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11. 发明授权

US3839105A Oxalyl dihydrazide compositions and use as a coolant in gas generating process 失效
标题翻译：氧化二异氰酸酯组合物和用作气体生成过程中的冷却剂
公开(公告)号：US3839105A
公开(公告)日：1974-10-01
申请号：US23379072
申请日：1972-03-10
申请人： THIOKOL CHEMICAL CORP
发明人： DEWITT I , PACANOWSKY E
IPC分类号： C06B23/04 , C06B47/08 , C06D5/06
CPC分类号： C06D5/06 , C06B23/04 , C06B47/08
摘要： A curable homogeneous gas-generating composition composed essentially of oxalyl dihydrazide coolant combined with: (a) a perchlorate oxidizer selected from the group consisting of ammonium perchlorate, the alkali metal perchlorates, and the alkali earth metal perchlorates, (b) a combustible fuel binder, and (c) propellant adjuvants. A process for the preparation of oxalyl dihydrazide is also disclosed. The gas-generating compositions of the present invention have greatly improved combustion characteristics and exhibit reduced flame temperatures.
摘要翻译：基本上由草酰二肼冷却剂组合的可固化的均匀气体发生组合物与（a）选自高氯酸铵，碱金属高氯酸盐和碱土金属高氯酸盐的高氯酸盐氧化剂组合，（b）可燃燃料粘合剂，和（c）推进剂佐剂。

12. 发明授权

US3837774A Apparatus for molding rigid product from synthetic resinous material 失效
标题翻译：用于从合成树脂材料中模制刚性产品的装置
公开(公告)号：US3837774A
公开(公告)日：1974-09-24
申请号：US31108872
申请日：1972-12-01
申请人： THIOKOL CORP
发明人： ROSS L , WILKINSON J , CRAIG F , HUDSON A
IPC分类号： B29C44/30 , B29C3/06
CPC分类号： B29C44/30
摘要： A machine operable to produce molded synthetic products in finished form in a continuous process, including mixing, pouring, molding, and curing the resultant product.
摘要翻译：一种可操作以在连续方法中生产成品的模制合成产品的机器，包括混合，浇注，模制和固化所得产品。

13. 发明授权

US3826087A Gas rocket system 失效
标题翻译：气体系统
公开(公告)号：US3826087A
公开(公告)日：1974-07-30
申请号：US19770871
申请日：1971-11-11
申请人： THIOKOL CHEMICAL CORP
发明人： MC DONALD A
IPC分类号： F02K9/08 , F02K9/42 , F02K9/44 , F02K
CPC分类号： F02K9/44 , F02K9/08 , F02K9/42
摘要： In the invention, a fuel gas generator has an orificed pressure vessel, an igniter, and a solid propellant that produces fuelrich gas on combustion; an oxidizer gas generator has an orificed pressure vessel, an igniter, and a solid propellant that produces oxidizer-rich gas on combustion; a reaction motor is connected to each gas generator by duct means, with valves in the ducts to meter and proportion the gases as desired into the reaction motor where they are burned for thrust. Gases from the gas generator are relatively cool and can be ducted through conventional valves and other devices to reaction motors for attitude and roll control, as well as for thrust of the vehicle.
摘要翻译：在本发明中，燃气发生器具有在燃烧时产生富燃气体的有孔压力容器，点火器和固体推进剂; 氧化剂气体发生器具有在燃烧时产生富氧化剂气体的有孔压力容器，点火器和固体推进剂; 反应电动机通过管道装置连接到每个气体发生器，管道中的阀门根据需要计量和比例气体到反应电动机中，在那里它们被推动用于推动。来自气体发生器的气体相当冷却，并且可以通过常规阀和其它装置传导到用于姿态和侧倾控制的反作用马达以及用于车辆的推力。

