SYNTHESIS OF 4,10-DINITRO-2,6,8,12-TETRAOXA-4,10-DIAZATETRACYCLO[5.5.0.05,903,11]DODECANE
    41.
    发明申请
    SYNTHESIS OF 4,10-DINITRO-2,6,8,12-TETRAOXA-4,10-DIAZATETRACYCLO[5.5.0.05,903,11]DODECANE 审中-公开
    合成4,10-十六烷基-2,6,8,12-四氢环-4,10-二氮杂萘并[5.5.0.0 <5,9> 0 <3,11>] DODECANE

    公开(公告)号:WO1995004062A1

    公开(公告)日:1995-02-09

    申请号:PCT/US1994008623

    申请日:1994-08-02

    CPC classification number: C07D498/22 C06B25/34 C06B45/10 C06B45/105

    Abstract: 4,10-dinitro-2,6,8,12-tetraoxa-4,10-diazatetracyclo-[5.5.0.0 0 ]dodecane is synthesized by reacting a diacyl-2,3,5,6-tetraoxypiperazine derivative, a strong acid, and a nitrate source at a temperature above ambient temperature. The reaction product is precipitated by cooling. It may be purified by washing with methanol and/or sodium bicarbonate and by simmering in nitric acid.

    Abstract translation: 4,10-二硝基-2,6,8,12-四氧杂-4,10-二氮杂四环[5.5.0.0 <5,9> 0 <3,1,1>]十二烷通过二酰基-2,3 ,5,6-四氧代哌嗪衍生物,强酸和硝酸根源,温度高于环境温度。 反应产物通过冷却沉淀。 它可以通过用甲醇和/或碳酸氢钠洗涤并通过在硝酸中煨来进行纯化。

    IMPROVED HYDROGENOLYSIS OF 2,4,6,8,10,12-HEXABENZYL-2,4,6,8,10,12-HEXAAZATETRACYCLO [5.5.0.05,9.03,11]DODECANE
    42.
    发明申请
    IMPROVED HYDROGENOLYSIS OF 2,4,6,8,10,12-HEXABENZYL-2,4,6,8,10,12-HEXAAZATETRACYCLO [5.5.0.05,9.03,11]DODECANE 审中-公开
    2,4,6,8,10,12-十六烷基-2,4,6,8,10,12-十六烷基丙酰氯[5.5.0.0 <5,9> .0 3,11]的改性氢化

    公开(公告)号:WO1997020785A1

    公开(公告)日:1997-06-12

    申请号:PCT/US1996019130

    申请日:1996-12-04

    CPC classification number: C07D487/22

    Abstract: A process for the hydrogenolysis of 2,4,6,8,10,12-hexabenzyl-2,4,6,8,10,12-hexaazatetracyclo [5.5.0.0 .0 ]dodecane ("HBIW") is disclosed in which a quantity of HBIW, cosolvent and a bromine source are placed into a reaction vessel. Acetic anhydride and a substantially water-free palladium catalyst are then rapidly added. The reaction vessel is purged of an atmosphere capable of reacting with hydrogen, and hydrogen is quickly introduced to convert the HBIW to tetraacetyl-dibenzylhexaazaisowurtzitane ("TADB"). The acetic anhydride is added immediately prior to hydrogen introduction so that it does not have time to react with the HBIW to form an acetylated derivative prior to commencement of the desired hydrogenation reaction. The process requires very little palladium catalyst, preferably less than 10 % wt./wt. based on the HBIW substrate. The TADB, precipitated on the palladium hydrogenation catalyst, is subjected to a second hydrogenation step using formic acid solvent in the presence of hydrogen to form tetraacetyldiformylhexaazaisowurtzitane ("TADF").

    Abstract translation: 2,4,6,8,10,12-六苄基-2,4,6,8,10,12-六氮杂四环[5.5.0.0 <5,9> .0 3,11]]氢解的方法, 公开了将一定量的HBIW,共溶剂和溴源放入反应容器中的十二烷(“HBIW”)。 然后快速加入乙酸酐和基本上无水的钯催化剂。 将反应容器吹扫出能够与氢反应的气氛,并迅速引入氢气以将HBIW转化为四乙酰基 - 二苄基六氮杂异纤锌矿型结构烷烃(“TADB”)。 在引入氢气之前立即加入乙酸酐,使得在开始所需的氢化反应之前,其没有时间与HBIW反应形成乙酰化的衍生物。 该方法需要非常少的钯催化剂,优选小于10重量% 基于HBIW底物。 在钯氢化催化剂上沉淀的TADB在氢气存在下使用甲酸溶剂进行第二氢化步骤以形成四乙酰基均一六氮杂异纤锌矿型结构烷烃(“TADF”)。

