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公开(公告)号：US20150209929A1
公开(公告)日：2015-07-30
申请号：US14166043
申请日：2014-01-28
CPC分类号： B24B5/36 , B23P6/04 , B24B5/04 , B24B5/35 , B24B19/14 , B24B23/028 , B24B23/08 , B24B27/0084 , B24B39/006 , F01D5/005 , F01D25/285
摘要： Embodiments of the present disclosure relate generally to an apparatus and method for treating a rotatable component. An apparatus according to the present disclosure can include: a sliding engagement member configured to slidably engage a portion of a rotating component that is temporarily stationary; and a tool engaging member for positioning a machining tool relative to the rotating component to machine a surface of the rotating component, wherein the tool engaging member is rotatable to one of a plurality of angles relative to the sliding engagement member.
摘要翻译： 本公开的实施例总体上涉及用于处理可旋转部件的装置和方法。 根据本公开的装置可以包括：滑动接合构件，其构造成可滑动地接合暂时静止的旋转部件的一部分; 以及工具接合构件，用于相对于所述旋转部件定位加工工具以加工所述旋转部件的表面，其中所述工具接合构件可相对于所述滑动接合构件转动到多个角度中的一个角度。
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公开(公告)号：US09089970B2
公开(公告)日：2015-07-28
申请号：US13356038
申请日：2012-01-23
CPC分类号： B25J9/1697 , B24B19/14 , B24B27/0038 , B25J9/06 , B25J11/0055 , B25J13/08 , B25J19/023 , G05B2219/2619 , G05B2219/39391 , G05B2219/40425 , G05B2219/45058
摘要： A robotic apparatus and system for cutting turbine bucket covers on a turbine rotor are provided. The robotic apparatus includes a grinding device operable to drive a grinding wheel, a robotic arm coupled to the grinding device, a base member coupled to the robotic arm, a vision system for locating the fastener on the turbine bucket cover, and a control system. The base member is mounted independently of the turbine bucket cover. The control system is coupled to the vision system, the grinding device, and the robotic apparatus, and configured to control movement of the robotic apparatus and the grinding device based upon vision system data and spatial information related to the turbine bucket cover. The system includes at least a portion of a turbine rotor including a turbine bucket cover having at least one fastener thereon, and a robotic device for cutting the turbine bucket cover.
摘要翻译： 提供了一种用于在涡轮转子上切割涡轮机桶盖的机器人装置和系统。 机器人装置包括可操作以驱动砂轮的研磨装置，联接到研磨装置的机器人臂，联接到机器人臂的基座构件，用于将紧固件定位在涡轮机罩盖上的视觉系统和控制系统。 基座构件独立于涡轮机罩盖安装。 控制系统耦合到视觉系统，研磨装置和机器人装置，并且被配置为基于与涡轮机罩盖相关的视觉系统数据和空间信息来控制机器人装置和研磨装置的运动。 该系统包括涡轮转子的至少一部分，其包括在其上具有至少一个紧固件的涡轮机叶片盖，以及用于切割涡轮叶片盖的机器人装置。
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公开(公告)号：US09089949B2
公开(公告)日：2015-07-28
申请号：US13693253
申请日：2012-12-04
发明人： Mark Lawrence Hunt
CPC分类号： B24B49/16 , B24B19/14 , B24B49/105 , B24B51/00
摘要： Automated polishing systems include a polisher for polishing the coating on the article and a robotic positioner for moving the polisher relative to the article on an automated path, wherein the polisher polishes at least a part of the coating during movement, a force feedback sensor for determining a force of the polisher against the article during polishing, and a controller for maintaining the polisher within a predetermined force range against the article based at least in part on the force determined by the force feedback sensor.
摘要翻译： 自动抛光系统包括用于抛光物品上的涂层的抛光机和用于在自动路径上相对于物品移动抛光机的机器人定位器，其中抛光机在运动期间抛光涂层的至少一部分，用于确定 在研磨期间抛光机抵靠物品的力，以及控制器，用于至少部分地基于由力反馈传感器确定的力，将抛光机保持在预定的力范围内。
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公开(公告)号：US20150118939A1
公开(公告)日：2015-04-30
申请号：US14521847
申请日：2014-10-23
CPC分类号： B24B23/08 , B23P6/002 , B24B19/14 , Y10T408/353
摘要： Embodiments of the invention are directed to a portable grinding apparatus comprising: a frame; a boring bar operatively coupled to the frame; and a grinding assembly operatively coupled to the boring bar, wherein the grinding assembly is adjustable in one or more axes by adjusting the frame or the grinding assembly for grinding a component secured to the frame.
