END MILL FOR ORBITAL DRILLING OF FIBER REINFORCED PLASTIC MATERIALS
    1.
    发明申请
    END MILL FOR ORBITAL DRILLING OF FIBER REINFORCED PLASTIC MATERIALS 审中-公开
    用于纤维增强塑料材料的直接钻孔的末端铣刀

    公开(公告)号:WO2008128035A1

    公开(公告)日:2008-10-23

    申请号:PCT/US2008/060022

    申请日:2008-04-11

    Abstract: A center or non-center cutting end mill (10) for orbital drilling of fiber reinforced plastic (FRP) materials includes a shank (12), a neck (14), a cutting head (16)and two or more flutes (36, 38). The end mill (10) has a tool geometry with the following features: a dish angle (28) between about 2 degrees to about 6 degrees; a helix angle (44) between about 5 degrees to about 18 degrees; an end teeth radial rake angle (46) between about 0 degrees and about 15 degrees; a peripheral teeth radial rake angle (47) between about 8 degrees and about 16 degrees; a gashing axial rake angle (48) between about 3 degrees to about 10 degrees; and a primary clearance angle between about 10 degrees to about 18 degrees. The end mill is made from a tungsten carbide substrate with cemented cobalt and a diamond coating.

    Abstract translation: 用于纤维增强塑料(FRP)材料的轨道钻孔的中心或非中心切割端铣刀(10)包括柄(12),颈部(14),切割头(16)和两个或更多个凹槽(36) 38)。 端铣刀(10)具有具有以下特征的刀具几何形状:约2度至约6度之间的盘角(28); 在约5度至约18度之间的螺旋角(44); 在大约0度和大约15度之间的端齿径向前角(46); 约8度至约16度之间的周边齿径向前角(47); 大约3度至大约10度之间的一个前进的轴向前角(48); 和约10度至约18度之间的主要间隙角。 立铣刀由具有胶结钴和金刚石涂层的碳化钨基底制成。

    MULTILAYER NITRIDE HARD COATINGS
    3.
    发明申请
    MULTILAYER NITRIDE HARD COATINGS 审中-公开
    多层硝酸硬涂层

    公开(公告)号:WO2011149580A1

    公开(公告)日:2011-12-01

    申请号:PCT/US2011/029153

    申请日:2011-03-21

    Abstract: A wear resistant multilayer nitride hard coating (2) for substrates (6). The hard coaling (2) includes a first layer (4) of titanium aluminum nitride and a second layer (8) comprising a plurality of sublayer groups (10a). Each sublayer group (10a) includes a first sublayer (12) of titanium silicon nitride and a second sublayer (14) of titanium aluminum nitride. The composition of the titanium aluminum nitride, both in the first layer (4) and in the sublayer groups (1Oa)5 is (Ti x AI 1-x )N, wherein 0.4 ≤ x ≤ 0.6, The composition of the titanium silicon nitride sublayers (12) is (TiySi 1-y )N, wherein 0.85 ≤ y ≤ 0.98, and all of the silicon is in solid solution in the titanium silicon nitride such that no silicon phase or silicon nitride phase exists in this sublayer (12). The combined amount of aluminum and silicon present in the sublayer groups (10A) is narrowly controlled such that the sum of x and y is in the range of 1.38 to 1.46.

    Abstract translation: 一种用于基板(6)的耐磨多层氮化物硬涂层(2)。 硬涂层(2)包括氮化钛铝的第一层(4)和包括多个子层组(10a)的第二层(8)。 每个子层组(10a)包括氮化硅钛的第一子层(12)和氮化铝钛的第二子层(14)。 在第一层(4)和子层组(10a)5中的氮化铝钛的组成为(TixA1-x)N,其中0.4 = x = 0.6。氮化硅钛层(12 )是(TiySi1-y)N,其中0.85 = y = 0.98,并且所有的硅在氮化硅钛中是固溶体,使得在该子层(12)中不存在硅相或氮化硅相。 存在于子层组(10A)中的铝和硅的组合量被狭窄地控制,使得x和y之和在1.38至1.46的范围内。

    END MILL FOR ORBITAL DRILLING
    4.
    发明申请
    END MILL FOR ORBITAL DRILLING 审中-公开
    终端钻机进行钻孔

    公开(公告)号:WO2010090777A1

    公开(公告)日:2010-08-12

    申请号:PCT/US2010/020018

    申请日:2010-01-04

    Abstract: A center or non-center cutting end mill (10, 10', 10'') for orbital drilling includes a shank (12) having a shank diameter (20); a neck (14) having a neck diameter (22); a cutting head (16) having a cutting diameter (24); a corner radius (30); a dish angle (28); and a longitudinal axis (18), the cutting head including a forward cutting end (26) having a convexly curved section (29) located between the longitudinal axis and the corner radius, wherein the convexly curved section causes material removed from a workpiece to flow radially outward from an initial contact area (31) toward the corner radius, thereby minimizing the accumulation of material in a central portion (26a) of the forward cutting end.

