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公开(公告)号：US4308309A
公开(公告)日：1981-12-29
申请号：US147700
申请日：1980-05-07
申请人： Robert A. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Frosch , Daniel B. Leiser , David A. Stewart , Marnell Smith , Carlos A. Estrella , Howard E. Goldstein
发明人： Robert A. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Frosch , Daniel B. Leiser , David A. Stewart , Marnell Smith , Carlos A. Estrella , Howard E. Goldstein
CPC分类号： B64G1/58 , F42B15/34 , B64G1/503 , Y10T428/166 , Y10T428/24777 , Y10T428/24785 , Y10T428/31663 , Y10T442/2631 , Y10T442/2975
摘要： A flexible, adjustable refractory filler (1) is disclosed for filling gaps between ceramic tiles (10, 11) forming the heat shield of a space shuttle vehicle, to protect its aluminum skin (20) during atmospheric re-entry. The easily installed and replaced filler (1) consists essentially of a strip of ceramic cloth (3) coated, at least along both its longitudinal edges (4, 5), with a room temperature vulcanizable silicone rubber compound with a high emittance colored pigment. The filler may have one or more layers (2, 3), as the gap width requires. Preferred materials are basket-weave aluminoborosilicate cloth, and a rubber compounded with silicon tetraboride as the emittance agent and finely divided borosilicate glass containing about 7.5% B.sub.2 O.sub.3 as high temperature binder. The filler cloth strip or tape is cut to proper width and length, inserted into the gap, and fastened with previously applied drops of silicone rubber adhesive.
摘要翻译： 公开了一种柔性可调节的耐火填料（1），用于填充形成航天飞行器的隔热罩的瓷砖（10,11）之间的间隙，以在大气重入期间保护其铝皮（20）。 容易安装和更换的填料（1）基本上由至少沿着其纵向边缘（4,5）涂覆的一块陶瓷布（3）组成，其中室温可硫化的硅橡胶化合物具有高发射率的着色颜料。 填料可以具有一个或多个层（2,3），如间隙宽度所要求的。 优选的材料是筐式编织的铝硼硅酸布，以及四硼化硅作为发射剂的橡胶和含有约7.5％B 2 O 3作为高温粘合剂的细碎的硼硅酸盐玻璃。 将填料布条或带切割成适当的宽度和长度，插入间隙中，并用预先施加的硅橡胶胶粘剂固定。
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公开(公告)号：US4148962A
公开(公告)日：1979-04-10
申请号：US940688
申请日：1978-09-08
申请人： Robert A. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Frosch , Daniel B. Leiser , Howard E. Goldstein , Marnell Smith
发明人： Robert A. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Frosch , Daniel B. Leiser , Howard E. Goldstein , Marnell Smith
CPC分类号： C04B30/02 , Y10T428/2916
摘要： A refractory composite insulating material prepared from silica fibers and aluminosilicate fibers in a weight ratio ranging from 1:19 to 19:1, and about 0.5 to 30% boron oxide, based on the total fiber weight. The aluminosilicate fiber and boron oxide requirements may be satisfied by using aluminoborosilicate fibers and, in such instances, additional free boron oxide may be incorporated in the mix up to the 30% limit. Small quanitites of refractory opacifiers, such as silicon carbide, may be also added. The composites just described are characterized by the absence of a nonfibrous matrix.
摘要翻译： 基于总纤维重量，由二氧化硅纤维和铝硅酸盐纤维以1:19至19:1的重量比和约0.5至30％的氧化硼制备的耐火复合绝缘材料。 硅铝酸盐纤维和氧化硼的要求可以通过使用铝硼硅酸盐纤维来满足，并且在这种情况下，额外的游离氧化硼可以掺入混合物中至30％的限度。 还可以加入耐火玻璃的小量例如碳化硅。 刚刚描述的复合材料的特征在于不存在非纤维矩阵。
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公开(公告)号：US5079082A
公开(公告)日：1992-01-07
申请号：US298149
申请日：1989-01-18
IPC分类号： C04B41/50
CPC分类号： C04B41/009 , C04B41/5022 , Y10S428/92 , Y10T428/249957 , Y10T428/252
摘要： A porous body of fibrous, low density silica-based insulation material is at least in part impregnated with a reactive boron oxide containing borosilicate glass frit, a silicon tetraboride fluxing agent and a molybdenum silicide emittance agent. The glass frit, fluxing agent and emittance agent are separately milled to reduce their particle size, then mixed together to produce a slurry in ethanol. The slurry is then applied to the insulation material and sintered to produce the porous body.
摘要翻译： 纤维状低密度二氧化硅基绝缘材料的多孔体至少部分地浸渍有含有硼硅酸盐玻璃料的反应性氧化硼，四硼化硅助熔剂和硅化钼发射剂。 将玻璃料，助熔剂和发射剂分别研磨以减小其粒度，然后混合在一起以在乙醇中产生浆料。 然后将浆料施加到绝缘材料上并烧结以产生多孔体。
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公开(公告)号：US3952083A
公开(公告)日：1976-04-20
申请号：US427775
申请日：1973-12-26
申请人： James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher , Howard E. Goldstein , Marnell Smith , Daniel Leiser
发明人： James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher , Howard E. Goldstein , Marnell Smith , Daniel Leiser
CPC分类号： C04B35/14
摘要： A reusable silica surface insulation (RSI) material is provided by bonding amorphous silica fibers with colloidal silica at an elevated temperature. The surface insulation is ordinarily manufactured in the form of blocks (i.e., tiles).
