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1. 发明公开

EP2581146A1 System and method of manufacturing a structure 有权
标题翻译：系统和Verfahren zum Herstellen einer Struktur
公开(公告)号：EP2581146A1
公开(公告)日：2013-04-17
申请号：EP12185032.5
申请日：2012-09-19
申请人： Bell Helicopter Textron Inc.
发明人： Bishop, Stephen K. , Swenson, Stephen S. , Wilson, Crystal L. , Lemond, Paulette D.
IPC分类号： B21D53/78 , B21D35/00 , B23P15/02 , B21H7/16
CPC分类号： B21D53/78 , B21D11/08 , B21D35/002 , B21H7/16 , B23P15/02 , B23P15/04 , B64C11/205 , B64C27/473
摘要： The system and method of the present application can include machining complex part features in a flat metal sheet (401), and subsequently forming the machined flat metal sheet to have the desired shape and contours. Prior to the step (303) of machining the complex part features, the method can include (311) calculating a scaled location of the complex part features so that the subsequent forming step (305) acts to translate and deform the complex part features into a desired location.
摘要翻译：本申请的系统和方法可以包括在扁平金属板（401）中加工复杂部件特征，并且随后形成加工后的平坦金属板以具有期望的形状和轮廓。在加工复杂零件特征的步骤（303）之前，该方法可以包括（311）计算复杂零件特征的缩放位置，使得随后的成形步骤（305）用于将复杂零件特征平移和变形为理想位置。

2. 发明公开

EP1422400A1 VARIABLE BLADE MANUFACTURING METHOD AND VARIABLE BLADE IN VGS TYPE TURBO CHARGER 有权
标题翻译： VERFAHREN ZER HERSTELLUNG VON VERSTELLBAREN SCHAUFELN在VGS-TURBOLADERN
公开(公告)号：EP1422400A1
公开(公告)日：2004-05-26
申请号：EP02755806.3
申请日：2002-08-02
申请人： Akita Fine Blanking Co., Ltd.
发明人： OHISHI, Shinjiroh
IPC分类号： F02B37/12 , F02B39/00 , B21K3/04 , B21H7/16
CPC分类号： B23P15/02 , B21H7/16 , B21K3/04 , F01D17/165 , F02B37/24 , F05D2220/40 , F05D2230/10 , F05D2230/25 , F05D2240/12 , Y02T10/144 , Y10T29/4932 , Y10T29/49336 , Y10T29/49995
摘要： A manufacturing method based on a plastic working technique which can eliminate cutting and welding as much as possible in manufacturing an adjustable blade incorporated in a VGS turbocharger is provided. The present invention is characterized in that: a blank is punched out from a metal material having a substantially constant thickness to be a shaped material (W) as a starting form for an adjustable blade (1); thereafter, the shaped material (W) is compressed between a pair of opposed dies to form a blade portion (11), a shaft portion (12) and the like having desired shapes; thereafter a non-product portion protruding from a product portion is trimmed; then the shaft portion (12) is rolled by pressing the shaft portion (12) of the shaped material (W) against a pair of dies to have a desired diametrical thickness and a near net shape having a shape and dimensions thereof made close to the aimed at adjustable blade; and in finishing the vane height corresponding to a blade width of the adjustable blade (1), the shaped material (W) having the near net shape is pressed by a pair of opposed dies, so that an accuracy of a vane height in a completed state can be achieved.
摘要翻译：提供了一种基于塑料加工技术的制造方法，其可以在制造结合在VGS涡轮增压器中的可调节叶片时尽可能地消除切割和焊接。本发明的特征在于：将坯料从具有基本上恒定厚度的金属材料冲压成成形材料（W），作为可调叶片（1）的起始形式; 此后，成形材料（W）被压缩在一对相对的模具之间以形成具有期望形状的叶片部分（11），轴部分（12）等; 之后修剪从产品部分突出的非产品部分; 然后通过将成形材料（W）的轴部分（12）压靠在一对模具上而使轴部分（12）具有期望的直径厚度，并且其形状和尺寸接近于针对可调叶片; 并且在完成对应于可调叶片（1）的叶片宽度的叶片高度时，具有近净形状的成形材料（W）被一对相对的模具挤压，使得叶片高度的精度在完成状态可以实现。

