Method and apparatus for connecting a fluid reservoir with pipelines
    1.
    发明授权
    Method and apparatus for connecting a fluid reservoir with pipelines 有权
    用于将流体储存器与管道连接的方法和装置

    公开(公告)号:US6098848A

    公开(公告)日:2000-08-08

    申请号:US216119

    申请日:1998-12-18

    IPC分类号: B67D1/08 B67D7/02 B67D5/00

    摘要: The object of the present invention is to simplify the process of connecting a reservoir for charging and discharging 2 or more fluids with a pipeline for conveying said fluid and to assist the automation of this process.In the present invention, a reservoir, having, at its end face, 2 or more openings for fluids for charging and discharging 2 or more fluids respectively, is connected with pipelines by using a connecting means having flow paths for 2 or more fluids and, at its end face, 2 or more openings for fluids corresponding to each of the flow paths, and each of the respective fluids is passed, when by aligning the center of 1 of the openings for fluids of the reservoir end face with 1 of the openings for fluids of the connecting means end face and by linking said openings for fluids to each other, closed passage spaces are respectively formed which are common to the 1 or more other opening(s) for fluids of the reservoir end face and to the 1 or more corresponding other opening(s) of the connecting means end face respectively, and each fluid is passed via said spaces respectively.

    摘要翻译: 本发明的目的是简化连接用于对2个或更多个流体进行充气和排出的储存器与用于输送所述流体的管道并帮助该过程的自动化的过程。 在本发明中,在其端面具有2个以上分别用于对2个以上的流体进行充放电的流体的开口的储存器通过使用具有2个以上流体的流路的连接装置与管道连接, 在其端面处有两个或更多个对应于每个流动路径的流体的开口,并且当通过使用于储存器端面的流体的开口的1的中心与1个开口 对于连接装置端面的流体并且通过将流体的所述开口彼此连接,分别形成用于储存器端面的流体的1个或更多个其它开口和1或更多的其它开口的共同的封闭通道空间 分别连接装置端面的更多对应的其他开口,并且每个流体分别经过所述空间。

    AIRPLANE WING STRUCTURE
    2.
    发明申请
    AIRPLANE WING STRUCTURE 有权
    飞机结构

    公开(公告)号:US20090314892A1

    公开(公告)日:2009-12-24

    申请号:US12368397

    申请日:2009-02-10

    IPC分类号: B64C3/18

    摘要: A rib of an airplane wing is prevented from deforming due to a machining load when machining a rivet hole in parts where the rib and a skin are joined. With regard to a rib that provides a connection between first and second spars of the airplane wing, the rib is formed with mounting flanges secured to a skin via a rivet, a stringer through hole for a stringer to be positioned through, and first and second cutouts facing parts where the first and second spars and the skin are connected. Since reinforcing beads are formed along the mounting flanges and reinforcing flanges are formed so as to extend in the span direction from the edges of the stringer through hole and the first and second cutouts and be connected integrally to the mounting flanges, the stiffness of the rib toward a load in the vertical direction when drilling a rivet hole can be enhanced.

    摘要翻译: 当在肋和皮肤接合的部分中加工铆钉孔时,防止飞机机翼的肋由于加工负载而变形。 关于提供飞机机翼的第一和第二翼梁之间的连接的肋,肋形成有通过铆钉固定到皮肤的安装凸缘,用于桁条的纵梁通孔,以及第一和第二 切口面向与第一和第二翼梁和皮肤相连的部分。 由于沿着安装凸缘形成增强凸缘,并且加强凸缘形成为从跨过纵梁的边缘和第一和第二切口的跨度方向延伸并且与安装凸缘一体地连接,肋的刚度 可以提高钻孔时向垂直方向的载荷。

    Process and apparatus for recovering and reusing resist composition
    3.
    发明授权
    Process and apparatus for recovering and reusing resist composition 失效
    回收和再利用组合物的方法和装置

    公开(公告)号:US5084483A

    公开(公告)日:1992-01-28

    申请号:US425335

    申请日:1989-10-23

    CPC分类号: G03F7/162 Y10T137/2506

    摘要: The present invention relates to a process for recovering and reusing a resist composition which comprises the steps of (a) collecting resin composition scattered from a spinner during application of the resist composition onto silicon wafers and otherwise no longer used and to be disposed of as waste liquid; (b) introducing the resist composition into a recovery tank; (c) introducing, while measuring the viscosity of the resist composition in the recovery tank, a solvent into the recovery tank in accordance with the measured viscosity until the resist composition shows a predetermined viscosity; (d) discontinuing the solvent supply when the viscosity of the resist composition has reached a predetermined value; (e) transferring the resist composition with the predetermined viscosity to a storage tank; and (f) taking out, whenever necessary, the resist composition from the storage tank for reuse.

