公开(公告)号：US11839928B2

公开(公告)日：2023-12-12

申请号：US17823659

申请日：2022-08-31

申请人： SCHUNK SONOSYSTEMS GMBH

发明人： Sebastian Rühl ,  Peter Wagner ,  Udo Wagenbach ,  Heiko Strobel

IPC分类号： B23K20/00 ,  B23K20/10 ,  B23K20/18

CPC分类号： B23K20/106 ,  B23K20/004 ,  B23K20/18

摘要： An ultrasonic metal welding device for welding electrical conductors using a compression chamber that is adjustable at least n height and that is delimited on opposite sides by a section of a sonotrode as a first delimiting surface and by at least one section of a counter electrode (156) as a second delimiting surface, wherein for welding, the counter electrode and the sonotrode are displaced relative to one another. The counter electrode used is one that comprises sections (152, 154) of geometrically different working surfaces or is composed of at least two sections that are displaceable relative to one another.

公开(公告)号：US20100270360A1

公开(公告)日：2010-10-28

申请号：US12757412

申请日：2010-04-09

申请人： Michael J. WALLIS

发明人： Michael J. WALLIS

IPC分类号： B23K31/02 ,  B23K28/00

CPC分类号： B32B15/01 ,  B23K20/023 ,  B23K20/16 ,  B23K20/18 ,  B23K20/233 ,  B23K20/24 ,  B23K2101/001 ,  B23K2103/12 ,  B23K2103/14 ,  C21D9/0068 ,  C21D9/20 ,  C21D9/24 ,  C22C14/00 ,  C22F1/00 ,  C22F1/183 ,  F01D5/147 ,  F01D5/282 ,  F01D5/286 ,  F05D2230/00 ,  F05D2230/90 ,  F05D2260/95 ,  Y10T29/49316 ,  Y10T29/4932 ,  Y10T29/49337

摘要： A method of manufacturing an aerofoil structure to have a portion with an increased erosion resistance, the method comprising: providing one or more titanium elements (2, 4, 6) and a beta-stabilizing material (8); wherein the one or more elements (2, 4, 6) have an alpha-beta microstructure; assembling the one or more elements (2, 4, 6) and the beta-stabilizing material (8) such that the beta-stabilizing material (8) is adjacent to the one or more elements (2, 4, 6); and heating the assembly such that the beta-stabilizing material (8) diffuses into an adjacent portion of the one or more elements (2, 4, 6), causing the adjacent portion of the one or more elements (2, 4, 6) to have a beta microstructure which provides an increased erosion resistance.

摘要翻译： 一种制造机翼结构以具有增加的抗侵蚀性的部分的方法，所述方法包括：提供一种或多种钛元素（2,4,6）和β-稳定材料（8）; 其中所述一个或多个元件（2,4,6）具有α-β微结构; 组装所述一种或多种元件（2,4,6）和所述β-稳定材料（8），使得所述β-稳定材料（8）与所述一个或多个元件（2,4,6）相邻; 并且加热所述组件使得所述β稳定材料（8）扩散到所述一个或多个元件（2,4,6）的相邻部分中，使得所述一个或多个元件（2,4,6）的相邻部分， 具有提供增加的耐腐蚀性的β微结构。

公开(公告)号：US06913842B2

公开(公告)日：2005-07-05

申请号：US10031369

申请日：2001-05-18

申请人： Yasushi Hasegawa ,  Yasuhiro Shinohara ,  Yutaka Takagi

发明人： Yasushi Hasegawa ,  Yasuhiro Shinohara ,  Yutaka Takagi

IPC分类号： B23K13/01 ,  B23K20/02 ,  B23K20/16 ,  B23K20/18 ,  B23K35/00 ,  B23K35/30 ,  B32B15/04 ,  B32B3/10 ,  B32B3/20 ,  B32B15/18

CPC分类号： C22C38/002 ,  B23K13/01 ,  B23K20/023 ,  B23K20/16 ,  B23K20/18 ,  B23K35/001 ,  B23K35/002 ,  B23K35/004 ,  B23K35/005 ,  B23K35/3033 ,  B23K35/3093 ,  C22C38/02 ,  C22C38/04 ,  C22C38/12 ,  C22C38/14 ,  C22C38/18 ,  Y10T428/12819 ,  Y10T428/12937 ,  Y10T428/12951 ,  Y10T428/12979 ,  Y10T428/24562 ,  Y10T428/24744

摘要： A precision machine part is made of a plurality of pieces with a transient liquid phase diffusion bonding alloy provided between the pieces to bond them together. The precision machine part has one or more conveyance passages formed in it, has a longitudinal axis and is configured to permit passage of liquid or gas through the conveyance passage from a pipe line or cylinder. The pieces of the precision machine part are adhered to each other by transient liquid phase bonding with a ribbon of an amorphous bonding alloy. The bonding alloy can contain 1 to 10 atomic % V or can contain 1 to 15 atomic % of B or P or a mixture of B and P and 1 to 10 atomic % V, the balance being Fe and unavoidable impurities, and can exhibit an amount of contraction in a bonding stress loading direction caused by plastic deformation in the bonding process of not more than 5%. The bonding alloy may be an amorphous Ni-based alloy.