14. 发明授权

US3799798A Method of bonding a polysulfide sealant to a masonry surface 失效
标题翻译：将聚碳酸酯密封剂与MASONRY表面结合的方法
公开(公告)号：US3799798A
公开(公告)日：1974-03-26
申请号：US24771772
申请日：1972-04-26
申请人： THIOKOL CHEMICAL CORP
发明人： ELMER R , PETERSON E
IPC分类号： B05D7/00 , C04B41/48 , C08L15/02 , C08L81/00 , C09J181/04 , B32B13/12 , B44D1/14
CPC分类号： C09J181/04 , C04B41/4838 , C08L15/02 , C08L33/10 , C08L81/00 , C04B41/483 , C08L2666/04
摘要： A FLUID PRIMER ADAPTED TO BE APPLIED TO MASONRY SURFACES TO IMPROVE THE ADHESION THERETO OF SEALANT COMPOSITIONS BASED ON THE LIQUID POLYSULFIDE POLYMERS. THE PRIMER COMPRISES AN ORGANIC SOLVENT SOLUTION OF A CHLORINATED RUBBER AND A POLY(LOWER ALKYL METHACRYLATE), PREFERABLY POLY(N-BUTYL METHACRYLATE). THE PRIMER PROVIDES A BOND WHICH EXHIBITS BOTH GOOD ADHESION AND RESISTANCE TO ULTRA-VIOLET LIGHT.

15. 发明授权

US3797394A Chaff dispenser, method of dispersing chaff 失效
标题翻译： CHAFF分配器，分配方法
公开(公告)号：US3797394A
公开(公告)日：1974-03-19
申请号：US3797394D
申请日：1972-09-11
申请人： THIOKOL CHEMICAL CORP
发明人： THURSTON J , ADAMS G
IPC分类号： F42B10/56 , F42B12/70 , C06D1/04 , H01Q15/00
CPC分类号： F42B10/56 , F42B12/70
摘要： A chaff dispenser for signals and other uses, which ejects from a moving craft and disperses the signal material after a pre-set delay time, comprises an outer case, a canister holding the chaff and explosive charge, a timer, and a parachute. Upon ejection, the timer measures the delay time, releases itself and the parachute which pulls the canister from the outer case. The canister explodes to disperse the chaff. The invention herein described was made in the course of or under contract with the U.S. Air Force (Contract F33657-72-C-0136).
摘要翻译：用于信号和其他用途的谷壳分配器，其从移动的工艺喷射并在预设的延迟时间之后分散信号材料，包括外壳，容纳谷壳和炸药的罐，定时器和降落伞。在弹出时，定时器测量延迟时间，释放自身和从外壳拉出罐的降落伞。罐子爆炸分散谷壳。本文所述的发明是在与美国空军（合同F33657-72-C-0136）的合同或合同下进行的。

16. 发明授权

US3765177A Rocket motor with blast tube and case bonded propellant 失效
标题翻译：具有BLAST管和壳结合螺旋桨的电动马达
公开(公告)号：US3765177A
公开(公告)日：1973-10-16
申请号：US3765177D
申请日：1959-12-30
申请人： THIOKOL CHEMICAL CORP
发明人： RITCHEY H , MC DERMOTT J
IPC分类号： F02K9/22 , F02K9/34 , F02K9/36 , F02K9/04
CPC分类号： F02K9/346 , F02K9/22 , F02K9/36
摘要： 2. A multiple end-burning rocket comprising a motor casing closed at its forward end and having rearward nozzle means, at least one propellant charge therein case-bonded to said motor casing and having a plurality of end-burning surfaces, and a hollow blast tube extending through said propellant charge and to which said charge is bonded, said tube being expansible and contractible in response to changes in the dimensions of said propellant charge, and said blast tube comprising a cured mixture of a liquid bisphenol epoxide polymer and a liquid polythiopolymercaptan polymer.
摘要翻译： 2.一种多端燃烧火箭，包括在其前端处封闭并具有后喷嘴装置的电动机壳体，其中壳体连接到所述电动机壳体并具有多个端部燃烧表面的至少一个推进剂装料和具有多个端部燃烧表面的空心鼓风管延伸通过所述推进剂装料并且所述装料结合到其上，所述管可响应于所述推进剂装料的尺寸的变化而可膨胀和收缩，并且所述鼓管包含液态双酚环氧化物聚合物和液体聚硫羟基硫醇的固化混合物聚合物。