    Method for manufacturing an edge protector and die assemblies therefor
    4.
    发明授权
    Method for manufacturing an edge protector and die assemblies therefor 有权
    用于制造边缘保护器和模具组件的方法

    公开(公告)号:US07650773B2

    公开(公告)日:2010-01-26

    申请号:US12155215

    申请日:2008-05-30

    IPC分类号: B21D5/16 B21D13/10

    摘要: In primary press forming process, a piece of blank sheet metal is draw worked so as to form a preformed work piece (Wb) provided with a bent portion (a) substantially conforming to a three dimensional contour of a leading edge of a blade to be protected and extending along a longitudinal direction, and a pair of planar portions (b and c) extending from either side of the bent portion. In a secondary press forming process, the planar portions (b and c) of the preformed work piece are stretch formed into a final shape that conforms to the corresponding profile of the blade while the bent portion (a) of the preformed work piece is clamped and protected from deformation. In other words, the bent portion of an edge protector (100) is already given with the final shape of the edge protector by the primary press forming process while the planar portions (b and c) thereof are given with the final shape by the secondary press forming process so that the two press forming processes can be executed without interfering with each other, and only two relatively simple press forming processes are required for forming the complex three dimensional shape of the edge protector.

    摘要翻译: 在一次冲压成形工序中,对一块坯料金属进行牵引加工,以形成预成型工件(Wb),该预制工件设有弯曲部分(a),该弯曲部分(a)基本上符合叶片前缘的三维轮廓, 保护并沿着纵向方向延伸,以及从弯曲部分的任一侧延伸的一对平面部分(b和c)。 在二次冲压成形过程中,预成型工件的平面部分(b和c)被拉伸成最终形状,其与预成型工件的弯曲部分(a)夹紧 并防止变形。 换句话说,边缘保护器(100)的弯曲部分已经通过初次压制成形过程赋予了边缘保护器的最终形状,而其平面部分(b和c)被赋予最终形状的二次 压制成形过程,使得可以执行两个冲压成型工艺而不会彼此干涉,并且仅需要两个相对简单的冲压成形工艺来形成边缘保护器的复杂三维形状。

    Method for manufacturing an edge protector and die assemblies therefor
    5.
    发明申请
    Method for manufacturing an edge protector and die assemblies therefor 有权
    用于制造边缘保护器和模具组件的方法

    公开(公告)号:US20090044592A1

    公开(公告)日:2009-02-19

    申请号:US12155215

    申请日:2008-05-30

    IPC分类号: B21D5/02 B21D17/02 B21D39/20

    摘要: In primary press forming process, a piece of blank sheet metal is draw worked so as to form a preformed work piece (Wb) provided with a bent portion (a) substantially conforming to a three dimensional contour of a leading edge of a blade to be protected and extending along a longitudinal direction, and a pair of planar portions (b and c) extending from either side of the bent portion. In a secondary press forming process, the planar portions (b and c) of the preformed work piece are stretch formed into a final shape that conforms to the corresponding profile of the blade while the bent portion (a) of the preformed work piece is clamped and protected from deformation. In other words, the bent portion of an edge protector (100) is already given with the final shape of the edge protector by the primary press forming process while the planar portions (b and c) thereof are given with the final shape by the secondary press forming process so that the two press forming processes can be executed without interfering with each other, and only two relatively simple press forming processes are required for forming the complex three dimensional shape of the edge protector.

    摘要翻译: 在一次冲压成形工序中,对一块坯料金属进行牵引加工,以形成预成型工件(Wb),该预制工件设有弯曲部分(a),该弯曲部分(a)基本上符合叶片前缘的三维轮廓, 保护并沿着纵向方向延伸,以及从弯曲部分的任一侧延伸的一对平面部分(b和c)。 在二次冲压成形过程中,预成型工件的平面部分(b和c)被拉伸成最终形状,其符合叶片的相应轮廓,同时预成形工件的弯曲部分(a)被夹紧 并防止变形。 换句话说,边缘保护器(100)的弯曲部分已经通过初次压制成形过程赋予了边缘保护器的最终形状,而其平面部分(b和c)被赋予最终形状的二次 压制成形过程,使得可以执行两个冲压成型工艺而不会彼此干涉,并且仅需要两个相对简单的冲压成形工艺来形成边缘保护器的复杂三维形状。

