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 一种大型轴流式叶轮一次装夹铣加工方法 CN201611031072.8 2016-11-22 CN106513797A 2017-03-22 盛永刚; 岳召启; 张积瑜
一种大型轴流式叶轮一次装夹铣加工方法,属于机械加工技术领域。本发明提供一种可提高大型轴流式整体叶轮加工效率,提高叶片部位表面质量,降低生产成本的大型轴流式叶轮一次装夹铣加工方法。本发明包括如下步骤:步骤一:采用高进给飞碟铣刀进行小切深层铣,完成粗加工;步骤二:采用减振重金属刀具进行轴向插铣;步骤三:采用球刀进行插铣残留余量的光整去除。
2 闭式整体叶盘五坐标插铣加工方法 CN200910219433.5 2009-12-10 CN101708559B 2011-03-02 姚倡锋; 任军学; 张定华; 史耀耀; 田荣鑫; 梁永收; 黄新春
发明公开了一种闭式整体叶盘五坐标插铣加工方法,对加工的闭式整体叶盘的通道进行加工区域划分,分别对进气边加工区域和排气边加工区域生成通道偏置面,并对通道边界线进行求解,生成叶盘通道偏置面直纹包络面,分别得到进气边加工区域和排气边加工区域的插铣刀位轨迹,进而得到了闭式整体叶盘通道的插铣刀位轨迹。最后在五坐标数控机床上按照得到的插铣刀位轨迹对闭式整体叶盘进行插铣加工。本发明避免了闭式整体叶盘加工时的刀具干涉现象,解决了加工过程中编程难度大、约束条件多、刀具轨迹求解过程复杂等技术问题,有效实现了闭式整体叶盘的五坐标插铣加工。
3 闭式整体叶盘五坐标插铣加工方法 CN200910219433.5 2009-12-10 CN101708559A 2010-05-19 姚倡锋; 任军学; 张定华; 史耀耀; 田荣鑫; 梁永收; 黄新春
发明公开了一种闭式整体叶盘五坐标插铣加工方法,对加工的闭式整体叶盘的通道进行加工区域划分,分别对进气边加工区域和排气边加工区域生成通道偏置面,并对通道边界线进行求解,生成叶盘通道偏置面直纹包络面,分别得到进气边加工区域和排气边加工区域的插铣刀位轨迹,进而得到了闭式整体叶盘通道的插铣刀位轨迹。最后在五坐标数控机床上按照得到的插铣刀位轨迹对闭式整体叶盘进行插铣加工。本发明避免了闭式整体叶盘加工时的刀具干涉现象,解决了加工过程中编程难度大、约束条件多、刀具轨迹求解过程复杂等技术问题,有效实现了闭式整体叶盘的五坐标插铣加工。
4 Method of generating a curved blade retention slot in a turbine disk US12037387 2008-02-26 US09662721B2 2017-05-30 Changsheng Guo
A method of forming a curved slot in a turbine disk includes the steps of forming a pre-slot in the turbine disk and finishing the pre-slot to form a slot that receives a portion of a turbine blade. The turbine disk including a first face, an opposing second face, and an outer perimeter surface extending between the first face and the opposing second face. The pre-slot includes a first curved wall and a second curved wall that each extend between the first face and the opposing second face. An intersection between the outer perimeter surface and each of the first curved wall and the second curved wall is defined by a curved line.
5 MILLING DEVICE AND METHOD FOR MILLING WITHIN A SLOT US15346759 2016-11-09 US20170136556A1 2017-05-18 MICHAEL CLOSSEN-VON LANKEN SCHULZ; STEFAN OBERMAYR
A milling device is provided, having a milling tool that rotates about a tool rotation axis, wherein the milling device has a slide, and in that the milling tool is held on a pivot axis that extends transversely, in particular perpendicular, to the tool rotation axis and through the slide, wherein the slide is designed and the position of the milling tool is selected such that, during milling, a traversing movement is effected by manually moving the slide and advance is effected by pivoting the milling tool about the pivot axis. Also provided is a method for milling within a slot of a component, in particular within a blade root receiving slot of a turbomachine, using a milling device.
6 Milling tool for portion of slot in rotor US14671293 2015-03-27 US09623492B2 2017-04-18 Daryl Paul Capriotti; James Bradford Holmes; Andrew Lee Trimmer
A milling tool is disclosed. The tool may include a base including a clamp for coupling to a selected mounting slot of a plurality of slots of the rotor; a milling tool including a motorized milling head; and a motorized linear actuator coupling the milling tool to the base. The base mounts the motorized linear actuator at an acute angle relative a portion of the slot to allow the motorized linear actuator to linearly move the milling tool to machine the portion of the slot. The portion of the slot may include, for example, an end face and, more particularly, a root corner of the slot where a cooling slot flange extends from the root of the slot. The milling tool may be portable.