    METHODS OF PREPARING GAS GENERANT FORMULATIONS
    43.
    发明申请
    METHODS OF PREPARING GAS GENERANT FORMULATIONS 审中-公开
    制备气体生成配方的方法

    公开(公告)号:WO1996022954A1

    公开(公告)日:1996-08-01

    申请号:PCT/US1995000083

    申请日:1995-01-26

    CPC classification number: C06B21/0066 C06B21/0091 C06D5/06

    Abstract: Novel methods for processing gas generant compositions to produce feed stock are disclosed. The methods of the present invention include utilizing a binding agent and other additives in a mixture of ingredients of gas generant compositions in sufficient quantities that the ingredients of the gas generating material will agglomerate to form granules as the ingredients are mixed. Processing methods, including roll coating, continuous mixing, static mixing, freeze drying, solvent extraction, emulsification, azeotropic distillation, spray drying, fluidized bed processing and particle grinding are also disclosed for use in preparing feed stock for final gas generant products. The methods of the present invention are particularly useful in processing gas generating materials having a non-azide based fuel.

    Abstract translation: 公开了用于处理气体发生剂组合物以生产原料的新方法。 本发明的方法包括在气体发生剂组合物的成分混合物中充分使用粘合剂和其它添加剂,使得气体发生材料的成分在混合成分时会附聚形成颗粒。 还公开了用于制备最终气体发生剂产品的原料的加工方法,包括辊涂,连续混合,静态混合,冷冻干燥,溶剂萃取,乳化,共沸蒸馏,喷雾干燥,流化床处理和颗粒研磨。 本发明的方法在具有非叠氮化物燃料的气体发生材料的处理中特别有用。

    SLOTTED HYBRID PRESSURE VESSEL
    44.
    发明申请
    SLOTTED HYBRID PRESSURE VESSEL 审中-公开
    缝合混合压力容器

    公开(公告)号:WO1996004474A1

    公开(公告)日:1996-02-15

    申请号:PCT/US1995009251

    申请日:1995-07-21

    CPC classification number: F42B39/20 F02K9/34 F02K9/38

    Abstract: A pressure vessel and process for manufacturing the pressure vessel. In one embodiment, the invention includes a case (10) for a rocket motor which includes a cylindrical, metal shell (12) which has been configured with a plurality of slots (20) positioned in axially extending rows. A fiber reinforced plastic layer (14) is attached to the metal shell. Each slot has a length (L) and is separated by adjacent slots in the same row by an axial distance (A) with adjacent rows of slots separated by a circumferential distance (C) and configured such that L + A >/= 6C and L >/= 4A. The method of the invention comprises using a carbon dioxide laser to cut a keyhole in the shell and then cutting axially outwardly from the keyhole to form the slot, resulting in slots having a width equal to the cutting width of the laser. The beam is then defocused and used to heat a portion of the metal shell surrounding the ends of each slot to produce a tempered zone.

    Abstract translation: 压力容器及制造压力容器的方法。 在一个实施例中,本发明包括一种用于火箭发动机的壳体(10),其包括圆柱形的金属壳体(12),该壳体已被构造成具有定位在轴向延伸的行中的多个狭槽(20)。 纤维增强塑料层(14)附着在金属外壳上。 每个槽具有长度(L),并且由相邻行中的相邻槽分开轴向距离(A),相邻行槽间隔开周向距离(C)并且被配置为使得L + A> = = 6和 L> / = 4A。 本发明的方法包括使用二氧化碳激光器切割壳体中的锁孔,然后从锁眼轴向向外切割以形成狭槽,从而形成具有等于激光切割宽度的宽度的槽。 然后将光束散焦并用于加热围绕每个槽的端部的金属壳的一部分以产生回火区。

    RUGGED QUICK-RESPONSE THERMOCOUPLE FOR USE IN EVALUATING GAS GENERANTS AND GAS GENERATORS
    45.
    发明申请
    RUGGED QUICK-RESPONSE THERMOCOUPLE FOR USE IN EVALUATING GAS GENERANTS AND GAS GENERATORS 审中-公开
    用于评估气体发生器和气体发生器的强制快速热电偶

    公开(公告)号:WO1995018960A1

    公开(公告)日:1995-07-13

    申请号:PCT/US1995000039

    申请日:1995-01-04

    CPC classification number: G01K13/02 G01K7/04 H01L35/32

    Abstract: A rugged quick-response thermocouple (10) for use in measuring the temperature of a gas flow includes two wires (12, 14) formed of different metals and electrically joined at an exposed junction (16). A ceramic sheath (18) substantially surrounds the two wires (12, 14) except near the junction (16). The sheath (18) is surrounded by a stainless steel tube (24). The junction (16) is positioned adjacent an end (28) of the ceramic sheath (18). In one embodiment, the wires (12, 14) are coated with an insulator (32) and the insulator (32) is positioned against the flat end (28) of the sheath (18). The exposed junction (16) resists damage from gas flows and from corrosive compounds in the gas mixture.