摘要翻译： 本发明的实施例涉及一种便携式研磨设备，包括：框架; 可操作地联接到框架的镗杆; 以及可操作地联接到所述钻杆的研磨组件，其中所述研磨组件可以在一个或多个轴线上调节，通过调整所述框架或所述研磨组件以研磨固定到所述框架的部件。
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公开(公告)号：US20150099425A1
公开(公告)日：2015-04-09
申请号：US14048591
申请日：2013-10-08
申请人： THE BOEING COMPANY
发明人： Thomas Edward Trnka
IPC分类号： B24B1/00
CPC分类号： B24B1/00 , B24B19/14 , B24B19/26 , B24B27/0038 , B24B49/12 , B25J5/02 , B25J9/0084 , B25J9/1684 , B25J11/0065 , Y10T29/49769 , Y10T29/5176
摘要： A method and apparatus for sanding a number of surface features on a surface of an object. A first type of operation may be performed on the number of surface features on the surface of the object using a first end effector. Feedback laser data may be generated about the number of surface features after the first type of operation has been performed using a laser device. A second type of operation may be performed on the number of surface features using a second end effector and the feedback laser data to rework the number of surface features until the number of surface features has been reworked to within selected tolerances.
摘要翻译： 一种用于在物体表面上打磨许多表面特征的方法和装置。 可以使用第一端部执行器对物体表面上的表面特征的数量执行第一类型的操作。 在使用激光装置执行第一类型的操作之后，可以产生关于表面特征的数量的反馈激光数据。 可以使用第二端部执行器和反馈激光数据对表面特征的数量执行第二类型的操作，以重新编号表面特征的数量，直到表面特征的数量已经重新设计到所选公差内。
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公开(公告)号：US08801502B2
公开(公告)日：2014-08-12
申请号：US13407302
申请日：2012-02-28
申请人： Henry Ng , Daniel O'Reilly
发明人： Henry Ng , Daniel O'Reilly
IPC分类号： B24B9/00
CPC分类号： B23P6/002 , B24B19/009 , B24B19/14 , B24B23/02 , B24D5/066 , F01D5/005 , F05D2230/80
摘要： A tool for in-situ airfoil contouring is provided. The tool has a pathway for an airfoil edge wherein the edge movement is limited and further wherein the edge is exposed to a grinding structure having a preselected profile shape therein. The tool makes this contouring process available for airfoils without the necessity of removing the airfoils from, for example, an aircraft engine.
摘要翻译： 提供了一种用于原位翼型轮廓的工具。 该工具具有用于翼型边缘的路径，其中边缘运动受到限制，并且进一步其中边缘暴露于其中具有预选轮廓形状的研磨结构。 该工具使这种轮廓加工过程可用于翼型件，而不需要从例如飞行器发动机去除翼型件。
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公开(公告)号：US08701287B2
公开(公告)日：2014-04-22
申请号：US12385329
申请日：2009-04-06
申请人： Liane Holze , Gregor Riedel
发明人： Liane Holze , Gregor Riedel
CPC分类号： B24B19/14 , B23C3/18 , B23C2215/44 , B23P15/006 , F01D5/141 , F01D5/34 , F05D2240/121 , F05D2240/303 , Y10T29/49325 , Y10T29/49336 , Y10T29/49337 , Y10T29/49995 , Y10T29/49996
摘要： For shaping the leading edge (1) of blisk blades (2), the shape, amount and disposition of the material to be removed in a subsequent grinding and polishing process is determined beforehand over the entire blade length. The blade leading edge is milled such that an elliptical profile (3) has a material allowance (7) which over the length of the leading edge exactly corresponds to an expected material removal during the grinding and polishing process, so that a blisk blade is produced whose leading edge features an aerodynamically advantageous shape.
