| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 1 | 整体成形箱底五轴镜像铣数控加工方法 | CN201610249461.1 | 2016-04-21 | CN105772812A | 2016-07-20 | 郭立杰; 任斐; 毕庆贞; 张伟; 毛惠明; 李敏明; 刘晓; 曹晓 |
| 本发明提供运载火箭燃料贮箱整体成形箱底五轴镜像铣数控加工方法包括：步骤一、将零件置于回转工装台面，并定位；步骤二、刀具沿所述零件外型面切削；随动装置沿零件内型面移动，刀具的轴线、随动装置的轴线与零件的法线在同一条直线上；步骤三、测厚仪测量当前点厚度，如果和设定的厚度相同，刀具移动到下一点；如果比设定的厚度大，继续切削当前点。 | ||||||
| 2 | 叶面精加工方法及叶零件 | CN201380076345.9 | 2013-05-09 | CN105358277A | 2016-02-24 | 落合宏行; 桑原贤吾; 武川峻久 |
| 叶面精加工方法将叶零件(M1)的叶面(S1)的前缘部(S1a)及后缘部(S1t)的精加工、与腹部(S1v)及背部(S1b)的精加工分为不同的工序，并且向坯料(W1)的叶面相当部位(P1)的腹部(P1v)及背部(P1b)分别加速后接近来实施精加工，并使精加工用立铣刀(30)从坯料(W1)的叶面相当部位(P1)离开后减速。 | ||||||
| 3 | 五轴加工中心上加工叶轮方法 | CN201410695278.5 | 2014-11-27 | CN104827113A | 2015-08-12 | 王晓冬 |
| 本发明五轴加工中心上加工叶轮方法涉及机械加工领域，具体涉及五轴加工中心上加工叶轮方法，包括以下步骤：采用心轴装夹定位，在毛坯上加工出键槽进行辅助定位，并制作适应心轴定位装夹；利用百分表找正工件，求出工件坐标系，将百分表的安装杆装在刀柄上，移动工作台使主轴中心线大约移到工件中心，本发明可以减少装夹次数，保证定位精度；同时，更能提高叶轮表面粗糙度，使用高速铣削能有效地降低切削力和切削区域温度，从而减少叶片的热变形，且不仅能提高加工效率；而且提高加工质量和精度，并且增加叶片的强度和刚度。 | ||||||
| 4 | APPARATUS FOR MORE EFFECTIVELY EXTRACTING ENERGY RESOURCES FROM UNDERGROUND RESERVOIRS AND A METHOD FOR MANUFACTURING THE SAME | US15453112 | 2017-03-08 | US20170298716A1 | 2017-10-19 | Taylor McConnell; Scott S. Brunner; Alan R. Keniston |
| An apparatus for more effectively extracting energy resources from underground reservoirs and a method for manufacturing the same. The apparatus is a perforating gun that includes scallops shaped such that charges that are displaced from their original location nevertheless remain located below the scallop, which increases the effectiveness of displaced charges when detonated. In addition, the scallops are created using a method that enables the entire scallop to be of a uniform thickness, which also increases the effectiveness of charges detonated beneath the scallop. | ||||||
| 5 | MILLING MACHINE | US14385176 | 2013-03-05 | US20150043986A1 | 2015-02-12 | Jose Antonio Estancona Ercilla |
| The invention relates to a milling machine comprising a frame (2) including a work surface (2.1) disposed in a vertical plane and a C-shaped moving bridge (3). In addition, the machine comprises: at least three heads (7), each head including a machining spindle (15); and five movement axes (X, Y, Z, A, B), such that the moving bridge (3) is moved by the frame (2) along a horizontal axis (X), and each head (7) is moved independently on the moving bridge (3) along a vertical axis (Y) in order to be moved towards or away from the work surface (2.1) along a depth axis (Z) perpendicular to both the horizontal axis (X) and the vertical axis (Y), as well as rotating independently about a first axis of rotation (A). Each spindle (15) rotates independently about a second axis of rotation (B). | ||||||
| 6 | METHOD FOR MILLING A CYLINDER HEAD AND CYLINDER HEAD | US13721378 | 2012-12-20 | US20130152781A1 | 2013-06-20 | FRANZ LAIMBOECK; SIEGFRIED LINS |
| A method for the machine-milling of intake and/or exhaust ducts formed in a cylinder head includes working off the inner wall surfaces of the intake and/or exhaust ducts at least in part, preferably completely, with a multi-axis, preferably five-axis, CNC-controlled cherry head in a stabbing movement. Grooves are thus formed in the inner wall surfaces that extend primarily in the flow direction of the ducts. | ||||||
| 7 | Method and device for cutting freeform surfaces by milling | US10552300 | 2004-07-02 | US20070172320A1 | 2007-07-26 | Arndt Glaesser |
| A method and a device for cutting freeform surfaces is disclosed. In 5-axis cutting, a workpiece is milled by a tool, i.e., a milling cutter, in such a way that a desired freeform surface is obtained. The tool is moved for cutting along at least one tool path, i.e., cutting path, defined on the basis of interpolation points in relation to the workpiece. According to this invention, a tool vector in the form of leading angles and setting angles is defined for each interpolation point on the tool path. For each interpolation point a normal vector is determined from the leading angles and the setting angles and also from a drive vector determined for each interpolation point. The normal vector in each interpolation point on the tool path is used for a 3D-radius correction for equalizing/compensating for deviations in dimensions of the milling cutter. | ||||||