3. 发明授权

EP0690768B1 VERFAHREN ZUM FESTWALZEN EINES BAUTEILS 失效
标题翻译：方法为组件的硬ROLLS
公开(公告)号：EP0690768B1
公开(公告)日：1998-07-22
申请号：EP94910332.9
申请日：1994-03-15
申请人： SIEMENS AKTIENGESELLSCHAFT
发明人： SEEGER, Horst , THIELE, Dieter , WAGNER, Hans
IPC分类号： B24B39/00 , C21D7/04 , B21H7/16 , B21H5/02
CPC分类号： B24B39/00 , B21H7/16 , B21H7/18 , B23P9/02 , C21D7/04 , F01D5/286 , F05D2230/26
摘要： The invention relates to a process for hard-rolling a component (2) to be loaded along a load axis (1) in a notch (3) running approximately parallel to the load axis (1) and having a minimum radius of curvature (4) to be determined in a cross-section parallel to the load axis (1). The notch (3) is hard-rolled over a plurality of adjacent paths (5) along the load axis and approximately perpendicular to the load axis (1), each path (5) covers only a part of the notch (3). This generates residual compressive stresses having axial (17) and tangential components (18) in relation to the load axis, with the axial components (17) substantially greater than the tangential components (18). This process is particularly suitable for hard-rolling a retaining groove (3) in the base (11) of a turbine blade (2).

4. 发明公开

EP3338950A1 DEEP ROLLING TOOL AND METHOD 审中-公开
公开(公告)号：EP3338950A1
公开(公告)日：2018-06-27
申请号：EP17204706.0
申请日：2017-11-30
申请人： United Technologies Corporation
发明人： HAWKES, Justin R. , RAMPONE, Joseph C. , EL-WARDANY, Tahany Ibrahim , SALVA, Randy. P , CLAVETTE, Patrick Louis , GAROSSHEN, Thomas J.
IPC分类号： B24B39/04 , B24B27/00 , B24B19/14 , B25J11/00 , B25J9/16 , B24B27/027 , B24B41/00 , B24B41/04 , B21H7/16 , B23P9/02
CPC分类号： C22F1/04 , B21B37/58 , B21H7/16 , B21K3/04 , B23P9/02 , B24B19/14 , B24B27/0038 , B24B27/027 , B24B39/00 , B24B39/04 , B24B41/007 , B24B41/04 , B25J9/1633 , B25J11/005 , B25J13/085 , F05D2230/26
摘要： An embodiment of a tool assembly (31) includes a hub (22) connected to a distal end of a spring-loaded shaft assembly disposed along a first axis (24). An upper hub portion (36A) is adjacent to the distal end of the spring-loaded shaft assembly aligned with the first axis (24), and a lower hub portion (36B) extends along a second axis (34), forming a nonzero angle relative to the first axis (24). A roller disk (20) is joined to the lower portion (36B) of the hub (22), and is rotatable about the second axis (34) parallel to the second portion (36B) of the hub (22). A load cell (60) is disposed along the first axis (24) between a proximal end of the shaft and the roller disk, and is adapted to measure a downward force applied along the shaft assembly.

