SUPERPLASTIC FORMING METHOD
    41.
    发明申请
    SUPERPLASTIC FORMING METHOD 审中-公开
    超塑成型方法

    公开(公告)号:WO01070428A1

    公开(公告)日:2001-09-27

    申请号:PCT/GB2001/000918

    申请日:2001-03-02

    Abstract: The present invention provides a method of superplastically forming at least two sheets of superplastically formable material to form a three dimensional article, the sheets being joined together along diffusion bonds (12) to form discrete cells (16) and wherein at least one gas path (18) is provided through the bond between cells; the method involves heating the sheets to a temperature at which they exhibit superplastic properties and injecting a gas between the sheets to expand the cells, the gas paths (18) allowing the injected gas to pas from cell to cell. According to the invention, the edges of the gas paths are locally heated (22), e.g. by laser heat treatment, to cause a change in the microstructure of the sheets in the heat-treated edge areas, which reduces the flow resistance of the edges under superplastic forming conditions as compared with the rest of the sheets and thereby reduces the propensity of the diffusion bonds (12) bordering the gas transfer holes to peel apart under the forces of the inert gas exerted on the sheets at the gas transfer paths (18).

    Abstract translation: 本发明提供了一种超塑性地形成至少两片超塑性成形材料以形成三维制品的方法,所述片材沿着扩散键(12)连接在一起以形成离散的细胞(16),并且其中至少一个气体路径 18)通过细胞之间的结合提供; 该方法包括将片材加热至表现出超塑性的温度,并在片材之间注入气体以使细胞膨胀,气体通道(18)允许注入的气体从细胞到细胞。 根据本发明,气体路径的边缘被局部加热(22),例如, 通过激光热处理,导致热处理边缘区域中的片材的微观结构的变化,这降低了在超塑性成形条件下边缘与其余片材相比的流动阻力,从而降低了 在气体传送通道(18)处施加在片材上的惰性气体的力作用下,使气体传输孔接合的扩散接合(12)分离。

    FORMING TUBULAR TITANIUM COMPONENTS
    42.
    发明申请
    FORMING TUBULAR TITANIUM COMPONENTS 审中-公开
    成形管状钛组件

    公开(公告)号:WO01054842A1

    公开(公告)日:2001-08-02

    申请号:PCT/GB2001/000328

    申请日:2001-01-26

    CPC classification number: B21D26/055 B21D26/033 B21D26/047 B21D37/16

    Abstract: A method of forming a plurality of large diameter tubular titanium components each suitable for use as a portion of a jet engine exhaust tube, the method includes the step of forming a large diameter titanium tube (1), and then subjecting the tube to a superplastic forming process. The superplastically formed titanium tube is then cut at at least one selected location (14, 15) along its length to sever it into at least two large diameter tubular titanium components (11, 12, 13). The titanium components (11, 12, 13) are particularly suitable for assembly to form an adjustable exhaust jet pipe for a VTOL aircraft.

    Abstract translation: 一种形成多个大直径管状钛成分的方法,每个都适合用作喷气式发动机排气管的一部分,所述方法包括形成大直径钛管(1)的步骤,然后将管经受超塑性 成型工艺。 然后在其长度的至少一个选定位置(14,15)处切割超塑性钛管,将其切割成至少两个大直径的管状钛部件(11,12,13)。 钛组件(11,12,13)特别适用于组装以形成用于垂直起落架飞机的可调排气喷管。

    A METHOD OF HOT FORMING LARGE SHEET METAL PARTS AND A FURNACE THEREFOR
    43.
    发明申请
    A METHOD OF HOT FORMING LARGE SHEET METAL PARTS AND A FURNACE THEREFOR 审中-公开
    一种热成型大型金属部件及其炉膛的方法

    公开(公告)号:WO01054841A1

    公开(公告)日:2001-08-02

    申请号:PCT/GB2001/000326

    申请日:2001-01-26

    Abstract: A large tubular sheet metal part (13) which is to be hot formed in a press is preheated in a portable furnace (17) and dropped from the furnace onto the punch portion (14) of the press tool outside the press. The punch portion (14) with the heated sheet metal part (13) supported on it is then translated into the press for the pressing step. A similar portable furnace which incorporates electric induction coils to heat a workpiece may be adapted for superlastic forming sheet metal.