| 8 | TURBOCHARGER COMPRESSOR IMPELLER WITH SERRATED LEADING EDGES | US15457539 | 2017-03-13 | US20180258945A1 | 2018-09-13 | Robert Dirk Lotz; Kenneth Lee Davis; John Paul Watson; Gordon Jenks |
| A turbocharger is disclosed. The turbocharger may comprise a turbine, and a compressor having a radial impeller. The radial impeller may include a body having a hub and a plurality of main blades extending from the hub. Each of the main blades may have a leading edge. The turbocharger may further comprise a plurality of serrations extending along the leading edge of each of the main blades, and a shaft interconnecting the compressor and the turbine. The body of the impeller may be formed by flank milling, and the serrations extending along the leading edges of the main blades may be formed by point milling. | ||||||
| 9 | Wing surface finishing method and wing component | US14933589 | 2015-11-05 | US09694430B2 | 2017-07-04 | Hiroyuki Ochiai; Kengo Kuwahara; Toshihisa Takekawa |
| A wing surface finishing method is the one in which after finishing of a leading edge and a trailing edge and finishing of a ventral portion and a back portion in a wing surface of a wing component are separated into separate steps, a finishing end mill is made to approach a ventral portion and a back portion of awing surface corresponding area of a workpiece after a speed of the finishing end mill is increased, finishing processing is applied to the ventral portion and the back portion of the wing surface corresponding area of the workpiece, respectively, and the speed of the finishing end mill is decreased after the finishing end mill is moved away from the wing surface corresponding area of the workpiece. | ||||||
| 10 | Method and device for cutting freeform surfaces by milling | US10552300 | 2004-07-02 | US07518329B2 | 2009-04-14 | Arndt Glaesser |
| A method and a device for cutting freeform surfaces is disclosed. In 5-axis cutting, a workpiece is milled by a tool, i.e., a milling cutter, in such a way that a desired freeform surface is obtained. The tool is moved for cutting along at least one tool path, i.e., cutting path, defined on the basis of interpolation points in relation to the workpiece. According to this invention, a tool vector in the form of leading angles and setting angles is defined for each interpolation point on the tool path. For each interpolation point a normal vector is determined from the leading angles and the setting angles and also from a drive vector determined for each interpolation point. The normal vector in each interpolation point on the tool path is used for a 3D-radius correction for equalizing/compensating for deviations in dimensions of the milling cutter. | ||||||
| 11 | VERFAHREN UND VORRICHTUNG ZUM FRÄSEN VON FREIFORMFLÄCHEN | EP04762337.6 | 2004-07-02 | EP1592527B1 | 2007-09-12 | GLÄSSER, Arndt |
| The invention relates to a method and a device for milling freeform surfaces. During milling of 5 axes, a work piece is milled by a tool and/or a miller, in order to produce a desired freeform surface. Said tool is displaced, with respect to the work piece, along at least one tool path and/or milling path defined by support points. According to the invention, a tool vector is defined for each support point of the tool path in the form of forward angles and setting angles. A normal vector is determined for each support point from the forward angles and setting angles, and from a drive vector determined for each support point. The normal vector in each support point of the tool path is used for 3D radius correction in order to compensate for measuring deviations of the miller. | ||||||
| 12 | VERFAHREN UND VORRICHTUNG ZUM FRÄSEN VON FREIFORMFLÄCHEN | EP04762337.6 | 2004-07-02 | EP1592527A2 | 2005-11-09 | GLÄSSER, Arndt |