5. 发明授权

EP1422399B1 VARIABLE BLADE MANUFACTURING METHOD IN VGS TYPE TURBO CHARGER 有权
标题翻译：用于生产可变几何涡轮增压器可调叶片
公开(公告)号：EP1422399B1
公开(公告)日：2012-08-01
申请号：EP02755805.5
申请日：2002-08-02
申请人： Akita Fine Blanking Co., Ltd.
发明人： OHISHI, Shinjiroh
IPC分类号： B23P15/02 , B21H7/16 , F01D17/16 , F02B37/24 , F02C6/12
CPC分类号： F01D17/165 , B21H7/16 , B21K3/04 , B23P15/02 , F02B37/24 , F02C6/12 , F05D2220/40 , F05D2230/26 , F05D2240/12 , Y02T10/144 , Y10T29/49316 , Y10T29/49336 , Y10T29/49337 , Y10T29/49995
摘要： A variable blade manufacturing method capable of realizing the mass-production of not only a variable blade but also a VGS type turbo charger formed by assembling the variable blade therein, comprising the steps of machining shaft parts to a specified diameter by rolling not by cutting to maximally eliminate a time-consuming cutting operation from a variable blade manufacturing process, remarkably suppressing the extension of the shaft parts and sharp edges due to rolling, and eliminating the cutting operation performed so far to correct the extension of the shaft parts and sharp edges, characterized in that a metal material forming the prototype of the variable blade (1) having blade parts (11) and shaft parts (12) formed integrally with each other is formed in the state of a near net shape where the shape and dimensions of the material near the specified variable blades (1), the shaft part forming parts of the material are rolled to a specified diameter to form the shaft part (12).

6. 发明公开

EP1422400A4 VARIABLE BLADE MANUFACTURING METHOD AND VARIABLE BLADE IN VGS TYPE TURBO CHARGER 有权
标题翻译：方法在VGS涡轮增压器产生与可变叶片可调铲
公开(公告)号：EP1422400A4
公开(公告)日：2009-03-04
申请号：EP02755806
申请日：2002-08-02
申请人： AKITA FINE BLANKING CO LTD
发明人： OHISHI SHINJIROH
IPC分类号： B21H7/16 , B21K3/04 , B23P15/02 , F01D17/16 , F02B37/24 , F02B37/12 , F02B39/00
CPC分类号： B23P15/02 , B21H7/16 , B21K3/04 , F01D17/165 , F02B37/24 , F05D2220/40 , F05D2230/10 , F05D2230/25 , F05D2240/12 , Y02T10/144 , Y10T29/4932 , Y10T29/49336 , Y10T29/49995
摘要： A variable blade manufacturing method based on plastic working technology capable of minimizing cutting and welding operations in manufacturing variable blades assembled in a VGS type turbo charger, comprising the steps of punching out a blank material from a metal material with an approximately constant plate thickness to form a raw material (W) forming the prototype of the variable blades (1), holding the raw material (W) by a pair of opposed molds, molding blade parts (11) and shaft parts (12) to specified shapes, trimming non−product portions projected from product portions, pressing the shaft parts (12) of the raw material (W) against a pair of dies to roll to a specified diameter so as to bring the shape and dimensions of the raw material into the state of a near net shape nearing the specified variable blades, characterized in that, when the variable blades (1) are finished to a blade height of the variable blades (1) equal to the blade width dimension of the variable blades (1), the raw material (W) formed in the state of the near net shape is held and pressed by a pair of opposed molds to realize the accuracy of the blade height in a completed state.

7. 发明公开

EP0165195A2 Manufacture of metal vanes for turbomachinery 失效
标题翻译：用于涡轮机械由金属制成的叶片的制备。
公开(公告)号：EP0165195A2
公开(公告)日：1985-12-18
申请号：EP85630063.7
申请日：1985-04-18
申请人： UNITED TECHNOLOGIES CORPORATION
发明人： Griffith, James Bryce , Sanborn, Harold Coffin
IPC分类号： B21D53/78 , B21H7/16
CPC分类号： B21K3/04 , B21B1/0815 , B21H7/16 , B23P15/02 , Y10S29/037 , Y10T29/49336 , Y10T29/49789 , Y10T29/49794
摘要： To make vane airfoils for an axial flow compressor metal strip (34) is first contour rolled to a cross section comprised of two oppposing airfoils (38, 40) separated by a center rib (42), where one (36) of the faces of the strip (34) is kept planar. The rib (42) is used to guide the strip (34) into dies where it is notched and slotted (at 66a, b, c) to define individual airfoils. Next, die stamping makes concave the planar surface (36) of each airfoil.