摘要翻译： 精密机械部件由多个片材构成，其中设置有两个片之间的瞬态液相扩散接合合金，以将它们结合在一起。 精密机械部件具有形成在其中的一个或多个输送通道，具有纵向轴线并且构造成允许液体或气体从管线或圆筒通过输送通道。 精密机械部件通过与非晶接合合金带的瞬态液相接合而相互粘合。 接合合金可以含有1至10原子％V或可含有1至15原子％的B或P，或B或P的混合物和1至10原子％的V，余量为Fe和不可避免的杂质，并且可以显示出 接合过程中由塑性变形引起的接合应力加载方向的收缩量不大于5％。 接合合金可以是非晶Ni基合金。

公开(公告)号：US20040200887A1

公开(公告)日：2004-10-14

申请号：US10812969

申请日：2004-03-31

申请人： SNECMA MOTEURS

发明人： Jean-Michel Franchet ,  Gilles Klein ,  Patrick Gesmier

IPC分类号： B23K035/12

CPC分类号： B21D26/055 ,  B21D53/78 ,  B23K20/023 ,  B23K20/18 ,  B23K26/32 ,  B23K26/34 ,  B23K35/22 ,  B23K35/224 ,  B23K2101/001 ,  B23K2103/14 ,  F01D5/147 ,  Y10T29/49339

摘要： The method of fabricating a hollow mechanical part of the invention includes a step b) of depositing an anti-diffusion substance in a predefined pattern on at least one face of primary parts to be assembled together. In characteristic manner, said step b) is performed in application of the following sequence of operations: b1) applying a layer of anti-diffusion substance comprising a powder over the entire surface of said at least one face of the primary parts; b2) localized sintering of the anti-diffusion substance in said predefined pattern by the heating that results from localized application of a laser beam along a track made up of at least one zone, thereby producing, in said at least one zone, both bonds between the particles of powder and also a diffusion phenomenon between the particles of powder and the material of said at least one face of the primary part; and b3) removing the anti-diffusion substance from the regions that are not subjected to the laser beam. The invention is applicable to fabricating a hollow blade for a turbomachine.

摘要翻译： 制造本发明的中空机械部件的方法包括步骤b）在要组装在一起的主要部件的至少一个面上以预定图案沉积防扩散物质。 以特征方式，在应用以下操作顺序的情况下执行所述步骤b）：b1）在主要部件的所述至少一个面的整个表面上施加包含粉末的防扩散物质层; b2）通过由沿着由至少一个区域构成的轨道的激光束的局部施加而导致的加热而使所述预定图案中的防扩散物质局部烧结，从而在所述至少一个区域中产生两个 粉末颗粒以及粉末颗粒与主要部分的所述至少一个表面的材料之间的扩散现象; 以及b3）从不经受激光束的区域去除防扩散物质。 本发明可应用于制造用于涡轮机的中空叶片。

公开(公告)号：US06467168B2

公开(公告)日：2002-10-22

申请号：US09799044

申请日：2001-03-06

申请人： Michael J Wallis

发明人： Michael J Wallis

IPC分类号： B23P1500

CPC分类号： B21D26/055 ,  B21D53/045 ,  B23K20/023 ,  B23K20/18 ,  B23K2101/001 ,  F01D5/147 ,  F05D2220/324 ,  Y10T29/49336 ,  Y10T29/49339 ,  Y10T29/49341

摘要： A method of manufacturing a gas turbine engine fan blade (10) comprises forming three metal workpieces (30,32,34). The metal workpieces (30,32,34) are assembled into a stack (36) so that the flat surfaces (38,42,46,48) are in mating abutment. Heat and pressure is applied across the thickness of the metal workpieces (30,32,34) to diffusion bond the metal workpieces (30,32,34) together to form an integral structure (80). The integral structure (80) is upset forged at one end (58) to produce an increase in thickness (82) for forming the blade root (26). The upset forged integral structure (80) is then hot creep formed and superplastically formed to produce the required aerofoil shape and the thickened end (82) is machined to form the blade root (26). The method enables thinner metallic workpieces with better microstructure to be used and increases the yield of metallic workpieces.