7 TURBOMACHINE ROTOR BLADE MILLING MACHINE SYSTEM AND METHOD OF FIELD REPAIRING A TURBOMACHINE ROTOR BLADE US14965938 2015-12-11 US20160097282A1 2016-04-07 Jason Matthew Clark; John William Herbold; James Bradford Holmes
A turbomachine rotor blade milling machine system includes a fixture having a body including first and second opposing surfaces and a slot. The fixture is configured and disposed to connect with first and second rotor blade sections mounted in a rotor wheel. A mounting system includes at least one mounting element coupled to one of the first and second opposing surfaces of the body at the slot. A milling machine is coupled to the one of the first and second opposing surfaces through the at least one mounting element. The milling machine includes a cutter and is configured and disposed to form an opening extending axially through a dovetail portion of a third rotor blade section arranged between the first and second rotor blade sections.
8 METHOD OF GENERATING A CURVED BLADE RETENTION SLOT IN A TURBINE DISK US12037387 2008-02-26 US20090214351A1 2009-08-27 Changsheng Guo
A method of forming a curved slot in a turbine disk includes the steps of forming a pre-slot in the turbine disk and finishing the pre-slot to form a slot that receives a portion of a turbine blade. The turbine disk including a first face, an opposing second face, and an outer perimeter surface extending between the first face and the opposing second face. The pre-slot includes a first curved wall and a second curved wall that each extend between the first face and the opposing second face. An intersection between the outer perimeter surface and each of the first curved wall and the second curved wall is defined by a curved line.
9 Step milling process US166248 1998-10-05 US6077002A 2000-06-20 Donald D. Lowe
A blank is milled using a rotating mill. A groove having a bottom is first cut across the blank to partially expose a sidewall in the blank. The sidewall is then cut by the mill. By alternately repeating cutting of the groove and sidewall, the groove is milled deeper in the blank to form a pocket along which the sidewall extends. Since the sidewall is formed in steps, improved efficiency and accuracy is obtained therefor.
10 携帯型ミル工具およびターボ機械ミル処理のための方法 JP2016240791 2016-12-13 JP2017113876A 2017-06-29 BRIAN EDWARD WILLIAM; CHARLES VAN BUCHAN; ANDREW JOSEPH COLLETTI
【課題】携帯型ミル工具とミル要素部品のための方法とを備える。【解決手段】携帯型ミル工具200は、複数のダブテール穴134を備える要素部品130のために提供され、複数のダブテール穴はそれぞれ要素部品の回転軸に対して実質的に軸方向に向けられる。携帯型ミル工具は、要素部品に係合するようになっている搭載プレート202と、搭載プレートに摺動可能に結合され、要素部品の回転軸に対して翼弦軸に沿って伸びる工具整列部材208と、工具整列部材から複数のダブテール穴の選択された1つへ向けて軸方向に伸びるミルヘッド220であって、搭載プレートに対する工具整列部材の摺動移動がミルヘッドを翼弦軸に沿って移動させて複数のダブテール穴の選択された1つに接触させるようになっている、ミルヘッドと、を備える。【選択図】図3
11 Method for machining turbine engine component JP2006326193 2006-12-01 JP2007152549A 2007-06-21 BURGESS GREG M; LOWE DONALD D
<P>PROBLEM TO BE SOLVED: To provide a method for machining a blank in the method for manufacturing a turbine engine component. <P>SOLUTION: The method (50) comprises steps of: (52) for machining a first pocket (54) having a first side wall (60) in the blank; (70) machining a second pocket (56) in the blank; (80) machining a groove (58) in a material positioned between the first and second pockets and exposing a second side wall (66) opposed to the first side wall; (76) machining the first and second side walls; and machining the groove and the side walls, milling the groove in the blank more deeply step by step, and alternately repeating the steps for forming a third pocket (68) where the second side wall extends along it. <P>COPYRIGHT: (C)2007,JPO&INPIT
12 総形回転切削工具 JP2016548500 2014-09-18 JP6295016B2 2018-03-14 都築 清志
13 METHOD OF GENERATING A CURVED BLADE RETENTION SLOT IN A TURBINE DISK US15498520 2017-04-27 US20170226874A1 2017-08-10 Changsheng Guo
A method of forming a curved slot in a turbine disk includes the steps of forming a pre-slot in the turbine disk and finishing the pre-slot to form a slot that receives a portion of a turbine blade. The turbine disk including a first face, an opposing second face, and an outer perimeter surface extending between the first face and the opposing second face. The pre-slot includes a first curved wall and a second curved wall that each extend between the first face and the opposing second face. An intersection between the outer perimeter surface and each of the first curved wall and the second curved wall is defined by a curved line.