    Abstract translation: 要在压机中热成型的大型管状金属片(13)在便携式炉(17)中被预热,并从炉子上落到压机外部的冲压工具的冲压部分(14)上。 随后将被加热的金属片(13)支撑在其上的冲压部分(14)被转换成用于压制步骤的压机。 结合电感线圈以加热工件的类似的便携式炉可适用于超塑性成形金属片。

    METHOD OF FORMING A TUBULAR BLANK INTO A STRUCTURAL COMPONENT AND DIE THEREFOR
    44.
    发明申请
    METHOD OF FORMING A TUBULAR BLANK INTO A STRUCTURAL COMPONENT AND DIE THEREFOR 审中-公开
    将管状空隙形成结构构件及其制造方法

    公开(公告)号:WO01023116A1

    公开(公告)日:2001-04-05

    申请号:PCT/US2000/021405

    申请日:2000-08-07

    Abstract: A method of forming an elongated tubular blank into a tubular structural component having a predetermined outer configuration, the method comprising: providing a shape imparting shell (66) from a low permeability, rigid material which includes an inner surface defining the predetermined shape, plugging the open ends of the tubular blank (A), placing the plugged blank into the shell, and forming the tubular blank into the tubular component by inductively heating axial portions (10, 12) of the blank by axially spaced conductors adjacent the shell while or before forcing gas at a high pressure into the plugged blank until the blank conforms to at least a portion of the inner surface of the shell to form the structural component.

    Abstract translation: 一种将细长管状坯料形成为具有预定外部构型的管状结构部件的方法,所述方法包括:从低渗透性刚性材料提供形状赋予外壳(66),所述刚性材料包括限定所述预定形状的内表面, 管状坯料(A)的敞开的端部,将堵塞的坯料放入外壳中,并且通过在或在之前感应地加热与坯件相邻的轴向间隔的导体的空腔的轴向部分(10,12),将管状坯料形成管状部件 迫使高压气体进入堵塞的坯料,直到坯料符合壳体的内表面的至少一部分以形成结构部件。

    SUPERPLASTIC FORMING WITH DIRECT ELECTRICAL HEATING
    45.
    发明申请
    SUPERPLASTIC FORMING WITH DIRECT ELECTRICAL HEATING 审中-公开
    具有直接电加热的超塑性成形

    公开(公告)号:WO1998020991A1

    公开(公告)日:1998-05-22

    申请号:PCT/US1997018171

    申请日:1997-10-08

    CPC classification number: B21D26/055 Y10S72/709

    Abstract: Sheet materials are superplastically formed and optionally diffusion bonded into structures, by directly electrically resistance heating the sheets and forming them with a controlled gas-mass flow while the dies (362) in which they are formed may remain relatively cool. The dies include electrodes and thermocouples placed therein, and gas interface ports that connect to the sheets to be formed to allow rapid formation of structures. Some of the gas interface ports may become sealably attached to the part during the formation process so that the structures may be removed from the dies hot, thus allowing a high die throughput.

    Abstract translation: 片状材料是超塑性的,并且任选地通过扩散结合到结构中,通过直接电阻加热片材并以受控的气体质量流量形成它们,同时形成它们的管芯(362)可以保持相对较冷。 模具包括放置在其中的电极和热电偶,以及连接到要形成的片材以允许快速形成结构的气体接口端口。 在形成过程中,一些气体接口端口可能变得可密封地附接到部件上,使得结构可以从模具中去除热,从而允许高的管芯生产量。

    HOLLOW TITANIUM BLADE MANUFACTURING
    46.
    发明申请
    HOLLOW TITANIUM BLADE MANUFACTURING 审中-公开
    中空钛片制造

    公开(公告)号:WO1995020441A1

    公开(公告)日:1995-08-03

    申请号:PCT/US1995001116

    申请日:1995-01-24

    CPC classification number: B21D26/055 Y10T29/49336 Y10T29/49343 Y10T29/49893

    Abstract: A titanium gas injection tube (18) is located within a counterbore (16) in the blade (10) halves which are to be bonded and formed. An internal stainless steel sleeve (24) is placed in the counterbore inside the titanium tube to resist bonding forces. An external stainless steel sleeve (28) is placed around the tube to resist gas pressure forces.