17. 发明授权

US3760730A Rocket vehicle 失效
标题翻译： ROCKET车辆
公开(公告)号：US3760730A
公开(公告)日：1973-09-25
申请号：US3760730D
申请日：1972-03-06
申请人： THIOKOL CHEMICAL CORP
发明人： OSBORNE D , PETERSON S
IPC分类号： F02K9/30 , F42B15/36 , F42B15/10
CPC分类号： F02K9/30 , F42B15/36
摘要： A rocket motor has a plurality of peripheral, canted, thrust nozzles and an aftwardly extending coupling member. A thermally operated time delay device in communication with the interior of the rocket motor, and operatively connected to a latch means that locks the rocket to a cargo carrying case, is capable of releasing the latch means and separating the rocket from the cargo at a predetermined instant in time.
摘要翻译：火箭发动机具有多个周边的倾斜的推力喷嘴和一个后伸的联接构件。与火箭发动机内部连通并且可操作地连接到锁定装置的热操作延时装置，其将火箭锁定到货物运载箱上，能够释放闩锁装置并以预定的方式将火箭与货物分离及时即时

18. 发明授权

US3760589A Throttling mechanism for controlling the thrust level of a solid propellant rocket motor 失效
标题翻译：用于控制固体推进式电动机的电平的转向机构
公开(公告)号：US3760589A
公开(公告)日：1973-09-25
申请号：US3760589D
申请日：1969-03-24
申请人： THIOKOL CHEMICAL CORP
发明人： OVERALL R , DE HAYE J , PUCKETT W , KELLY J
IPC分类号： F02K9/86 , F02K9/04
CPC分类号： F02K9/86
摘要： A throttling mechanism for the nozzle of a solid propellant rocket motor that is capable of selectively controlling the effective area of the discharge orifices of the nozzle whereby the magnitude of the thrust of the solid propellant rocket motor may be varied.
摘要翻译：用于固体推进剂火箭发动机喷嘴的节流机构，其能够选择性地控制喷嘴的排出孔的有效面积，从而可以改变固体推进剂火箭发动机的推力的大小。

19. 发明授权

US3759039A Thrust control and modulation system 失效
标题翻译：控制和调节系统
公开(公告)号：US3759039A
公开(公告)日：1973-09-18
申请号：US3759039D
申请日：1968-11-22
申请人： THIOKOL CHEMICAL CORP
发明人： WILLIAMS A
IPC分类号： F02K9/82 , F02K1/14
CPC分类号： F02K9/82
摘要： A device, more particularly a thrust control system, is disclosed wherein gases bled from the rocket motor combustion chamber are thereafter conduited to a canister having a perforated solid propellant grain therein, which is combusted by the gases bled from the main chamber and thereafter conducted to discharges arranged with respect to the rocket motor to provide thrust vector control, roll and/or pitch control and thrust modulation. Associated valve control means is also provided.
摘要翻译：公开了一种装置，更具体地说是一种推力控制系统，其中从火箭发动机燃烧室排出的气体此后被导入到其中具有穿孔的固体推进剂颗粒的罐中，该罐由主室排出的气体燃烧，然后传导至相对于火箭发动机布置的排放物以提供推力矢量控制，滚动和/或俯仰控制和推力调制。还提供了相关的阀控制装置。

20. 发明授权

US3756025A Handling means for slot formers 失效
标题翻译：处理方法
公开(公告)号：US3756025A
公开(公告)日：1973-09-04
申请号：US3756025D
申请日：1971-07-14
申请人： THIOKOL CHEMICAL CORP
发明人： MC CULLOUGH E
IPC分类号： F02K9/10 , F02C3/26
CPC分类号： F02K9/10
摘要： In slot formers for solid propellant rocket grains, of the type wherein a disk of propellant is equipped with ribs on one side to provide a radially extending slot between forward and aft components of a solid propellant rocket grain, a rigid reinforcing frame embedded in the propellant disk is provided with loops that extend beyond the surface of the disk to serve as handling means therefore.
摘要翻译：在用于固体推进剂火箭颗粒的槽形成器中，其中推进剂盘在一侧上装有肋，以在固体推进剂火箭颗粒的前部和后部部件之间提供径向延伸的狭槽，嵌入推进剂中的刚性加强框架盘具有延伸超过盘的表面的循环，从而用作处理装置。

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