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公开(公告)号：US5653581A
公开(公告)日：1997-08-05
申请号：US346058
申请日：1994-11-29
CPC分类号： F01D25/246
摘要： The attachment for securing the stator vanes to the outer compressor case includes hooks strategically located with one set in the center of a segment and one set each at either end of each segment. The segments are assembled end to end to form a ring of an array of rows of airfoils for directing air to the compressor blades of a gas turbine engine. Each assembled segment may include three rows of vanes. The axial gap between the structure of the upstream stage of the compressor, the axial and circumferential gap of radially extending pins attached to the "floating" lug-nuts assembled in each pair of hooks and the tight fit of the pins in the center pair of hooks allow for axial and circumferential thermal expansion and the bolted lug-nuts and outer case provide radial restraint, all of which combine to reduce stresses on the airfoil during engine transient conditions.
摘要翻译： 用于将定子叶片固定到外部压缩机壳体的附件包括在一段的中心具有一组的策略性定位的钩，并且每个段在每个段的任一端各设一个。 这些段被端对端地组装成一排翼型阵列的环，用于将空气引导到燃气涡轮发动机的压缩机叶片。 每个装配的片段可以包括三排叶片。 压缩机上游级结构之间的轴向间隙，连接到组装在每对钩中的“浮动”凸耳螺母的径向延伸销的轴向和周向间隙以及销在中心对中的紧密配合 钩子允许轴向和周向热膨胀，并且螺栓连接的螺母和外壳提供径向约束，所有这些结合在发动机瞬态条件下结合以减少翼型上的应力。
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公开(公告)号：US5873699A
公开(公告)日：1999-02-23
申请号：US670302
申请日：1996-06-27
CPC分类号： F01D5/147 , F01D5/282 , F05D2230/24 , F05D2300/173 , F05D2300/603 , Y10T29/49337 , Y10T29/49339
摘要： An airfoil is provided having a cross-sectional geometry which includes a first wall, a second wall disposed opposite the first wall, a leading edge, a trailing edge disposed opposite the leading edge, and a first cavity. The first cavity is disposed between the first and second walls, and the leading and trailing edges. The cross-sectional geometry extends between a first and a second end, and the airfoil is formed from discontinuously reinforced aluminum.
摘要翻译： 提供一种翼型件，其横截面几何形状包括第一壁，与第一壁相对设置的第二壁，前缘，与前缘相对设置的后缘和第一腔。 第一腔设置在第一和第二壁之间以及前缘和后缘之间。 横截面几何形状在第一和第二端之间延伸，翼型由不连续增强的铝形成。
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公开(公告)号：US5927130A
公开(公告)日：1999-07-27
申请号：US961818
申请日：1997-10-31
CPC分类号： F01D5/147 , F01D5/282 , F05D2230/24 , F05D2300/173 , F05D2300/603 , Y10T29/49337 , Y10T29/49339
摘要： A method for manufacturing an airfoil is provided which includes the steps of: a) providing a billet of discontinuously reinforced aluminum having at least 10 volume percent of silicon carbide as a reinforcing element, and no more than 30 volume percent of silicon carbide as the reinforcing element; 2) extruding the billet into an airfoil shaped geometry from a die, wherein the geometry includes a first wall, a second wall disposed opposite the first wall, a leading edge, a trailing edge disposed opposite the leading edge, and a first cavity disposed between the first and second walls, and the leading and trailing edges.
摘要翻译： 提供一种用于制造翼型的方法，其包括以下步骤：a）提供具有至少10体积％的碳化硅作为增强元素的不连续增强的铝坯料，并且不超过30体积％的碳化硅作为增强材料 元件; 2）将坯料从模具中挤出成翼型几何形状，其中几何形状包括第一壁，与第一壁相对设置的第二壁，前缘，与前缘相对设置的后缘，以及设置在 第一和第二壁，以及前缘和后缘。
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