Consolidation of composite material
    2.
    发明授权
    Consolidation of composite material 有权
    复合材料的固结

    公开(公告)号:US08343402B1

    公开(公告)日:2013-01-01

    申请号:US12625354

    申请日:2009-11-24

    IPC分类号: B22F3/04

    摘要: In one embodiment method to form a composite part from a metallic composite powder, comprises positioning a metallic composite powder preform in a mold cavity formed by a first susceptor and a second susceptor, heating the mold cavity to a first processing temperature, applying a pressure to the mold cavity, and applying a thermal oscillation cycle to the mold cavity, wherein the thermal oscillation cycle oscillates the temperature of the mold cavity between a first temperature in which the metallic composite powder is in a first phase and a second temperature in which the metallic composite powder is in a second phase, different from the first phase.

    摘要翻译: 在一种实施方式中,从金属复合粉末形成复合部件,包括将金属复合粉末预制件定位在由第一基座和第二基座形成的模腔中,将模腔加热至第一加工温度,施加压力 模腔,并且向模腔施加热振荡循环,其中所述热振荡循环使所述模腔的温度在所述金属复合粉末处于第一相的第一温度和所述金属复合粉末处于第一温度的第二温度之间振荡,其中所述金属 复合粉末处于与第一相不同的第二相。

    Silica-enriched protective coating
    6.
    发明授权
    Silica-enriched protective coating 失效
    二氧化硅保护涂层

    公开(公告)号:US5405706A

    公开(公告)日:1995-04-11

    申请号:US146586

    申请日:1993-12-03

    摘要: Coatings which protect the skin of hypersonic flight vehicles are disclosed. Silicide coatings, such as R512E, is used to minimize catalytic recombination of dissociated species, such as atomic oxygen and atomic nitrogen, thus, decreasing thermal and oxidative degradation. Prehydrated, polymerized sol of tetraethylorthosilicate is applied to a coating, and is fired, to produce an integral protective coating.

    摘要翻译: 公开了保护超音速飞行器皮肤的涂层。 诸如R512E的硅化物涂层用于使解离的物质如原子氧和原子氮的催化重组最小化,从而降低热和氧化降解。 将原硅酸四乙酯的预水合聚合溶胶施加到涂层上,并被烧制,以产生整体保护涂层。

    Oxidation protected susceptor
    8.
    发明授权
    Oxidation protected susceptor 失效
    氧化保护感受器

    公开(公告)号:US06653608B1

    公开(公告)日:2003-11-25

    申请号:US10032625

    申请日:2001-10-24

    IPC分类号: H05B606

    CPC分类号: H05B6/105

    摘要: A single or multilayer smart susceptor for temperature control of part fabrication in an induction processing system generally consists of single layer or laminated layers of ferromagnetic material susceptible to heating by induction. The use of the susceptors in fabrication at elevated temperatures causes oxidation damage to the surface. The susceptor may be coated with a nickel aluminide surface coating to minimize oxidation of the susceptor outer surface.

    摘要翻译: 用于感应加工系统中部件制造的温度控制的单层或多层智能基座通常由容易受感应加热的铁磁材料的单层或层压层组成。 在高温制造中使用感受体会对表面造成氧化损伤。 基座可以涂覆有镍铝表面涂层,以使基座外表面的氧化最小化。

    SELF EXPANDING FASTENER
    9.
    发明申请
    SELF EXPANDING FASTENER 有权
    自扩张紧固件

    公开(公告)号:US20110135418A1

    公开(公告)日:2011-06-09

    申请号:US12632604

    申请日:2009-12-07

    IPC分类号: F16B13/04 B23P11/00

    摘要: In one embodiment a method to join a first structure to a second structure, comprises aligning a first hole in the first structure with a second hole in the second structure and inserting a fastener into the first hole and the second hole. The fastener comprises a shape memory alloy which was formed into a first shape having a diameter slightly larger than a diameter of the first hole and the second hole when the shape memory alloy was in an austenite state and reduced to a second shape having a diameter less than the diameter of the first hole and the second hole when the shape memory alloy was in a martensite state. The method further comprises heating the fastener above an austenite start transition temperature, such that the fastener initiates free expansion from the second shape back to the first shape and establishes physical contact with the surface of the first hole and the second hole and continuing to heat the fastener such that first structure and the second structure proximate the holes and the fastener undergo plastic deformation.

    摘要翻译: 在一个实施例中,将第一结构连接到第二结构的方法包括将第一结构中的第一孔与第二结构中的第二孔对准,并将紧固件插入第一孔和第二孔中。 紧固件包括形状记忆合金,其形状为第一形状,其形状记忆合金处于奥氏体状态时,直径略大于第一孔的直径,第二孔缩小至直径较小的第二形状 比形状记忆合金处于马氏体状态时的第一孔和第二孔的直径大。 该方法还包括将紧固件加热到高于奥氏体起始转变温度,使得紧固件开始从第二形状到第一形状的自由膨胀,并且与第一孔和第二孔的表面建立物理接触,并且继续加热 紧固件使得第一结构和靠近孔和紧固件的第二结构经历塑性变形。