    Abstract translation: 用于轨道钻孔的中心或非中心切割端铣刀(10,10',10“)包括具有柄直径(20)的柄(12); 具有颈部直径(22)的颈部(14); 具有切割直径(24)的切割头(16); 角半径(30); 盘角(28); 和纵向轴线(18),所述切割头包括具有位于纵向轴线和拐角半径之间的凸形弯曲部分(29)的前切割端(26),其中所述凸形弯曲部分使得从工件移除的材料流动 从初始接触区域(31)径向向外朝向拐角半径,从而最小化在前切割端的中心部分(26a)中材料的积聚。

    COATED ARTICLE WITH NANOLAYERED COATING SCHEME
    5.
    发明申请
    COATED ARTICLE WITH NANOLAYERED COATING SCHEME 审中-公开
    带有纳米涂层的涂层制品

    公开(公告)号:WO2009079184A2

    公开(公告)日:2009-06-25

    申请号:PCT/US2008/084838

    申请日:2008-11-26

    Abstract: An article including a substrate 22 and a coating is provided. The article may be a cutting insert 20 shown to improve performance in chip-forming material removal operations or a wear-resistant component for chipless forming operations. One wear-resistant coating scheme 40 has an underlayer 42 and top layer 46 containing aluminum, chromium, and nitrogen. The coating scheme 40 also includes a mediate multi-periodicity nanolayer coating scheme 44 containing titanium, aluminum, chromium and nitrogen. The mediate multi-periodicity nanolayer 44 coating scheme includes a plurality of sets of alternating layer arrangements 50, 52, 54, 56, 58, 60, 62. Each one of the alternating layer arrangements 50, 52, 54, 56, 58, 60, 62 has a base layer 64 comprising titanium, aluminum and nitrogen and a nanolayer region having a plurality of sets of alternating nanolayers 68, 70, 72, 74, 76, 78. Each set of alternating nanolayers 68, 70, 72, 74, 76, 78 has one nanolayer 82 having aluminum, chromium, titanium and nitrogen and another nanolayer 84 having aluminum, chromium, titanium and nitrogen. The base layer thickness G is smaller than the nanolayer region thickness F.

    Abstract translation: 提供了包括基底22和涂层的制品。 制品可以是所示的切削刀片20以改善切屑形成材料去除操作中的性能或用于无屑形成操作的耐磨部件。 一种耐磨涂层方案40具有包含铝,铬和氮的底层42和顶层46。 涂布方案40还包括含有钛,铝,铬和氮的中间多周期性纳米层涂布方案44。 中间多周期性纳米层44涂层方案包括多组交替层布置50,52,54,56,58,60,62。交替层布置50,52,54,56,58,60中的每一个 62具有包含钛,铝和氮的基底层64和具有多组交替纳米层68,70,72,74,76,78的纳米层区域。 76,78具有一个具有铝,铬,钛和氮的纳米层82以及另一个具有铝,铬,钛和氮的纳米层84。 基层厚度G小于纳米层区域厚度F.

    DRILL FOR MACHINING FIBER REINFORCED COMPOSITE MATERIAL
    6.
    发明申请
    DRILL FOR MACHINING FIBER REINFORCED COMPOSITE MATERIAL 审中-公开
    加工纤维增强复合材料的钻孔机

    公开(公告)号:WO2008013725A2

    公开(公告)日:2008-01-31

    申请号:PCT/US2007/016319

    申请日:2007-07-19

    Abstract: A diamond coated drill (10) capable of drilling holes in fiber reinforced composite materials. The drill (10) is made from a tungsten carbide (WC) substrate with cemented cobalt (Co) in a range between about 3 to 10 wt. % and a diamond coating having a thickness in a range between 3 to 20 microns. The drill (10) includes a shank (11), a longitudinal axis and includes two flutes (14 and 16) at a helix angle (18) that is in a range between 25 and 35 degrees with respect to the axis (12). A margin width (24) is maintained between about 5 to 10 percent of the drill diameter (22). A body clearance diameter (26) is maintained at between about 92 to 96 percent of the drill diameter (22). A web thickness (28) before splitting is about 20 to 30 percent of the drill diameter (22). A clearance angle or lip relief angle (36) is between about 10 and 20 degrees. A chisel edge angle (42) is between about 105 and 120 degrees. A chisel edge length (43) is up to about 0.035mm. A splitting angle (44) is between about 130 and 150 degrees. A notch angle (46) is between about 30 and 40 degrees with respect to the drill axis (12). A notch rake angle (48) lies between about -5 and 10 degrees. A split point angle (34) is between about 70 and 100 degrees, and preferably about 90 degrees.

    Abstract translation: 能够在纤维增强复合材料中钻孔的金刚石涂层钻头(10)。 钻(10)由碳化钨(WC)基体制成,其中钴(Co)含量为约3-10重量% %的金刚石涂层和厚度在3至20微米范围内的金刚石涂层。 钻头(10)包括柄部(11),纵向轴线并且包括处于相对于轴线(12)在25度和35度之间的范围内的螺旋角(18)的两个凹槽(14和16)。 边缘宽度(24)保持在钻头直径(22)的约5%至10%之间。 体间隙直径(26)保持在钻头直径(22)的约92%至96%之间。 分裂前的腹板厚度(28)约为钻头直径(22)的20%至30%。 间隙角或唇后角(36)在大约10度和20度之间。 凿锋角(42)在大约105度和120度之间。 凿子边缘长度(43)高达约0.035mm。 分裂角(44)在大约130和150度之间。 切口角度(46)相对于钻孔轴线(12)在大约30度和40度之间。 切口前角(48)位于大约-5度和10度之间。 分割点角度(34)在大约70度和100度之间,优选大约90度。

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