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    • 51. 发明授权
    • Sealed joint for a rocket employing fused inorganic vitreous material
    • 用于使用熔融无机玻璃质材料的火箭的密封接头
    • US4913472A
    • 1990-04-03
    • US898917
    • 1986-08-21
    • Bhogaraju V. Janakirama-Rao
    • Bhogaraju V. Janakirama-Rao
    • F02K9/34F16J15/06F16J15/14F16L23/16
    • F16J15/064F02K9/34F02K9/343F16J15/14F16L23/16Y10S277/931Y10S285/911
    • A design for sealing metal-to-metal, of sections of rocket shell with fusible vitreous inorganic "glass-ceramic" compositions, which will not burn-out from high temperatures of rocket-exhaust, is disclosed. The design is intended to set up a thermal-gradient across the cross section of the sealed metal flanges. The thermal-gradient utilizes the useful property of the vitreous state of the seal, viz., the continuous viscosity change from the relatively low viscosity of molten glass at high temperature, to a very high viscosity of almost solid state at lower temperatures. This mechanism achieves a leak-proof "glass-ceramic" or glass seal between the metal flange joints of sections of rocket-shell. The vitreous seal is capable of withstanding a wide range of temperature inside the rocket, of -50.degree. C., to over 1000.degree. C., without failure when the rocket is fired. A metal-to-metal joint provided with leak-proof fused inorganic vitreous seal material capable of withstanding high and low temperatures, and the method of making the same are disclosed.
    • 公开了一种用于将金属与金属密封的设计,其不含火焰排气高温的不熔化的可熔玻璃质无机“玻璃 - 陶瓷”组合物的火箭壳部分。 该设计用于在密封金属法兰的横截面上设置热梯度。 热梯度利用了密封玻璃状态的有用性质,即从较高温度下熔融玻璃相对较低粘度的连续粘度变化到较低温度下几乎固态的非常高的粘度。 这种机制在火箭壳部分的金属法兰接头之间实现了防漏“玻璃陶瓷”或玻璃密封。 玻璃密封件能够承受火箭内的温度范围为-50℃至超过1000℃,而火箭发射时不发生故障。 公开了一种金属对金属接头,其具有能够承受高低温的防漏熔融无机玻璃密封材料及其制造方法。
    • 54. 发明授权
    • Sealant spray applicator system and method employing same
    • 密封剂喷涂系统及其使用方法
    • US4786060A
    • 1988-11-22
    • US97135
    • 1987-09-16
    • Keith B. Davis
    • Keith B. Davis
    • B05B12/02B05C11/06B05D1/02B05D3/04B05D7/22B21J15/10F16B33/00F16J15/14E21B33/00B05C9/02B23P25/00
    • F16J15/14B05B12/02B05C11/06B05D3/042B05D7/22B21J15/10B05D1/02F16B33/004Y10T29/49885
    • Method and system for applying liquid sealant in holes of a structural member prior to installing fasteners in such holes, which comprises mixing air with a liquid sealant, spraying a controlled amount of the resulting air-sealant mixture into the holes and depositing liquid sealant therein, and impinging an elevated pressure air stream on the deposited liquid sealant to spread the sealant out and produce a thin layer of sealant in the holes. A system for carrying out the method comprises a spray gun having separate air and liquid sealant paths which meet at the spray nozzle of the spray gun to achieve the mixing of air with the liquid sealant. The liquid spray system also includes a sealant applicator controller which is arranged to activate a series of timers and valves to provide controlled flow of high pressure air and liquid sealant to the nozzle for mixture therein, and spraying to form the sealant deposit, and to provide for continued high pressure flow of air on the layer of sealant deposit to spread the sealant and produce a thin sealant layer.
    • 在将紧固件安装在这样的孔中之前,将结构构件的孔中的液体密封剂施加到包括混合空气与液体密封剂的方法和系统中,将受控量的所得空气密封剂混合物喷洒到孔中并在其中沉积液体密封剂, 并在沉积的液体密封剂上冲击高压气流以将密封剂散开,并在孔中产生一薄层密封剂。 用于执行该方法的系统包括具有分开的空气和液体密封剂路径的喷枪,其在喷枪的喷嘴处相交,以实现空气与液体密封剂的混合。 液体喷射系统还包括一个密封剂涂抹器控制器,该控制器设置成激活一系列定时器和阀门,以将高压空气和液体密封剂控制流到喷嘴以进行混合,并喷涂以形成密封剂沉积物,并提供 用于在密封剂层上持续的高压空气流动以扩散密封剂并产生薄的密封剂层。
    • 59. 发明授权
    • Hydraulic seal with pressure-actuated ridges
    • 带压力脊的液压密封
    • US4557488A
    • 1985-12-10
    • US701939
    • 1985-02-15
    • James A. F. Litherland
    • James A. F. Litherland
    • E21D15/44F16J15/32F16J15/06F16J15/14
    • F16J15/32E21D15/44F16J15/324
    • An elastomeric seal (1), particularly for mining roof supports, has a circumferentially extending primary sealing ridge (4) for sealing against the cylinder wall (15) at both low and high pressure differentials. In order to provide lubrication of the primary sealing ridge, a series of fluid reservoirs (10) are defined adjacent to opposite sides of the primary sealing ridge by a respective web (5) of secondary sealing ridges, each web consisting of a circumferential ridge (6) and a series of axial ridges (7). The secondary ridges (6, 7) are dimensioned such that at low fluid pressure differentials across the piston there is a radial clearance between the secondary ridges and the cylinder wall, to reduce seal friction at low pressures, but at high pressure differentials the portion of the seal adjacent to the low pressure chamber is elastomerically deformed to bring the web of secondary ridges at that end into sealing engagement with the cylinder walls, to provide a secondary seal and to trap fluid in the reservoirs. The seal may be arranged to be single acting or double-acting.
    • 弹性体密封件(1),特别是用于采矿屋顶支撑件的弹性体密封件(1)具有周向延伸的主密封脊(4),用于在低压差和高压力差下都与气缸壁(15)密封。 为了提供主密封脊的润滑,一系列流体储存器(10)通过相应的第二密封脊的腹板(5)限定在主密封脊的相对侧附近,每个腹板由圆周脊( 6)和一系列轴向脊(7)。 次级脊(6,7)的尺寸使得在活塞的低流体压力差下,在次级脊和气缸壁之间存在径向间隙,以减小在低压下的密封摩擦,但是在高压下将部分 靠近低压室的密封件弹性变形,使得在该端的次级脊的腹板与气缸壁密封接合,以提供次级密封并将液体收集在储液器中。 密封件可以被布置为单作用或双作用。