8. 发明公开

EP3225713A3 METHOD OF FORMING ALUMINUM ALLOY AIRFOILS 有权转让
标题翻译：形成铝合金翼型的方法
公开(公告)号：EP3225713A3
公开(公告)日：2017-12-27
申请号：EP17162173.3
申请日：2017-03-21
申请人： United Technologies Corporation
发明人： PALITSCH, John Richard , HANSEN, James O. , FIGUEIREDO, Nicolas , GYNTHER, Daniel , GRAUSHINSKY, Stephen E. , NORTRUP, John H.
IPC分类号： C22C21/00 , C22F1/04 , F01D5/28
CPC分类号： C22F1/04 , B21H7/16 , C22C21/00 , F01D5/28 , F01D5/30 , F05D2220/32 , F05D2230/20 , F05D2230/90 , F05D2300/173
摘要： A method of forming an airfoil includes placing (102) a material onto a die (10) that is heated (100) to a predetermined temperature to pre-heat (106) the material to a first temperature, while the die is in an open position (104). The method further includes closing (108) the die at a predetermined rate and holding (110) the die in a closed position for a predetermined period of time at a first force. The method still further includes removing (114) the part from the die, cooling (116) the die, placing (124) the part onto the die, and closing (126) the die at a second force.
摘要翻译：形成翼型件的方法包括将材料放置（102）到被加热（100）到预定温度的模具（10）上以预热（106）材料到第一温度，同时模具处于打开位置（104）。该方法还包括以预定速率关闭（108）模具并在第一力下将模具保持（110）关闭位置达预定时间段。该方法还包括从模具中取出（114）零件，冷却（116）模具，将部件放置（124）到模具上，以及在第二力下关闭（126）模具。

9. 发明授权

EP2581146B1 System and method of manufacturing a structure 有权
标题翻译：系统和方法，用于生产结构
公开(公告)号：EP2581146B1
公开(公告)日：2014-01-01
申请号：EP12185032.5
申请日：2012-09-19
申请人： Bell Helicopter Textron Inc.
发明人： Bishop, Stephen K. , Swenson, Stephen S. , Wilson, Crystal L. , Lemond, Paulette D.
IPC分类号： B21D53/78 , B21D35/00 , B23P15/02 , B21H7/16
CPC分类号： B21D53/78 , B21D11/08 , B21D35/002 , B21H7/16 , B23P15/02 , B23P15/04 , B64C11/205 , B64C27/473
摘要： The system and method of the present application can include machining complex part features in a flat metal sheet (401), and subsequently forming the machined flat metal sheet to have the desired shape and contours. Prior to the step (303) of machining the complex part features, the method can include (311) calculating a scaled location of the complex part features so that the subsequent forming step (305) acts to translate and deform the complex part features into a desired location.

10. 发明公开

EP2488315A1 VERFAHREN UND VORRICHTUNG ZUR KOMPLEXEN UMFORMUNG EINES BLECHES MIT HILFE VON ROTATIONSKÖRPERN 审中-公开
标题翻译：方法和设备的络合物形成一个表中使用的旋转体
公开(公告)号：EP2488315A1
公开(公告)日：2012-08-22
申请号：EP10771063.4
申请日：2010-10-11
申请人： Ostseestaal GmbH
发明人： EILERS, Günter
IPC分类号： B21H7/00 , B21H7/16
CPC分类号： B21H7/007 , B21H7/16
摘要： The invention relates to a method for the forming of a metal sheet with the aid of bodies of revolution. For this purpose, two receiving shafts (3, 4) that are spaced apart from each other are provided with shaped bodies (1, 2), wherein the shaped bodies are configured in their surface in such a way that they replicate the end product. Then, the shaped bodies are aligned in such a way that they are opposite each other in neutral positions, the inserted workpiece (5) defining this neutral position by an outer edge. Finally, in a first forming phase, as it is being advanced, the workpiece is subjected to deformation while pressure is applied, to the extent that the workpiece is changed in its thickness and/or curved. If the workpiece is advanced counter to the working direction (16), no pressure is applied. This operation is repeated until the workpiece has achieved the desired thickness. For further forming phases, the forming process is repeated, the number of forming phases being dependent on the number and type of changes in thickness and curvature that are desired. The invention also relates to a device for carrying out said method.

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