摘要翻译： 为了对叶片叶片（2）的前缘（1）进行成形，在整个叶片长度上预先确定在随后的研磨和抛光过程中待除去的材料的形状，数量和布置。 刀片前缘被铣削，使得椭圆形轮廓（3）具有材料余量（7），其在前缘的长度上精确对应于在研磨和抛光过程期间的预期材料去除，从而产生叶片叶片 其前沿具有空气动力学有利的形状。
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公开(公告)号：US08684790B2
公开(公告)日：2014-04-01
申请号：US12668833
申请日：2008-07-10
IPC分类号： B24B49/00
CPC分类号： B24B17/00 , B23P6/002 , B24B17/10 , B24B19/14 , B24B21/16 , B24B27/0038 , B24B49/00 , B24B49/16 , B25J11/0065 , B25J15/0491 , F01D25/285
摘要： The invention relates to a method and an arrangement for re-creation of an optimized contour of the leading edges of gas-turbine blades, in which a gas-turbine blade (2) is passed by one or more grinding machine or machines (71, 71′) with the aid of a computer-controlled robot (10). The desired contour is achieved by following a movement procedure which is stored in a data memory (21). The stored movement procedure is designed to convert a blade from a previously determined statistical mean wear state to a likewise previously determined or calculated design contour. The contact pressure of the gas-turbine blade on the grinding disk or disks (71, 71′) is measured and is taken into account in the movement procedure of the robot (10) such that the desired design contour is achieved irrespective of the initial contour and wear of the grinding disks.
摘要翻译： 本发明涉及一种用于重新创建燃气轮机叶片的前缘的优化轮廓的方法和装置，其中燃气轮机叶片（2）由一个或多个研磨机或机器（71， 71'）借助于计算机控制的机器人（10）。 通过遵循存储在数据存储器（21）中的移动过程来实现期望的轮廓。 存储的运动过程被设计成将刀片从先前确定的统计平均磨损状态转换成同样预先确定或计算的设计轮廓。 在机器人（10）的移动过程中测量燃气轮机叶片在研磨盘或盘（71,71'）上的接触压力，使得实现期望的设计轮廓，而不管初始 研磨盘的轮廓和磨损。
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公开(公告)号：US20140041224A1
公开(公告)日：2014-02-13
申请号：US13584257
申请日：2012-08-13
申请人： David S. Murphy
发明人： David S. Murphy
CPC分类号： C21D10/005 , B23K26/356 , B23P9/00 , B23P15/02 , B24B19/14 , B24C1/00 , F01D5/286 , Y10T29/49336
摘要： A method of post processing a laser peened component to remove a laser remelt layer is proposed. The post processing includes a series of steps including grit blasting, chemical etching and mechanical finishing the component. This will ensure that the mechanical property (i.e., damage tolerance) benefit of laser peening is restored to the surface of the component.
摘要翻译： 提出了一种后处理激光喷丸组件去除激光重熔层的方法。 后处理包括一系列步骤，包括喷砂，化学蚀刻和机械加工组件。 这将确保激光喷丸处理的机械性能（即损伤公差）恢复到部件的表面。
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80.发明申请METHOD FOR DETERMINING THE DIAMETER OF A ROTOR, WHICH IS EQUIPPED WITH ROTOR BLADES, OF A TURBOMACHINE 有权用于确定具有转子叶片的涡轮机转子的直径的方法公开(公告)号：US20130330173A1
公开(公告)日：2013-12-12
申请号：US14000629
申请日：2011-12-30
申请人： Karsten Klein
发明人： Karsten Klein
CPC分类号： G01M15/14 , B24B19/14 , B24B49/04 , F01D5/027 , F01D11/14 , F01D21/003 , F01D21/04 , F01D25/00 , F05D2230/64 , F05D2260/34 , G01B7/30 , G01B7/305 , G01B7/31 , G01B7/312 , G01B7/315 , G01B11/028 , G01B11/08 , G01B11/12 , G01B11/14 , G01B11/27 , G01B11/272 , G01B21/22 , G01B21/24 , G01B21/26 , G01S17/88 , Y10T29/4932
摘要： A method is provided for determining the diameter of a rotor of a turbomachine, rotor being equipped with rotor blades. The method involves setting the rotor with the rotor blade ring in rotation, arranging a clearance measuring device assigned to the rotor blade ring outside the region of the latter, measuring the distance to the rotor blades of the rotor blade ring which are rotating past the clearance measuring device, and using the measured distance for determining the diameter of the rotor. During measuring, the rotational speed is identical to, almost identical to or higher than the setpoint rotational speed of the rotor.
摘要翻译： 提供了一种用于确定涡轮机的转子的直径的方法，转子配备有转子叶片。 该方法包括使转子叶片环旋转地设置转子，将分配给转子叶片环的间隙测量装置布置在后者的区域外部，测量与转动叶片环的转子叶片的距离，该转子叶片环旋转经过间隙 测量装置，并使用测量的距离来确定转子的直径。 在测量期间，转速与转子的额定转速相同，几乎相同或更高。
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