摘要翻译： 一种制造燃气涡轮发动机风扇叶片（10）的方法包括形成三个金属工件（30,32,34）。 金属工件（30,32,34）组装成堆叠（36），使得平坦表面（38,42,46,48）处于配合邻接处。 在金属工件（30,32,34）的厚度上施加热和压力以将金属工件（30,32,34）扩散连接在一起以形成整体结构（80）。 整体结构（80）在一端锻造（58）以产生用于形成叶根（26）的厚度（82）的增加。 镦锻锻造的整体结构（80）然后形成热蠕变并且超塑性地形成以产生所需的机翼形状，并且加厚端（82）被加工以形成叶根（26）。 该方法使得能够使用具有更好的微观结构的较薄的金属工件并增加金属工件的产量。

公开(公告)号：US5505256A

公开(公告)日：1996-04-09

申请号：US412210

申请日：1995-03-27

申请人： James E. Boardman ,  John O. Fowler

发明人： James E. Boardman ,  John O. Fowler

IPC分类号： B21D53/04 ,  B23K20/18 ,  F28D9/00 ,  F28F3/14

CPC分类号： B23K20/18 ,  B21D53/045 ,  F28D9/0031 ,  B23K2201/14 ,  Y10T29/49371

摘要： It is common practice to assemble heat exchangers from a multitude of pre-formed and sometimes extremely delicate pieces. The pieces have to be held in jigs along with appropriately placed braze material and then heated to achieve brazing. The invention takes advantage of the ability which some materials have, to considerably extend their areas without rupturing, by using such materials in that they are assembled in the flat condition and then diffusion bonded, followed by inflation of the parts of the assembly which are to provide the fluid passageways, inlet manifolds and headers. The construction of heat exchangers is thus considerably simplified.

摘要翻译： 通常的做法是从大量预先形成的和有时非常细腻的部件组装热交换器。 必须将夹具与适当放置的钎焊材料一起夹在夹具中，然后加热以实现钎焊。 本发明利用某些材料具有的能力，通过使用这些材料来显着地扩展它们的面积而不破裂，因为它们被组装在平坦状态然后扩散粘合，随后将组件的部分充气到 提供流体通道，入口歧管和集管。 因此，热交换器的结构大大简化。

公开(公告)号：US5479705A

公开(公告)日：1996-01-02

申请号：US255764

申请日：1994-06-07

申请人： John O. Fowler ,  Brian Richardson

发明人： John O. Fowler ,  Brian Richardson

IPC分类号： B21D26/055 ,  B21D53/04 ,  B23K20/02 ,  B23K20/18 ,  B23P15/04

CPC分类号： B21D26/055 ,  B21D53/045 ,  B23K20/023 ,  B23K20/18 ,  B23K2201/001 ,  Y10T29/49339

摘要： A plurality of titanium sheets are assembled into a stack. At least one of the sheets is provided with a stop off material on one of its surfaces to prevent diffusion bonding at predetermined positions. The edges of the sheets are welded together and a pipe is welded to the stack to interconnect with the stop off material to form a sealed assembly. The assembly is heated and externally pressurized to diffusion bond the sheets together. The integral structure so formed is heated and opposite ends of the integral structure are twisted relatively to contour the integral structure to a predetermined shape. The integral structure is internally pressurized to break the adhesive bonds. The integral structure is heated and internally pressurized to superplastically form one sheet to produce an article, e.g. a fan blade.

摘要翻译： 将多个钛片组装成堆叠。 至少一个片材在其一个表面上设置有停止材料，以防止在预定位置的扩散接合。 板的边缘被焊接在一起，并且管被焊接到堆叠以与停止材料互连以形成密封组件。 组件被加热和外部加压以将片材扩散粘合在一起。 这样形成的整体结构被加热，并且整体结构的相对端被相对扭转以将整体结构轮廓化为预定的形状。 整体结构内部加压以破坏粘结。 整体结构被加热并在内部被加压以超塑性地形成一片以产生制品，例如。 风扇叶片。

公开(公告)号：US5273202A

公开(公告)日：1993-12-28

申请号：US057550

申请日：1993-05-06

申请人： Joseph Douglas

发明人： Joseph Douglas

IPC分类号： B21D26/055 ,  B23K20/14 ,  B23K20/18 ,  B23K20/00 ,  B23K20/26

CPC分类号： B21D26/055 ,  B23K20/14 ,  B23K20/18

摘要： A stack of titanium sheets are placed between a pair of pressurizable chambers in a vacuum chamber. One of the mating surfaces of each pair of mating surfaces has had a stop off material applied in a desired pattern to prevent diffusion bonding. A pump evacuates the vacuum chamber and heaters heat the stack to evaporate volatile binders from the stop off. When all the binder has been removed the stack is heated and the pressure in the pressurizable chambers is increased to cause a pair of resilient members to apply pressure on the stack to diffusion bond the sheets together. The volatile binder is removed quickly and oxidation of the titanium is prevented during baking out of the binder. The integral structure is then heated and internally pressurized to superplastically form one of the sheets to produce an article of predetermined shape. No welding of the sheets before bonding is required.

