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公开(公告)号：US5063662A
公开(公告)日：1991-11-12
申请号：US641327
申请日：1991-01-15
CPC分类号： B23P15/04 , B21D11/14 , Y10T29/49336 , Y10T29/49339
摘要： An untwisted hollow blade with internal reinforcing ribs is formed by diffusion bonding two halves. A predominate portion of the blade twist is accomplished by gravity creep deforming against a supporting die, aided by applying twisting moments at the ends. The blade is free to move axially at one end. Simultaneous heat soak for solution heat treatment minimizes overall grain growth. Later, hot forming between heated dies is supplemented with internal blade pressure after die closing. Metal flow is more easily predictable whereby finite element analysis may establish the proper starting form.
摘要翻译： 通过扩散接合两半形成具有内部加强肋的未扭绞中空叶片。 叶片扭转的主要部分是通过在支撑模具上的重力蠕变变形来实现的，辅助通过在端部施加扭转力矩。 刀片可在一端自由移动。 用于固溶热处理的同时热浸最小化整体晶粒生长。 之后，加热后的模具之间的热成型在封闭后补充内部刀片压力。 金属流动更容易预测，有限元分析可以建立适当的起始形式。
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公开(公告)号：US5448829A
公开(公告)日：1995-09-12
申请号：US189384
申请日：1994-01-31
IPC分类号： B21D26/055 , B23P15/00
CPC分类号： B21D26/055 , Y10T29/49336 , Y10T29/49343 , Y10T29/49893
摘要： 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.
摘要翻译： 钛气注射管18位于要粘合和形成的刀片（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。
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公开(公告)号：US4301584A
公开(公告)日：1981-11-24
申请号：US117169
申请日：1980-01-31
IPC分类号： B21D26/053 , B21D26/059 , B23K20/00 , B23P15/04 , B21D53/78 , B23K31/00
CPC分类号： B21D26/059 , B21D26/053 , B21D53/78 , B23P15/04 , Y10T29/49337 , Y10T29/49805 , Y10T29/4981
摘要： Disclosed is an improved method of fabricating boron fiber and aluminum matrix composite structures, especially gas turbine compressor blades having titanium metal skins. Titanium skins and boron aluminum composite cores are preformed by gas pressure and hard dies prior to hot pressing. The composite sheets of the core are preformed with the use of expendable carrier sheets, which hold the stacked sheets firmly as both the carrier sheets and composites are shaped through moderate temperature and gas pressure against a hard die. The preforming permanently shapes and lightly bonds the composite sheets. The skins are preformed in an analogous process using gas pressurization of a metal envelope into die cavities. The skins and composite core are then hot pressed in hard dies to form the finished part.
摘要翻译： 公开了一种改进的制造硼纤维和铝基复合结构的方法，特别是具有钛金属表皮的燃气轮机压缩机叶片。 钛皮和硼铝复合芯通过气压和硬模在热压之前进行。 芯片的复合片材通过使用消耗性载体片进行预成型，这两种载体片材牢固地保持堆叠的片材，因为载体片和复合材料都通过适度的温度和气体压力对着硬模具成形。 预成型件永久地形成并轻轻地粘合复合片材。 皮肤以类似的方法进行，其中使用气体加压金属外壳进入模腔。 然后将表皮和复合芯材在硬模具中热压成型成品。
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公开(公告)号：US4729804A
公开(公告)日：1988-03-08
申请号：US946474
申请日：1986-12-24
申请人： James R. Dillner
发明人： James R. Dillner
摘要： A workholder (6) has a contoured bonding surface (7), which essentially matches a contoured surface (4) of an airfoil (1). A plurality of studs (8) are disposed within a plurality of tapped holes (9) located about the workholder bonding surface. In operation, the studs are extended outwardly from the surface, and both the studs and bonding surface are contacted with a release agent (10). A curable resinous material (11) is applied to the bonding surface and studs, and an airfoil positioned next to the bonding surface, sandwiching the resinous material therebetween. After curing, a plurality of tapped holes (13) are formed in resin layer (11), with the extended studs fixably positioning the airfoil relative to the workholder. Removing the studs provides heatless release of the airfoil from the workholder.
摘要翻译： 工作台（6）具有与机翼（1）的轮廓表面（4）基本相匹配的轮廓结合表面（7）。 多个螺栓（8）设置在位于工件接合表面周围的多个螺纹孔（9）内。 在操作中，螺栓从表面向外延伸，并且螺栓和粘合表面都与脱模剂（10）接触。 将粘合表面和螺栓以及位于接合表面旁边的翼型件施加固化树脂材料（11），将树脂材料夹在其间。 固化后，在树脂层（11）中形成多个螺纹孔（13），其中延伸的螺柱可固定地将翼型件相对于夹持器定位。 卸下螺柱提供了翼型件从加工支架的无热释放。
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公开(公告)号：US4685660A
公开(公告)日：1987-08-11
申请号：US829050
申请日：1986-02-13
申请人： James R. Dillner
发明人： James R. Dillner
摘要： A workholder (6) has a contoured bonding surface (7), which essentially matches a contoured surface (4) of an airfoil (1). A plurality of studs (8) are disposed within a plurality of tapped holes (9) located about the workholder bonding surface. In operation, the studs are extended outwardly from the surface, and both the studs and bonding surface are contacted with a release agent (10). A curable resinous material (11) is applied to the bonding surface and studs, and an airfoil positioned next to the bonding surface, sandwiching the resinous material therebetween. After curing, a plurality of tapped holes (13) are formed in resin layer (11), with the extended studs fixedly positioning the airfoil relative to the workholder. Removing the studs provides heatless release of the airfoil from the workholder.
摘要翻译： 工作台（6）具有与机翼（1）的轮廓表面（4）基本相匹配的轮廓结合表面（7）。 多个螺栓（8）设置在位于工件接合表面周围的多个螺纹孔（9）内。 在操作中，螺栓从表面向外延伸，并且螺栓和粘合表面都与脱模剂（10）接触。 将粘合表面和螺栓以及位于接合表面旁边的翼型件施加固化树脂材料（11），将树脂材料夹在其间。 固化后，在树脂层（11）中形成多个螺纹孔（13），其中延伸的螺柱相对于夹持器固定地定位翼型件。 卸下螺柱提供了翼型件从加工支架的无热释放。
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