| The invention relates to a method and a device for milling freeform surfaces. During milling of 5 axes, a work piece is milled by a tool and/or a miller, in order to produce a desired freeform surface. Said tool is displaced, with respect to the work piece, along at least one tool path and/or milling path defined by support points. According to the invention, a tool vector is defined for each support point of the tool path in the form of forward angles and setting angles. A normal vector is determined for each support point from the forward angles and setting angles, and from a drive vector determined for each support point. The normal vector in each support point of the tool path is used for 3D radius correction in order to compensate for measuring deviations of the miller. | ||||||
| 13 | METHOD AND APPARATUS FOR ADAPTING STANDARD END CAP ASSEMBLIES OF A PERFORATING GUN TO FUNCTION AS TUBING CONVEYED PERFORATING END CAP ASSEMBLIES | US15453152 | 2017-03-08 | US20170298715A1 | 2017-10-19 | Taylor McConnell; Scott S. Brunner; Alan R. Keniston |
| Method and apparatus for adapting a Standard End Cap assembly of a perforating gun to function as a Tubing Conveyed Perforating end cap assembly of a perforating gun. The method includes inserting an inner end cap into an opening of a Standard End Cap, and positioning the inner end cap such that the inner end cap and Standard End Cap become interlocked without the need of a snap ring. The apparatus includes an inner end cap that may include anchors or receivers, and a Standard End Cap that may include anchors or receivers, such that the anchors in one component correspond to the receivers in the other component to facilitate the interlocking of the two components. | ||||||
| 14 | Milling machine | US14385176 | 2013-03-05 | US09616504B2 | 2017-04-11 | Jose Antonio Estancona Ercilla |
| A milling machine including a frame (2) having a work surface (2.1) disposed in a vertical plane and a C-shaped moving bridge (3). In addition, the machine includes: at least three heads (7), each head including a machining spindle (15); and five movement axes (X, Y, Z, A, B), such that the moving bridge (3) is moved by the frame (2) along a horizontal axis (X). Each head (7) is moved independently on the moving bridge (3) along a vertical axis (Y) in order to be moved towards or away from the work surface (2.1) along a depth axis (Z) perpendicular to both the horizontal axis (X) and the vertical axis (Y), as well as rotating independently about a first axis of rotation (A). Each spindle (15) rotates independently about a second axis of rotation (B). | ||||||
| 15 | Method for milling a cylinder head and cylinder head | US13721378 | 2012-12-20 | US09383014B2 | 2016-07-05 | Franz Laimboeck; Siegfried Lins |
| A method for the machine-milling of intake and/or exhaust ducts formed in a cylinder head includes working off the inner wall surfaces of the intake and/or exhaust ducts at least in part, preferably completely, with a multi-axis, preferably five-axis, CNC-controlled cherry head in a stabbing movement. Grooves are thus formed in the inner wall surfaces that extend primarily in the flow direction of the ducts. | ||||||
| 16 | WING SURFACE FINISHING METHOD AND WING COMPONENT | US14933589 | 2015-11-05 | US20160052071A1 | 2016-02-25 | Hiroyuki OCHIAI; Kengo KUWAHARA; Toshihisa TAKEKAWA |
| A wing surface finishing method is the one in which after finishing of a leading edge and a trailing edge and finishing of a ventral portion and a back portion in a wing surface of a wing component are separated into separate steps, a finishing end mill is made to approach a ventral portion and a back portion of awing surface corresponding area of a workpiece after a speed of the finishing end mill is increased, finishing processing is applied to the ventral portion and the back portion of the wing surface corresponding area of the workpiece, respectively, and the speed of the finishing end mill is decreased after the finishing end mill is moved away from the wing surface corresponding area of the workpiece. | ||||||