摘要翻译： 将一叠钛片放置在真空室中的一对可加压室之间。 每对配合表面的一个配合表面具有以期望的图案施加的停止材料以防止扩散粘合。 泵抽真空室，加热器加热堆，使挥发性粘合剂从停止点蒸发。 当所有粘合剂已经被去除时，堆叠被加热并且可加压室中的压力增加，以使一对弹性构件对叠层施加压力以将片材扩散粘合在一起。 快速去除挥发性粘合剂，并在烘烤出粘合剂之前防止钛的氧化。 然后将整体结构加热并内部加压以超塑性地形成其中一个片材以产生预定形状的制品。 在焊接之前不需要焊接片材。

公开(公告)号：US5263638A

公开(公告)日：1993-11-23

申请号：US53335

申请日：1993-04-28

申请人： Joseph Douglas

发明人： Joseph Douglas

IPC分类号： B21D53/04 ,  B23K20/14 ,  B23K20/18

CPC分类号： B23K20/18 ,  B21D53/045 ,  B23K20/14

摘要： A stack of titanium sheets are placed on a worktable in a vacuum chamber. One of the mating surfaces of each pair of mating surfaces has had a stop off material applied in a desired pattern to prevent diffusion bonding. A pump evacuates the vacuum chamber and heaters heat the stack to evaporate volatile binder from the stop off. When all the binder has been removed the worktable is moved relative to an electron beam gun to weld the edges of the sheets together to form a sealed assembly. The volatile binder is removed quickly and oxidation of the titanium is prevented during baking out of the binder. The sealed assembly is then heated and externally pressurised to diffusion bond the sheets together. The integral structure is then heated and internally pressured to superplastically form one of the sheets to produce an article of predetermined shape.

摘要翻译： 将一叠钛片放置在真空室中的工作台上。 每对配合表面的一个配合表面具有以期望的图案施加的停止材料以防止扩散粘合。 泵抽真空室，加热器加热堆，使挥发性粘合剂从停止点蒸发。 当所有粘合剂已经被去除时，工作台相对于电子束枪移动，以将片材的边缘焊接在一起以形成密封组件。 快速去除挥发性粘合剂，并在烘烤出粘合剂之前防止钛的氧化。 然后将密封组件加热并进行外部加压以将片材扩散粘合在一起。 然后将整体结构加热并在内部压力以超塑性地形成其中一个片材以产生预定形状的制品。

公开(公告)号：US4882823A

公开(公告)日：1989-11-28

申请号：US149216

申请日：1988-01-27

申请人： Edward D. Weisert ,  John R. Fischer ,  William L. McCauley

发明人： Edward D. Weisert ,  John R. Fischer ,  William L. McCauley

IPC分类号： B21D26/055 ,  B23K20/18

CPC分类号： B21D26/055 ,  B23K20/18 ,  Y10T29/18 ,  Y10T29/49339 ,  Y10T29/49805

摘要： A method is set forth of forming a hollow structure having a varying mass distribution. Two sheets of a diffusion bondable and superplastic formable material are formed with one flat surface and an opposite surface contoured to have a selected mass distribution. A stop-off material is applied between selected non-peripheral portions of each of the flat surfaces whereat diffusion bonding is to be prevented and superplastic forming is to be required. An intermediate flat core sheet may also be present. The flat surfaces are positioned in abutting relation to each other or to the intermediate flat core sheet. The sheets are subjected to diffusion bonding conditions. The sheets are superplastically formed to expand them apart against a die. The invention also provides a method of preinflating contoured sheets prior to superplastically forming them to avoid truss core rupture. Hollow aircraft engine components are formed by the methods.

摘要翻译： 阐述形成具有不同质量分布的中空结构的方法。 两片可扩散粘合和超塑性可成形材料形成有一个平坦表面和相对的表面，具有选定的质量分布。 在每个平坦表面的选定的非外围部分之间施加停止材料，其中需要防止扩散接合，并且需要超塑性成形。 也可以存在中间扁平芯片。 平坦的表面彼此邻接或与中间平的芯片片相对置。 片材经受扩散接合条件。 片材被超塑性地形成以使它们相对于模具分开。 本发明还提供了一种在超塑性成型之前对成形片材进行预压缩以避免桁架芯断裂的方法。 中空飞机发动机部件由方法形成。