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1. 发明申请

US20190204809A1 METHOD AND SYSTEM FOR PRODUCING BLADES OF A MACHINE INTERACTING WITH A FLUID 审中-公开
公开(公告)号：US20190204809A1
公开(公告)日：2019-07-04
申请号：US16329964
申请日：2017-08-30
申请人： Fraunhofer-Gesellschaft zu Förderung der angewandten Forschung e.V.
发明人： Bernhard Stoevesandt , Matthias Schramm , Florian Sayer , Heiko Rosemann , Christian Dörsch
IPC分类号： G05B19/4099 , B23C3/18
CPC分类号： G05B19/4099 , B23C3/18 , G05B19/41875 , G05B2219/32189 , G05B2219/32217 , G05B2219/32218 , G05B2219/35134 , G05B2219/37205 , G05B2219/37576 , G05B2219/37617 , G05B2219/45147 , G05B2219/50207 , Y02E10/721 , Y02P90/22
摘要： The invention relates to a method and to system for producing blades (1) of a machine interacting with a fluid, in particular a fluid-driven machine, in particular a wind turbine, comprising an examination device (19) for determining geometric deviations (A, B, C, D, E, F) from a target shape for one or more shaped blades (1), a device (21) for determining a deviation evaluation of one or more determined geometric deviations from the target shape for each blade with respect to the aerodynamic and/or mechanical consequences thereof, a device (23) for assigning one or more corrective measures (100, 101, 102), each including an expenditure evaluation (100″, 101″, 102″), to one or more determined geometric deviations (A, B, C, D, E, F) from the target shape for each blade, and a linking device (24) for linking a deviation evaluation that was determined for one or more of the determined geometric deviations to the expenditure evaluation for one or more determined corrective measures and for determining the corrective measures to be carried out from the result of the linkage.

2. 发明申请

US20170368614A1 SYSTEM AND METHOD FOR MACHINING BLADES, BLISKS AND AEROFOILS 审中-公开
公开(公告)号：US20170368614A1
公开(公告)日：2017-12-28
申请号：US15698603
申请日：2017-09-07
申请人： Delcam Limited
发明人： Ian Darren Caldicott
IPC分类号： B23C3/18
CPC分类号： B23C3/18 , B23C2215/44 , G05B19/4099 , G05B2219/36296 , G05B2219/36301 , G05B2219/36304 , G05B2219/45147
摘要： Systems and method relating to machining parts include a CNC system including CNC machining tools, and a computer including a processor and a computer-readable medium, wherein the computer-readable medium encodes instructions of a single NC program that, when run on the processor, causes the computer to control a selected CNC machining tool to perform operations including alternating between (i) moving the selected CNC machining tool along a semi-finishing toolpath segment using a first set of spindle speed and feed rate values to remove a next portion of rough stock material in a next region of a part being manufactured, and (ii) moving the selected CNC machining tool along a finishing toolpath segment to remove a semi-finishing thickness portion of the part in the next region, wherein the first set of spindle speed and feed rate values are different from the second set of spindle speed and feed rate values.

3. 发明授权

US09817389B2 Adaptively machining component surfaces and hole drilling 有权
公开(公告)号：US09817389B2
公开(公告)日：2017-11-14
申请号：US14197876
申请日：2014-03-05
申请人： Rolls-Royce Corporation
发明人： Jeffrey F. Rhodes , Timothy Paul Fuesting , Joseph Peter Henderkott , Ronald J. Snyder , John F. Click , Larry Allen Junod
IPC分类号： G05B19/4099 , G05B19/4097 , G05B19/42
CPC分类号： G05B19/4099 , G05B19/4097 , G05B19/4207 , G05B2219/45147
摘要： A method includes receiving a design surface data set, obtaining a component surface data set from the inspection of a component, creating a modified surface data set in response to the design surface data set and the component surface data set, generating a machining path in response to the modified surface data set, and machining the component in response to the machining path to produce a machined component according to the modified surface data set. The machined component deviates from the design surface data set.

4. 发明申请

US20170316146A1 Adaptive Repair Method for Aerofoil Blades 审中-公开
公开(公告)号：US20170316146A1
公开(公告)日：2017-11-02
申请号：US15493192
申请日：2017-04-21
申请人： ROLLS-ROYCE plc
发明人： Karl S. Huckerby
IPC分类号： G06F17/50
CPC分类号： G06F17/5086 , G05B19/401 , G05B2219/45147 , G06F17/5009 , Y02P90/265
摘要： This disclosure concerns an adaptive repair method, for example for aerofoil blade components. The method generates a digitised model of a physical component and uses data from the digitised model to align a part of the physical component with a nominal CAD model of the component. A combination of the digitised data and data from the nominal CAD model are then used to create an adapted model for repair of the component.