| 17 | MULTI-AXIS MILLING TOOL | US14409098 | 2013-06-26 | US20150224616A1 | 2015-08-13 | Florent Miquel; Jean Robichaud |
| There is provided an apparatus for machining a workpiece having a plurality of faces. The apparatus comprises a machine frame, a cutting tool mounted to the machine frame, a support member, a first connecting member interconnecting the machine frame to the support member and defining a relative rotation between the support member and the machine frame about first and second transverse axes, and a second connecting member engaged to the support member and configured to retain the workpiece, the second connecting member being rotatable with respect to the first connecting member about a third axis for exposing alternate ones of the plurality of faces of the retained workpiece to the cutting tool, the third axis extending along a direction different than respective directions of the first and second axes. | ||||||
| 18 | 5축 로봇라우터 셀 유닛 | KR1020110052380 | 2011-05-31 | KR1020120133642A | 2012-12-11 | 김휘승 |
| PURPOSE: A five-axis robot router cell unit is provided with a minimum installation space as rotary and movable units are integrally placed on a ceiling. CONSTITUTION: A five-axis robot router cell unit comprises X-axis, Y-axis, and Z-axis units(100,200,300), a rotary unit(400), a movable unit(500), and a control unit. The Y-axis unit moves side by side on a transfer rail. The Y-axis unit is settled on the X-axis unit, and the X-axis unit longitudinally moves on the transfer rail. The Z-axis unit passes through the X-axis and Y-axis units, and vertically moves. The rotary unit is connected to a first support(310) extended from the end of the Z-axis unit. The rotary unit horizontally rotates around a rotary shaft(410). The movable unit is connected to a second support(420) extended from the rotary unit, and rotates around a movable shaft(510). The control unit controls the process of cutting, processing, and deburring die-cast products. | ||||||
| 19 | WING SURFACE FINISHING METHOD AND WING COMPONENT | EP13884227 | 2013-05-09 | EP2995404A4 | 2017-01-11 | OCHIAI HIROYUKI; KUWAHARA KENGO; TAKEKAWA TOSHIHISA |
| A wing surface finishing method is the one in which after finishing of a leading edge (S1a) and a trailing edge (S1t) and finishing of a ventral portion (S1v) and a back portion (S1b) in a wing surface (S1) of a wing component (M1) are separated into separate steps, a finishing end mill (30) is made to approach a ventral portion (P1v) and a back portion (P1b) of a wing surface corresponding area (P1) of a workpiece (W1) after a speed of the finishing end mill (30) is increased, finishing processing is applied to the ventral portion (P1v) and the back portion (P1b) of the wing surface corresponding area (P1) of the workpiece (W1), respectively, and the speed of the finishing end mill (30) is decreased after the finishing end mill (30) is moved away from the wing surface corresponding area (P1) of the workpiece (W1). | ||||||
| 20 | WING SURFACE FINISHING METHOD AND WING COMPONENT | EP13884227.3 | 2013-05-09 | EP2995404A1 | 2016-03-16 | OCHIAI, Hiroyuki; KUWAHARA, Kengo; TAKEKAWA, Toshihisa |
A wing surface finishing method is the one in which after finishing of a leading edge (S1a) and a trailing edge (S1t) and finishing of a ventral portion (S1v) and a back portion (S1b) in a wing surface (S1) of a wing component (M1) are separated into separate steps, a finishing end mill (30) is made to approach a ventral portion (P1v) and a back portion (P1b) of a wing surface corresponding area (P1) of a workpiece (W1) after a speed of the finishing end mill (30) is increased, finishing processing is applied to the ventral portion (P1v) and the back portion (P1b) of the wing surface corresponding area (P1) of the workpiece (W1), respectively, and the speed of the finishing end mill (30) is decreased after the finishing end mill (30) is moved away from the wing surface corresponding area (P1) of the workpiece (W1). |
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