57 , F05D2260/201 , F05D2260/22141
摘要： A stator heat shield (6) for a gas turbine (1) includes an outside (11) which in the installed state faces a hot gas path (9) of the gas turbine (1), and an inside (12) facing away from the outside (11). A plurality of ribs (13) are formed on the inside (12) and extend axially in the installed state with regard to an axis of rotation (8) of a rotor (3) of the gas turbine (1) and, in the circumferential direction, are spaced a distance apart from one another. At least one baffle plate (14) is arranged on the inside (12) and is in contact with the ribs (13). At least one groove (16) is designed in an end face (15) bordering the stator heat shield (6) in the circumferential direction, into which at least one sealing element (18) can be inserted. A plurality of bores (19) are included, each opening at a distance from the groove (16) in the direction of the outside (11) at the inside (12) at one end and on the end face (15) at the other end and arranged a distance apart from one another in the axial direction.
摘要翻译： 一种用于燃气轮机（1）的定子隔热罩（6）包括：外部（11），其处于安装状态，面对燃气轮机（1）的热气路径（9）;以及内部（12） 外面（11）。 多个肋（13）形成在内侧（12）上，并且相对于燃气轮机（1）的转子（3）的旋转轴线（8）在安装状态下轴向延伸，并且在周向 方向彼此隔开一段距离。 至少一个挡板（14）设置在内部（12）上并与肋（13）接触。 至少一个凹槽（16）被设计在沿圆周方向邻接定子隔热罩（6）的端面（15）中，至少一个密封元件（18）可插入该凹槽中。 包括多个孔（19），每个孔在一端处在一个端部处和在另一端的端面（15）处沿着外部（11）的方向在一个距离槽（16）处一定距离处 并且在轴向方向上彼此分开设置一段距离。
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公开(公告)号：US07665958B2
公开(公告)日：2010-02-23
申请号：US11860099
申请日：2007-09-24
申请人： Alexander Khanin , Edouard Sloutski
发明人： Alexander Khanin , Edouard Sloutski
IPC分类号： F01D25/26
CPC分类号： F01D11/18 , F01D25/246 , F05D2240/11
摘要： A heat accumulation segment for local separation of a flow duct inside a turbo engine, from a stator housing that radially surrounds the flow duct is provided. The heat accumulation segment includes two axially opposed joining contoured elements that are engagable with two components that are axially adjacent along the flow duct. A first one of the two joining contoured elements has a radially oriented recess with a contoured surface against which a securing pin having an external contour complementary to the contoured surface acts radially under force action from a component that adjoins the first joining contoured element. The first joining contoured element has a collar portion having radially upper and lower collar surfaces, and the collar portion is connected within a counter-contoured receiving contoured element in the axially adjacent component by a joining force that acts between the securing pin and the conical contoured surface.
摘要翻译： 提供了一种用于将涡轮发动机内的流动管道与径向围绕流动管道的定子壳体局部分离的热积聚段。 热积聚段包括两个轴向相对的接合轮廓元件，其可与沿着流动管道轴向相邻的两个部件接合。 两个接合轮廓元件中的第一个具有带有轮廓表面的径向定向的凹部，固定销具有与轮廓表面互补的外部轮廓，该紧固销在与来自与第一接合轮廓元件相邻的部件的力作用下径向作用。 第一接合轮廓元件具有轴环部分，其具有径向上部和下部轴环表面，并且轴环部分通过接合力连接在轴向相邻部件中的反轮廓接收轮廓元件内，该接合力作用在固定销和锥形轮廓 表面。
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公开(公告)号：US06857639B2
公开(公告)日：2005-02-22
申请号：US10611941
申请日：2003-07-03
CPC分类号： F16J15/0887 , F01D11/005
摘要： The invention relates to a gap seal (6) for sealing a gap (3) between two adjacent components (1, 2), in particular of turbo machines, with the following characteristics: each component (1) has one each groove (7) that is open towards the gap (3), the two grooves (7) are essentially facing each other in the gap (3), in each groove (7), a compensation body (16) is movably positioned transversely to the longitudinal groove direction and parallel to the gap plane (10), each compensation body (11) abuts the groove bottom (9) of the corresponding groove (7) in a sealing manner, each compensation body (11) has a V-shaped receiving groove (14) that is open towards the facing compensation body (11), a mutual sealing body (16) has a rhombus-shaped cross-section and projects with outer sides (17) into both receiving grooves (14), the straight inner sides (15) of each receiving groove (14) are angled towards each other at the same angle as the straight outer sides (17), in each receiving groove (14), at least one outer side (17) of the sealing body (16) abuts the corresponding inner side (15) of the receiving groove (14) with surface contact and in a sealing manner.
摘要翻译： 本发明涉及一种用于密封两个相邻部件（1,2）（特别是涡轮机）之间的间隙（3）的间隙密封（6），具有以下特征：每个部件（1）具有一个每个凹槽（7） 向间隙（3）开口，两个槽（7）在间隙（3）中基本上彼此面对，在每个槽（7）中，补偿体（16）可以横向于纵向槽方向 并且平行于间隙平面（10），每个补偿体（11）以密封方式与相应的凹槽（7）的凹槽底部（9）邻接，每个补偿体（11）具有V形接收凹槽（14） ）向相对的补偿体（11）开口，相互密封体（16）具有菱形的横截面并与外侧（17）突出成两个容纳槽（14），直内侧（15） 每个接收槽（14）在每个接收槽（14）中以与直的外侧（17）相同的角度彼此成角度，在 密封体（16）的至少一个外侧（17）以表面接触和密封方式与接收槽（14）的相应的内侧（15）邻接。
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公开(公告)号：US07658593B2
公开(公告)日：2010-02-09
申请号：US11859984
申请日：2007-09-24
申请人： Alexander Khanin , Edouard Sloutski
发明人： Alexander Khanin , Edouard Sloutski
IPC分类号： F01D25/26
CPC分类号： F01D11/24 , F05D2230/64 , F05D2230/642 , F05D2230/644 , F05D2240/11
摘要： A heat accumulation segment for local separation of a flow duct inside a turbo engine, from a stator housing that radially surrounds the flow duct is provided. The heat accumulation segment includes two axially opposed joining contoured elements that are engageable with two components that are axially adjacent along the flow duct. A first one of the two joining contoured elements has a radially oriented recess with a frustoconical contoured surface against which a securing pin having a frustoconical external contour that acts radially under force action from a component that adjoins the first joining contoured element, and the first joining contoured element has a collar portion having a radially upper collar surface and a radially lower collar surface. The collar portion is connected within a counter-contoured receiving contoured element in the axially adjacent component by a joining force that acts between the securing pin and the frustoconical contoured surface.
摘要翻译： 提供了一种用于将涡轮发动机内的流动管道与径向围绕流动管道的定子壳体局部分离的热积聚段。 热积聚段包括两个轴向相对的接合轮廓元件，其可与沿着流动管道轴向相邻的两个部件接合。 两个连接轮廓元件中的第一个具有径向定向的凹陷，其具有截头圆锥形轮廓表面，固定销具有截头圆锥形外部轮廓，该截面圆锥形外部轮廓在与邻接第一接合轮廓元件的部件的力作用下径向作用，并且第一连接 轮廓元件具有凸缘部分，其具有径向上部凸缘表面和径向下部凸缘表面。 轴环部分通过作用在固定销和截头圆锥形轮廓表面之间的接合力连接在轴向相邻部件中的反轮廓接收轮廓元件内。
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