5. 发明授权

US08844132B2 Method of machining using an automatic tool path generator adapted to individual blade surfaces on an integrally bladed rotor 有权
标题翻译：使用适合于整体叶片转子上的各个叶片表面的自动刀具路径发生器的加工方法
公开(公告)号：US08844132B2
公开(公告)日：2014-09-30
申请号：US13188570
申请日：2011-07-22
申请人： Mario Blais , Michel Bellerose
发明人： Mario Blais , Michel Bellerose
IPC分类号： B23B35/00 , B23C3/00 , B23P15/02 , B23C3/18
CPC分类号： B23C3/18 , B23C2215/44 , G05B19/4207 , G05B2219/45147 , Y10T29/49325 , Y10T29/49336 , Y10T29/49995 , Y10T408/03 , Y10T409/303808
摘要： A method of flank and/or point milling an integrally bladed rotor is conducted with an automatic tool path generator which generates a new created tool path including smooth transitions merging between an actual finished surface and a nominal surface of the integrally bladed rotor. The actual finished surface is presented in a mathematical transformation matrix which may be obtained in a 3-D scanning process.
摘要翻译：使用自动刀具路径发生器进行侧面和/或点铣削整体叶片转子的方法，该自动刀具轨迹发生器产生新的创建的刀具路径，其包括实际成品表面与整体叶片转子的标称表面之间的平滑过渡合并。实际的成品表面呈现在可以在3-D扫描过程中获得的数学变换矩阵中。

6. 发明申请

US20140283378A1 METHOD FOR AUTOMATICALLY DETERMINING A FINISHING RECIPE OF A MANUFACTURED COMPONENT 审中-公开
标题翻译：用于自动确定制造部件的成品配件的方法
公开(公告)号：US20140283378A1
公开(公告)日：2014-09-25
申请号：US13847014
申请日：2013-03-19
申请人： Francois-Imran Arrien
发明人： Francois-Imran Arrien
IPC分类号： G06F17/50
CPC分类号： G06F17/50 , G05B19/4099 , G05B2219/35098 , G05B2219/35167 , G05B2219/45147 , Y10T29/53
摘要： The present relates to a method for automatically determining a finishing recipe of a manufactured component. A non-finished 3D model, consisting in a 3D representation of the manufactured component at a non-finished stage, is received at a computer. And a finished 3D model, consisting in a 3D representation of the manufactured component at a finished stage, is received. The non-finished 3D model and the finished 3D model are further processed, to calculate a finishing recipe of one or more tool(s), The tool performs a finishing operation according to the finishing recipe on the manufactured component at the non-finished stage, to obtain the manufactured component at the finished stage. The finishing recipe may include a trajectory of the tool(s), an operational parameter(s) of the tool(s). The manufactured component may consist in a blade. The finishing operation may consist in profiling, polishing, tri-blending, weld blending, twist and bow.
摘要翻译：本发明涉及一种用于自动确定所制造的部件的精加工配方的方法。在计算机上接收未完成的3D模型，其在未完成的阶段中组装在制造的部件的3D表示中。并且接收完成的3D模型，其包括在完成的阶段中制造的部件的3D表示。进一步处理未完成的3D模型和完成的3D模型，以计算一个或多个工具的精加工配方。该工具根据制造零件在未完成阶段的精加工配方执行精加工操作，以在最后阶段获得制造的部件。整理配方可以包括工具的轨迹，一个或多个工具的操作参数。制造的部件可以由叶片组成。整理操作可以包括成型，抛光，三次混合，焊接混合，捻合和弯曲。

7. 发明授权

US08826537B2 Aerofoil structure and a method of making a rib for an aerofoil structure 有权
标题翻译：机翼结构和制作机翼结构的肋骨的方法
公开(公告)号：US08826537B2
公开(公告)日：2014-09-09
申请号：US12680915
申请日：2008-10-17
申请人： Amir Kayani , Ian L Gray
发明人： Amir Kayani , Ian L Gray
IPC分类号： G05B19/4099 , B64C3/26 , B64C3/18 , B64C3/24
CPC分类号： G05B19/4099 , B64C3/187 , B64C3/24 , B64C3/26 , G05B2219/35062 , G05B2219/36248 , G05B2219/37558 , G05B2219/45147 , Y10T29/49316 , Y10T29/49336 , Y10T29/49337 , Y10T29/49339 , Y10T29/49771
摘要： A method for making a rib for an aerofoil structure, the aerofoil structure including a skin component, the method including the steps of scanning the inner surface of the skin component to determine the surface profile thereof, providing a rib having a rib body and a rib foot protruding from the body, machining a foot surface profile into the rib foot, the foot surface profile being arranged to complement the skin inner surface profile where the rib foot is intended to abut the skin component.
摘要翻译：一种用于制造机翼结构的肋的方法，所述机翼结构包括皮肤部件，所述方法包括以下步骤：扫描皮肤部件的内表面以确定其表面轮廓，提供具有肋体和肋的肋脚从身体突出，将脚表面轮廓加工成肋脚，脚表面轮廓被布置成补充肋脚旨在邻接皮肤部件的皮肤内表面轮廓。