14 FORMED ROTARY CUTTING TOOL US15500851 2014-09-18 US20170216938A1 2017-08-03 Kiyoshi TSUDUKI
A formed rotary cutting tool includes a cutting edge defining a cutting edge diameter that is increased and reduced in a direction of an axis of the tool, so as to have at least one neck portion in which the cutting edge diameter is minimized. The cutting tool includes a roughing portion which is provided on a periphery thereof and which is constituted by a succession of protrusions and recesses arranged in the direction of the axis. The roughing portion includes (i) a fine roughing portion that is provided in at least one of the at least one neck portion, and (ii) another portion that is provided in a portion that is other than the at least one of the at least one neck portion. The fine roughing portion of the roughing portion is different in characteristics from the above-described another portion of the roughing portion.
15 PORTABLE MILLING TOOL WITH METHOD FOR TURBOMACHINE MILLING US14976776 2015-12-21 US20170173708A1 2017-06-22 Bryan Edward Williams; Charles Van Buchan; Andrew Joseph Colletti
Embodiments of the present disclosure include portable milling tools and methods for milling components. In an embodiment, a portable milling tool can be provided for a component including a plurality of dovetail slots therein, each of the plurality of dovetail slots being oriented substantially axially relative to a rotation axis of the component. The portable milling tool can include: a mounting plate configured to engage the component; a tool-aligning member slidably coupled to the mounting plate and extending along a chordal axis relative to the rotation axis of the component; and a milling head extending axially from the tool-aligning member to a selected one of the plurality of dovetail slots, such that sliding movement of the tool-aligning member relative to the mounting plate moves the milling head along the chordal axis to contact a selected one of the plurality of dovetail slots.
16 Processing method of a semi-processed product for the production of a rotor equipped with a series of blades integral therewith US11328350 2006-01-09 US07784181B2 2010-08-31 Enzo Nocciolini; Roberto Ciappi
A processing method of a semi-processed product for obtaining a rotor equipped with a series of blades integral therewith by using a rotating tool such as a cutter, integral or with inserts. The processing method includes a) forming a hole into the semi-processed product; b) forming a series of cavities in the semi-processed product by removing material with the rotating tool to create the series of blades, starting from the hole and following predetermined paths; and c) removing material from the semi-processed product by advancing the rotating tool along its rotation axis and not removing material when the rotating tool advances along the predetermined paths. The rotation axis of the rotating tool is misaligned with respect to an axis of the hole.
17 Methods for machining turbine engine components US11292245 2005-12-01 US07637010B2 2009-12-29 Greg M. Burgess; Donald D. Lowe
A method for machining a blank includes machining a first pocket in the blank having a first sidewall, machining a second pocket in the blank, machining a groove within material located between the first and second pockets to expose a second sidewall opposite the first sidewall, machining the first and second sidewalls, and alternately repeating machining the grove and the sidewalls to step mill the groove deeper in the blank and form a third pocket along which the second sidewall extends.
18 Method and tooling for machining the annulus of gas-turbine rotor provided with integrally formed-on blades US12379377 2009-02-19 US20090245959A1 2009-10-01 Jan Hollmann; Gregor Kappmeyer
With an integrally bladed rotor, material removal is performed from the annulus (5) on a wide, even machining path (8) using the front-side cutting area of an essentially cylindrical cutter head (7). The tool shank (9) is shaped and dimensioned such that it does not collide with the opposite lateral surfaces of the differently curved and twisted blades (4). This type of machining enables an essentially even, smooth annulus surface to be obtained with a reduced number of overlapping machining paths (8). The time required for machining the annulus and the tool wear are reduced. With an annulus machined in accordance with the present invention, the rotor will satisfy high requirements on aerodynamics.
19 PORTABLE MILLING TOOL WITH METHOD FOR TURBOMACHINE MILLING EP16204629.6 2016-12-16 EP3184220A1 2017-06-28 WILLIAMS, Bryan Edward; BUCHAN, Charles Van; COLLETTI, Andrew Joseph

Embodiments of the present disclosure include portable milling tools (200) and methods for milling components (130). In an embodiment, a portable milling tool (200) can be provided for a component (130) including a plurality of dovetail slots (134) therein, each of the plurality of dovetail slots (134) being oriented substantially axially relative to a rotation axis of the component (130). The portable milling tool (200) can include: a mounting plate (202) configured to engage the component (130); a tool-aligning member (208) slidably coupled to the mounting plate (202) and extending along a chordal axis relative to the rotation axis of the component; and a milling head (220) extending axially from the tool-aligning member (208) to a selected one of the plurality of dovetail slots (134), such that sliding movement of the tool-aligning member (208) relative to the mounting plate (202) moves the milling head (220) along the chordal axis to contact a selected one of the plurality of dovetail slots (134).

20 Verfahren zur Annulusbearbeitung eines Gasturbinenrotors mit integral angeformten Schaufeln EP09152591.5 2009-02-11 EP2093012B1 2011-12-21 Kappmeyer, Gregor; Hollmann, Jan
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