    Adhesive material for hemostasis and a method for hemostasis
    6.
    发明授权
    Adhesive material for hemostasis and a method for hemostasis 失效
    用于止血的粘合剂材料和止血方法

    公开(公告)号:US5690610A

    公开(公告)日:1997-11-25

    申请号:US209537

    申请日:1994-03-10

    IPC分类号: A61F13/00 A61F13/02 A61F13/15

    摘要: A sticking material for hemostasis has a flexible strip-shaped base member having a high recovery property, a main surface, and side edges extending in a first longitudinal direction. An adhesive layer is disposed on the main surface of the base member. A pad is disposed on the adhesive layer and extends in a second longitudinal direction substantially transverse to the first longitudinal direction such that a space is defined between the pad and each of the side edges of the base member. The pad is of a size sufficient to exert pressure at a puncture area including punctures of both a blood vessel and a skin surface. The pad has a slight elasticity and a hardness capable of securely exerting pressure on the punctures by a shrinking action of the base member when the base member is adhered to the skin surface while being stretched to secure the pad over the punctures. A pressure plate having a width equal to or less than the width of the base member may be interposed between the base member and the pad to enable the pad to be more strongly pressed against the puncture area. The pressure plate has a size greater than the size of the pad. Hemostasis is conducted readily and effectively without the possibility of blood leaking from the puncture area.

    摘要翻译: 用于止血的粘附材料具有具有高恢复性能的柔性条状基底构件,主表面和沿第一纵向方向延伸的侧边缘。 粘合剂层设置在基体的主表面上。 衬垫设置在粘合剂层上并且在基本上横向于第一纵向方向的第二纵向方向上延伸,使得在衬垫和基部构件的每个侧边缘之间限定空间。 衬垫的尺寸足以在包括血管和皮肤表面的穿刺的穿刺区域施加压力。 衬垫具有轻微的弹性和硬度,当基部构件被拉伸以将垫固定在穿刺上时,基底构件的收缩作用可以可靠地施加穿刺上的压力。 宽度等于或小于基部构件的宽度的压板可以插入在基部构件和衬垫之间,使得垫更牢固地压靠穿刺区域。 压板的尺寸大于垫的尺寸。 止血是容易且有效地进行的,而不会引起穿刺区域的血液泄漏。

    Airplane wing structure
    7.
    发明授权
    Airplane wing structure 有权
    飞机翼结构

    公开(公告)号:US08056859B2

    公开(公告)日:2011-11-15

    申请号:US12368397

    申请日:2009-02-10

    IPC分类号: B64C1/06

    摘要: A rib of an airplane wing is prevented from deforming due to a machining load when machining a rivet hole in parts where the rib and a skin are joined. With regard to a rib that provides a connection between first and second spars of the airplane wing, the rib is formed with mounting flanges secured to a skin via a rivet, a stringer through hole for a stringer to be positioned through, and first and second cutouts facing parts where the first and second spars and the skin are connected. Since reinforcing beads are formed along the mounting flanges and reinforcing flanges are formed so as to extend in the span direction from the edges of the stringer through hole and the first and second cutouts and be connected integrally to the mounting flanges, the stiffness of the rib toward a load in the vertical direction when drilling a rivet hole can be enhanced.

    摘要翻译: 当在肋和皮肤接合的部分中加工铆钉孔时,防止飞机机翼的肋由于加工负载而变形。 关于提供飞机机翼的第一和第二翼梁之间的连接的肋,肋形成有通过铆钉固定到皮肤的安装凸缘,用于桁条的纵梁通孔,以及第一和第二 切口面向与第一和第二翼梁和皮肤相连的部分。 由于沿着安装凸缘形成增强凸缘,并且加强凸缘形成为从跨过纵梁的边缘和第一和第二切口的跨度方向延伸并且与安装凸缘一体地连接,肋的刚度 可以提高钻孔时向垂直方向的载荷。

    Method For Manufacturing Steel Plate-Shaped Component, Pole Parking, And Cold Forging Die
    8.
    发明申请
    Method For Manufacturing Steel Plate-Shaped Component, Pole Parking, And Cold Forging Die 审中-公开
    制造钢板组件,杆停车和冷锻模的方法