8. 发明申请

US20130019477A1 METHOD OF MACHINING USING AN AUTOMATIC TOOL PATH GENERATOR ADAPTED TO INDIVIDUAL BLADE SURFACES ON AN INTEGRALLY BLADED ROTOR 有权
标题翻译：使用自动工具路径发生器加工的方法适用于全面刀片转子上的个别叶片表面
公开(公告)号：US20130019477A1
公开(公告)日：2013-01-24
申请号：US13188570
申请日：2011-07-22
申请人： Mario BLAIS , Michel BELLEROSE
发明人： Mario BLAIS , Michel BELLEROSE
IPC分类号： B23P15/02
CPC分类号： B23C3/18 , B23C2215/44 , G05B19/4207 , G05B2219/45147 , Y10T29/49325 , Y10T29/49336 , Y10T29/49995 , Y10T408/03 , Y10T409/303808
摘要： A method of flank and/or point milling an integrally bladed rotor is conducted with an automatic tool path generator which generates a new created tool path including smooth transitions merging between an actual finished surface and a nominal surface of the integrally bladed rotor. The actual finished surface is presented in a mathematical transformation matrix which may be obtained in a 3-D scanning process.
摘要翻译：使用自动刀具路径发生器进行侧面和/或点铣削整体叶片转子的方法，该自动刀具轨迹发生器产生新的创建的刀具路径，其包括实际成品表面与整体叶片转子的标称表面之间的平滑过渡合并。实际的成品表面呈现在可以在3-D扫描过程中获得的数学变换矩阵中。

9. 发明授权

US08326573B2 Method for characterising the profile of a surface 有权
标题翻译：表征曲面轮廓的方法
公开(公告)号：US08326573B2
公开(公告)日：2012-12-04
申请号：US12310195
申请日：2007-06-21
申请人： Andrew D Jackson , Peter I Wright , Michael A Howard , Robert J Stafford
发明人： Andrew D Jackson , Peter I Wright , Michael A Howard , Robert J Stafford
IPC分类号： G01B7/28
CPC分类号： G01B21/20 , F05D2250/74 , G05B19/4099 , G05B2219/34145 , G05B2219/35016 , G05B2219/35128 , G05B2219/35131 , G05B2219/35193 , G05B2219/37064 , G05B2219/45147 , Y02P90/265 , Y02T50/673
摘要： A method for characterising the surface profile of a component comprises the steps of a) dividing the surface into at least two regions; b) for each region, measuring the surface and selecting a number of measured points to define a co-ordinate dataset for the region; c) for each region, applying a curve-fitting algorithm to the dataset for the region to define the surface profile of the region; d) combining the defined surface profiles for the regions to produce a defined surface profile for the aerofoil surface. The characterization may be used in the design, analysis and manufacturing steps of product development, thereby decreasing the total time and work required.
摘要翻译：用于表征部件的表面轮廓的方法包括以下步骤：a）将所述表面分成至少两个区域; b）对于每个区域，测量表面并选择一些测量点以定义该区域的坐标数据集; c）对于每个区域，对区域的数据集应用曲线拟合算法来定义区域的表面轮廓; d）组合用于区域的限定的表面轮廓以产生用于机翼表面的限定的表面轮廓。特征描述可用于产品开发的设计，分析和制造步骤，从而减少所需的总时间和工作。

10. 发明授权

US08070555B2 Visual feedback for airfoil polishing 有权
标题翻译：翼型抛光的视觉反馈
公开(公告)号：US08070555B2
公开(公告)日：2011-12-06
申请号：US12263515
申请日：2008-11-03
申请人： Douglas Carl Hofer
发明人： Douglas Carl Hofer
IPC分类号： B24B49/00
CPC分类号： B24B19/14 , B24B21/16 , B24B49/12 , G05B19/401 , G05B2219/31048 , G05B2219/45147 , G05B2219/45199
摘要： A visual feedback system and method for airfoil polishing is disclosed. In one aspect there is a system for providing visual feedback during a polishing operation of a workpiece. In this system there is a model having a representation of a desired shape of the workpiece. A scanning system generates a representation of a current shape of the workpiece while in-process during the polishing operation. A comparator compares the current shape of the workpiece to the desired shape of the workpiece. An illumination system highlights the workpiece with visible light during the polishing operation. The highlighting of the workpiece with visible light is a function of the comparison between the current shape and the desired shape. The illumination system highlights a portion of the workpiece that needs additional polishing to conform to the desired shape.
摘要翻译：公开了一种用于翼型抛光的视觉反馈系统和方法。在一个方面，存在在工件的抛光操作期间提供视觉反馈的系统。在该系统中，存在具有所需工件形状的表示的模型。扫描系统在抛光操作过程中产生工件的当前形状的表示。比较器将工件的当前形状与工件的所需形状进行比较。在抛光操作期间，照明系统用可见光强调工件。具有可见光的工件的突出显示是当前形状和所需形状之间的比较的函数。照明系统突出了需要额外抛光以符合所需形状的工件的一部分。

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