摘要翻译： 通过在高温下将无定形二氧化硅纤维与胶体二氧化硅结合来提供可重复使用的二氧化硅表面绝缘（RSI）材料。 表面绝缘通常以块（即瓦片）的形式制造。
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公开(公告)号：US4713275A
公开(公告)日：1987-12-15
申请号：US862925
申请日：1986-05-14
CPC分类号： F27D5/00 , B64G1/50 , B64G1/58 , F27D1/06 , Y10S428/92 , Y10T428/16 , Y10T428/166 , Y10T428/237 , Y10T428/239
摘要： The present invention discloses a ceramic reusable externally applied thermal protection system (TPS). The system functions by using the composite device created by combining an upper shell, thermal insulation and lower tile components shown in FIG. 2. The upper shell effectively separates its primary functions as a toughened outer-surface and load carrier. In a preferred embodiment, a structurally strong ceramic/ceramic upper shell is manufactured from ceramic cloth upon which additional ceramic material has been deposited and maintains the configuration of the upper shell. The lower tile is composed of lightweight ceramic normally acceptable in this application. One or more lightweight rigid or flexible insulation materials are used in the cavity created by combining the upper shell and lower tile. The assembly of the overall tile is facilitated by attachment means effective to withstand the temperature and stress conditions. These attachment means include a self-locking wedge and complementary surface, ceramic pins, augers and the like. The device is useful on the interior surface of a kiln or the like and is also attached to the exterior surface of an aerospace vehicle for thermal protection.
摘要翻译： 本发明公开了一种陶瓷可重复使用的外置热保护系统（TPS）。 该系统通过使用通过组合图2所示的上壳体，隔热层和下瓦片部件而形成的复合装置来起作用。 上壳体有效地将其作为增韧的外表面和负载载体的主要功能分离。 在优选实施例中，结构强的陶瓷/陶瓷上壳由陶瓷布制成，其上已经沉积了另外的陶瓷材料并保持了上壳的构型。 该瓦片由本应用中通常可接受的轻质陶瓷组成。 在通过组合上壳体和下瓦片而产生的空腔中使用一种或多种轻质刚性或柔性绝缘材料。 通过有效承受温度和压力条件的附接装置便于整体瓦片的组装。 这些附接装置包括自锁楔和互补表面，陶瓷销，螺旋推运器等。 该装置在窑等的内表面上是有用的，并且还附接到航空航天车辆的外表面用于热保护。
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公开(公告)号：US4312292A
公开(公告)日：1982-01-26
申请号：US945040
申请日：1978-09-22
CPC分类号： B05B13/0228
摘要： A spray coating apparatus is provided for rotating a workpiece relative to a spray station to obtain a uniform coating of the workpiece. In a typical example, the workpiece comprises a ceramic tile which is to be coated with a ceramic coating and the tile is to be used as a reusable component of the thermal protection system for a space shuttle. The apparatus for rotating the workpiece includes a base support having a first rotatable stage for rotation in the horizontal plane and a second rotatable stage for rotation in a second plane inclined at an angle, such as 45 degrees, to the horizontal plane and the workpiece is supported on this second stage. Thus the workpiece is rotatable in both of two planes of rotation. The workpiece support is detachable from the first rotatable stage and the workpiece is readily detachable from the workpiece support to facilitate off loading of the spray coated workpiece. The workpiece holder includes a spray guard extending around the periphery of the workpiece to shield that surface of the workpiece where no coating is desired. The two degrees of freedom provided in the rotation of the workpiece relative to the spray station permits the various facets of the tile to be sequentially rotated into an orthogonal relationship to the spray station for uniform coating of the workpiece.
摘要翻译： 提供喷涂装置用于相对于喷雾站旋转工件以获得工件的均匀涂层。 在典型的例子中，工件包括陶瓷砖，该瓷砖将被涂覆有陶瓷涂层，该瓦片将被用作航天飞机热保护系统的可再利用部件。 用于旋转工件的装置包括：基座支架，其具有用于在水平面中旋转的第一可旋转台和用于在与水平面成45度角倾斜的第二平面中旋转的第二可旋转台，并且工件是 在第二阶段支持。 因此，工件能够在两个旋转平面中旋转。 工件支撑件可从第一可旋转台拆卸，并且工件容易地从工件支撑件拆卸，以便于喷涂工件的卸载。 工件保持器包括围绕工件的周边延伸的防护罩，以防止不需要涂层的工件的表面。 在工件相对于喷射台的旋转中提供的两个自由度允许瓦片的各个面顺序地旋转成与喷涂站正交的关系，以均匀地涂覆工件。
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