    Abstract translation: 用于测量气流温度的坚固的快速响应热电偶(10)包括由不同金属形成并在暴露的结(16)处电连接的两根导线(12,14)。 除了接合点(16)之外,陶瓷护套(18)基本上围绕着两个电线(12,14)。 护套(18)由不锈钢管(24)包围。 接头(16)位于陶瓷护套(18)的端部(28)附近。 在一个实施例中,电线(12,14)涂覆有绝缘体(32),并且绝缘体(32)抵靠护套(18)的平坦端(28)定位。 暴露的接点(16)可以抵抗气体流动和气体混合物中腐蚀性化合物的损坏。

    SYSTEM AND METHOD FOR GAS BAG INFLATION AND DEFLATION
    46.
    发明申请
    SYSTEM AND METHOD FOR GAS BAG INFLATION AND DEFLATION 审中-公开
    气囊渗透和定位的系​​统和方法

    公开(公告)号:WO1995018730A1

    公开(公告)日:1995-07-13

    申请号:PCT/US1995000037

    申请日:1995-01-04

    CPC classification number: B60R21/30

    Abstract: A system for inflating and deflating an air bag (140) within a vehicle without substantially exposing the occupants of the vehicle to toxic compounds, particulates, and other contaminants. The system includes a flow guide (114) having an exterior port (117) in communication with ambient air outside the vehicle, an air bag port (120) connected to the air bag (140), and an internal bore (122) permitting fluid flow between the exterior port (117) and the air bag (140). A nozzle (124) disposed within the flow guide bore (122) is secured to an inflator (126). Gas is expelled from the inflator (126) through the nozzle (124) at a velocity sufficient to entrain ambient air from outside the vehicle. The entrained ambient air mixes with the gas expelled through the nozzle (124), and the mixture inflates the air bag (140). The air bag (140) is deflated by moving the mixture out of the air bag (140) and through the flow guide bore (122) for disposition amidst ambient air outside the vehicle.

    Abstract translation: 一种用于对车辆内的气囊(140)进行充气和放气的系统,而不会使车辆的乘客基本上暴露于有毒化合物,颗粒物和其它污染物。 该系统包括具有与车辆外部的环境空气连通的外部端口(117)的流动引导件(114),连接到气囊(140)的气囊端口(120)和允许流体 在外部端口(117)和气囊(140)之间流动。 设置在流动导向孔(122)内的喷嘴(124)固定到充气机(126)。 气体以足以从车辆外部夹带环境空气的速度通过喷嘴(124)从充气器(126)排出。 夹带的环境空气与通过喷嘴(124)排出的气体混合,并且混合物使气囊(140)膨胀。 通过将混合物从气囊(140)中移出并通过流动导向孔(122)而使气囊(140)放气,以便在车辆外部的环境空气中进行配置。

    PYROTECHNICALLY DRIVEN NOZZLE RESTRICTOR
    47.
    发明申请
    PYROTECHNICALLY DRIVEN NOZZLE RESTRICTOR 审中-公开
    PYROTECHNICALLY驱动喷嘴限制器

    公开(公告)号:WO1995014163A1

    公开(公告)日:1995-05-26

    申请号:PCT/US1994013059

    申请日:1994-11-14

    CPC classification number: F02K9/80 F02K1/08 F42B10/66

    Abstract: A pyrotechnically driven device for restricting the area of the nozzle throat (16) in a solid propellant rocket motor includes a piston support (22) mounted in the rocket motor exit cone (14). Attached to a piston (34) is a restrictor (54) movable from a retracted position outside of the nozzle throat (16) to a restricting position within the nozzle throat (16). The piston (34) and attached restrictor (54) are driven by a pyrotechnic charge (30) which includes an initiator (32) operable independently from the solid propellant of the rocket motor. A locking means (44, 48) locks the restrictor in its restricting position.

    Abstract translation: 用于限制固体推进剂火箭发动机中喷嘴喉部16的区域的烟火驱动装置包括安装在火箭发动机出口锥体(14)中的活塞支架(22)。 连接到活塞(34)的是限制器(54),其可从喷嘴喉部(16)外部的缩回位置移动到喷嘴喉部(16)内的限制位置。 活塞(34)和连接的限制器(54)由烟火装置(30)驱动,烟火装置包括可独立于火箭发动机的固体推进剂操作的起动器(32)。 锁定装置(44,48)将限制器锁定在其限制位置。

    PERCHLORATE REMOVAL PROCESS
    48.
    发明申请
    PERCHLORATE REMOVAL PROCESS 审中-公开
    PERCHLORATE拆卸过程

    公开(公告)号:WO1995011858A1

    公开(公告)日:1995-05-04

    申请号:PCT/US1994010991

    申请日:1994-09-28

    CPC classification number: C06B21/0091 C01B11/18 Y10S149/124

    Abstract: A process for removing perchlorate ions from waste water using KCl is disclosed. In the process, waste perchlorate is concentrated by water evaporation in a stripping tower. Ammonia and volatile organics are removed during the concentrating step. Potassium chloride (KCl) is added to the concentrated perchlorate solution to form potassium perchlorate (KClO4), and the reaction mixture is cooled to effect crystallization of the potassium perchlorate. The crystallization liquor is removed by centrifuge or filter press and may be further treated as part of an overall waste water treatment system.