    Abstract translation: 钛气注射管(18)位于待粘合和形成的刀片(10)半部中的沉孔(16)内。 内部不锈钢套管(24)被放置在钛管内的沉孔中以抵抗结合力。 外管不锈钢套管(28)放置在管周围以抵抗气体压力。

    PROCESS FOR THE MANUFACTURE OF ASSEMBLIES COMPOSED OF TWO GLUED PIECES AND INCLUDING A FORMING STAGE
    47.
    发明申请
    PROCESS FOR THE MANUFACTURE OF ASSEMBLIES COMPOSED OF TWO GLUED PIECES AND INCLUDING A FORMING STAGE 审中-公开
    制造两个玻璃制品的组装过程,包括成型阶段

    公开(公告)号:WO1994004293A1

    公开(公告)日:1994-03-03

    申请号:PCT/FR1993000813

    申请日:1993-08-18

    Applicant: HISPANO-SUIZA

    CPC classification number: B21D26/055 B21D39/03 Y10T156/1025

    Abstract: Process for the manufacture of assemblies consisting of two formed and glued pieces. Both pieces (1 and 3) are disposed on a punch and die (2 and 4) provisionally separated in order to introduce sufficient pressure to hot form them. The punch and die are then brought together so that the surfaces previously coated with adhesive are face to face and contact one another. The invention is essentially advantageous in that no manual intervention is required.

    Abstract translation: 用于制造由两个成形和胶合件组成的组件的方法。 将两个片(1和3)放置在冲模和模具(2和4)上,以便将它们热压形成足够的压力。 然后将冲头和模具组合在一起,使得先前用粘合剂涂覆的表面面对面并且彼此接触。 本发明基本上是有利的,因为不需要手动干预。

    USING EXHAUST GAS MASS FLOW RATE TO CONTROL SUPERPLASTIC FORMING
    48.
    发明申请
    USING EXHAUST GAS MASS FLOW RATE TO CONTROL SUPERPLASTIC FORMING 审中-公开
    使用排气气体流量控制超塑性成形

    公开(公告)号:WO1993010923A1

    公开(公告)日:1993-06-10

    申请号:PCT/US1992007469

    申请日:1992-09-01

    CPC classification number: B21D26/055 Y10S72/709

    Abstract: A forming die (13) which includes a die cavity (19) contains a forming blank (17) composed of a metallic alloy having superplastic properties. The forming pressure in a pressurized space (18) adjacent the forming blank (17) is regulated by a pressure regulator (23). The volume of the die cavity (19) is determined, as is the mass of gas initially contained in the die cavity (19) at the beginning of the forming cycle. The total forming time is empirically determined. The average gas mass flow rate that will be exhausted from the die cavity (19) is calculated by dividing the total mass of gas initially contained in the die cavity (19) by the total forming time. A gas mass flow meter (33) fluidly communicates with the die cavity (19) and measures the mass flow rate of the gas (35) displaced by the forming blank (17) and exhausted from the die cavity (19). The gas mass flow meter (33) is continuously monitored during the forming cycle or a gas mass flow rate signal is fed back to the pressure regulator (23). The forming pressure is regulated by the pressure regulator (23) so that the gas mass flow rate exhausted from the die cavity (19) approximates the predetermined average gas mass flow rate.

    APPARATUS FOR FORMING METALLIC UNITS
    49.
    发明申请
    APPARATUS FOR FORMING METALLIC UNITS 审中-公开
    形成金属单位的装置

    公开(公告)号:WO1992011957A1

    公开(公告)日:1992-07-23

    申请号:PCT/CA1991000456

    申请日:1991-12-23

    Applicant: FRITSCH, Rudy

    CPC classification number: B21D26/055

    Abstract: Each of the metallic units (1) has a concave portion (5) bounded by a peripheral edge (7) which has a predetermined shape. The apparatus includes an upper member (11) and a lower member (13) and a tool (41) is adapted to be mounted on the upper or lower member (11, 13). The tool (41) comprises a wall-like structure (51) having a bottom edge (53) which defines a shape corresponding with the predetermined shape. The upper member (11) and lower member (13) are arranged to be movable relative one to the other, and a workpiece (1) is placed between the two members (11, 13) and the members (11, 13) are brought together until the bottom edge of the tool (41) abuts the workpiece (1) so that the tool (41) and workpiece (1) are clamped together in airtight engagement. Air under pressure is applied under the workpiece (1) to form the workpiece into a concave shape.

    Abstract translation: 每个金属单元(1)具有由具有预定形状的周缘(7)限定的凹部(5)。 该装置包括上部构件(11)和下部构件(13),并且工具(41)适于安装在上部构件(11)和下部构件(13)上。 工具(41)包括壁状结构(51),其具有限定与预定形状对应的形状的底部边缘(53)。 上部构件(11)和下部构件(13)被布置成可相对于彼此移动,并且工件(1)被放置在两个构件(11,13)之间,并且构件(11,13)被带入 一起直到工具(41)的底边缘邻接工件(1),使得工具(41)和工件(1)以气密接合方式被夹紧在一起。 在工件(1)下施加压力空气以将工件形成为凹形。

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