    公开(公告)号:US20110139572A1

    公开(公告)日:2011-06-16

    申请号:US12939648

    申请日:2010-11-04

    IPC分类号: F16H61/22 B21J5/02 B21J13/02

    CPC分类号: B21K1/76 B21J5/02 F16H63/3425

    摘要: The present invention provides a method for manufacturing a steel plate-shaped component which can increase the yield and the working efficiency. When a steel plate-shaped component (1) such as a pole parking is manufactured, a steel disk-shaped initial material (10) is vertically placed in a cavity (41) of a dice (40) of a cold forging die so that the thickness direction of the initial material (10) is perpendicular to a pressing direction. The initial material (10) is pressed through cold forging against the peripheral side portion (11) by a punch (42) while the initial thickness of the initial material (10) is maintained substantially as it is, whereby an approximate component (20) approximating the plate-shaped component (1) is obtained. Subsequently, a margin portion (25) of the approximate component (20) is removed, whereby a half-finished product (30) is obtained. The half-finished product (30) is subjected to cutting work, carburizing processing, and so on, whereby the plate-shaped component (1) is obtained.

    摘要翻译: 本发明提供一种能够提高成品率和工作效率的钢板状部件的制造方法。 当制造诸如柱形停车场的钢板状部件(1)时,将钢盘形初始材料(10)垂直放置在冷锻模具的骰子(40)的空腔(41)中,使得 初始材料(10)的厚度方向垂直于按压方向。 初始材料(10)通过冲头(42)对周边侧部分(11)进行冷锻压制,同时初始材料(10)的初始厚度基本保持原样,由此近似组分(20) 获得板状部件(1)的近似。 接着,除去大致成分(20)的边缘部(25),得到半成品(30)。 对半成品(30)进行切割加工,渗碳处理等,得到板状部件(1)。

    Method of manufacturing elliptic deep-drawn products
    9.
    发明授权
    Method of manufacturing elliptic deep-drawn products 有权
    椭圆形深冲制品的制造方法

    公开(公告)号:US07121128B2

    公开(公告)日:2006-10-17

    申请号:US10828301

    申请日:2004-04-21

    CPC分类号: B21D22/16

    摘要: A method of manufacturing an elliptic deep-drawn product including a first step of providing an intermediate product and a second step of providing an end product. In the first step, a rotary forming die is used to form in a blank a substantially round formed portion of a U-shaped cross-section. In the second step, the formed portion is deformed at its semicircular portion by press working to form an elliptic portion, being formed into a final shape.

    摘要翻译: 一种制造椭圆深拉制品的方法,包括提供中间产品的第一步骤和提供最终产品的第二步骤。 在第一步骤中,使用旋转成型模具在坯件中形成U形横截面的大致圆形的部分。 在第二步骤中,成形部分通过冲压加工在其半圆形部分处变形,以形成椭圆形部分,形成最终形状。

    Process and apparatus for recovering and reusing resist composition
    10.
    发明授权
    Process and apparatus for recovering and reusing resist composition 失效
    用于回收和再利用抗蚀剂组合物的方法和设备

    公开(公告)号:US4967782A

    公开(公告)日:1990-11-06

    申请号:US251224

    申请日:1988-08-25

    CPC分类号: G03F7/162 Y10T137/2506

    摘要: The present invention relates to a tank for use in recovering and reusing resist compositions, which comprises (a) means for measuring the viscosity of a previously used resist composition introduced into the recovery tank; (b) line means for feeding a solvent into the recovery tank; (c) line means for introducing the previously used resist composition into the recovery tank; (d) line means for discharging the viscosity adjusted resist composition from the recovery tank; and (e) means for opening the solvent feed line means described above in (b) when the viscosity as measured by the viscosity measuring means described above in (a) is higher than a predetermined viscosity, and means for closing the same when the predetermined viscosity is reached.

    摘要翻译: PCT No.PCP / JP87 / 01035 Sec。 371日期1988年8月25日第 102(e)日期1988年8月25日PCT Filted 1987年12月25日PCT公布。 出版物WO88 / 05179 日期:1988年7月14日。本发明涉及用于回收和再利用抗蚀剂组合物的罐,其包括(a)测量引入回收罐中的先前使用的抗蚀剂组合物的粘度的装置; (b)用于将溶剂进料到回收罐中的管路装置; (c)用于将先前使用的抗蚀剂组合物引入回收罐的管线装置; (d)用于从回收罐中排出粘度调节的抗蚀剂组合物的管线装置; 和(e)当(a)中所述的粘度测量装置测量的粘度高于预定粘度时,用于打开上述(b)中所述的溶剂供给管路装置的装置,以及当预定的 达到粘度。