    Abstract translation: 公开了一种使用KCl从废水中除去高氯酸根离子的方法。 在此过程中,高氯酸废物在汽提塔中通过水蒸发浓缩。 浓缩步骤期间除去氨和挥发性有机物。 将氯化钾(KCl)加入到浓缩的高氯酸盐溶液中以形成高氯酸钾(KClO 4),并将反应混合物冷却以使高氯酸钾结晶。 通过离心机或压滤机除去结晶液,并可进一步处理作为整体废水处理系统的一部分。

    USE OF CARBON FIBRILS TO ENHANCE BURN RATE OF PYROTECHNICS AND GAS GENERANTS
    49.
    发明申请
    USE OF CARBON FIBRILS TO ENHANCE BURN RATE OF PYROTECHNICS AND GAS GENERANTS 审中-公开
    使用碳纤维来提高聚氯乙烯和气体总量的燃烧速率

    公开(公告)号:WO1995011207A1

    公开(公告)日:1995-04-27

    申请号:PCT/US1994007907

    申请日:1994-07-14

    CPC classification number: C06D3/00 C06B23/001 C06B23/007 C06B27/00 C06B33/00

    Abstract: Conductive carbon fibrils are incorporated into energetic compositions to enhance the burn rate. The carbon fibrils are grown catalytically from carbon precursors and are substantially free of pyrolytically deposited thermal carbon. The fibrils generally have a length in the range from about 1 mu to about 10 mu and a diameter in the range from about 3.5 nanometers to about 75 nanometers. Length to diameter aspect ratios are greater than 5, and typically in the range from about 100:1 to about 1000:1. A 100 % improvement in burn rate was observed in compositions containing as little as 0.1 weight percent carbon fibrils. Greater amounts of carbon fibrils (2 weight percent) have increased the burn rate 500 %. In most cases, fibril concentration will be in the range from about 0.1 to about 2 weight percent, although greater amounts are possible. The burn rate may be effectively tailored by varying the amount of fibrils added to the composition.

    Abstract translation: 将导电碳纤维引入能量组合物中以增加燃烧速率。 碳原纤维从碳前体催化生长并且基本上不含热解沉积的热碳。 原纤维通常具有在约1微米至约10微米范围内的直径和约3.5纳米至约75纳米范围内的直径。 长径比直径比大于5,通常在约100:1至约1000:1的范围内。 在含有少至0.1重量%碳原纤维的组合物中观察到燃烧速率提高100%。 较大量的碳原纤维(2重量%)使燃烧率提高了500%。 在大多数情况下,原纤维浓度将在约0.1至约2重量百分比的范围内,尽管更大的量是可能的。 可以通过改变添加到组合物中的原纤维的量来有效地调节燃烧速率。

    FINLESS AERODYNAMIC CONTROL SYSTEM
    50.
    发明申请
    FINLESS AERODYNAMIC CONTROL SYSTEM 审中-公开
    完美的航空控制系统

    公开(公告)号:WO1995010748A1

    公开(公告)日:1995-04-20

    申请号:PCT/US1994009610

    申请日:1994-08-26

    CPC classification number: F02K9/90 B64C19/00 F02K1/008 F42B10/14

    Abstract: A control system (10) for use in missiles and other projectiles which provides pitch, yaw and roll control. The control system (10) includes two opposing pairs (14 and 16, 18 and 20) of flaps configured in the aft end of the missile case. Each flap is attached for rotation about its leading edge (24). Prior to actuation, the flaps conform to the exterior surface of the missile. Upon actuation, the flaps extend into the airstream to induce aerodynamic forces. The axis of rotation of each flap is positioned at an oblique angle to the radial plane of the missile.

    Abstract translation: 用于导弹和其他射弹的控制系统(10),其提供俯仰,偏航和滚动控制。 控制系统(10)包括配置在导弹箱的后端的两个折翼对(14和16,18和20)。 每个翼片被附接以绕其前缘(24)旋转。 在致动之前,翼片符合导弹的外表面。 在致动时,翼片延伸到气流中以引起空气动力。 每个翼片的旋转轴线定位成与导弹的径向平面成倾斜的角度。

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