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1. 发明授权

US4600453A Nitrate ester monopropellant 失效
标题翻译：硝酸酯单体推进剂
公开(公告)号：US4600453A
公开(公告)日：1986-07-15
申请号：US789816
申请日：1985-10-21
申请人： Barry D. Allan , Porter H. Mitchell
发明人： Barry D. Allan , Porter H. Mitchell
IPC分类号： C06B47/08
CPC分类号： C06B47/08
摘要： The incorporation of a nitrated pentaerythritol additive selected from theono-, di-, tri-, and tetra-nitrated pentaerythritols into hydrazine is effective in lowering the freezing point of the combination while enhancing the performance of the monopropellant by contributing to the total energy of the monopropellant combination. Hydrazine content varies from about 65 to 95 weight percent while the additive of a nitrated pentaerythritol varies from about 5 to about 25 weight percent. An optional additional additive of methyl alcohol from about 5 to about 20 weight percent can be employed with a corresponding adjustment in weight percent of hydrazine when said additive of methyl alcohol is employed in addition to said additive of said nitrated pentaerythritol.
摘要翻译：将选自单 - ，二 - ，三 - 和四 - 氮化的季戊四醇的硝化季戊四醇添加剂并入肼中有效降低组合的凝固点，同时通过促进单组分推进剂的总能量单组分推进剂组合。肼的含量在约65至95重量％的范围内变化，而硝化季戊四醇的添加剂的变化范围约为5至25重量％。除了所述硝酸季戊四醇的所述添加剂之外，当使用所述甲醇添加剂时，可以使用约5至约20重量％的任选的另外的甲醇添加剂，相应地调节肼的重量百分数。

2. 发明授权

US5194112A Method of applying a fiber optic adhesive to a fiber optic material 失效
标题翻译：将光纤粘合剂应用于光纤材料的方法
公开(公告)号：US5194112A
公开(公告)日：1993-03-16
申请号：US915566
申请日：1992-07-20
申请人： Barry D. Allan
发明人： Barry D. Allan
IPC分类号： B65H55/00 , B65H71/00 , C03C25/10 , C08G18/69 , C09J175/14
CPC分类号： C03C25/1065 , B65H55/00 , B65H71/00 , C03C25/104 , C08G18/69 , C09J175/14
摘要： Disclosed is a method and a fiber optic adhesive which composition is appd to a fiber optic having a buffer coat thereon and is, subsequently, partially cured to a tacky outer surface while being wound onto a bobbin from which the adhesively coated fiber optic material is to payout during use. The adhesively coated fiber optic material must be cured to a tacky cure while being wound onto a bobbin. The cured adhesive composition functions to hold the fiber optic material in place on the bobbin during storage and allows consistent payout during use of the fiber optic material. The typical composition of the fiber optic adhesive comprises hydroxyterminated polybutadiene from about 88.14 to about 92.48 percent by weight, isophorone diisocyanate from about 6.23 to about 6.42 percent by weight, a catalyst of ferric acetylacetonate of dibutyltin dilaurate in an amount from about 0.89 to about 1.15 percent by weight respectively, and a thixotropic agent in an amount of about 4.48 by weight.
摘要翻译：公开了一种方法和光纤粘合剂，其组合物被施加到其上具有缓冲涂层的光纤上，并随后部分地固化到粘性外表面，同时被缠绕到被粘合涂覆的光纤材料所在的线轴上在使用期间支付。粘合涂覆的光纤材料必须固化成粘合固化，同时缠绕在线轴上。固化的粘合剂组合物用于在存储期间将光纤材料保持在线轴上的适当位置，并且允许在使用光纤材料期间一致地支付。纤维光学粘合剂的典型组成包括约88.14-约92.48重量％的羟基封端的聚丁二烯，约6.23至约6.42重量％的异佛尔酮二异氰酸酯，二月桂酸二丁基锡的乙酰丙酮铁的催化剂，其量为约0.89至约1.15 ，触变剂的量为约4.48重量％。

3. 发明授权

US3989560A Method of preparing gelled monomethylhydrazine 失效
标题翻译：凝胶化单甲肼的制备方法
公开(公告)号：US3989560A
公开(公告)日：1976-11-02
申请号：US518492
申请日：1966-01-03
申请人： Barry D. Allan
发明人： Barry D. Allan
IPC分类号： B01J19/06 , C06B47/08
CPC分类号： B01J19/06 , C06B47/08
摘要： Liquid monomethylhydrazine is converted to a thiotropic gel by dispersing erein a cellulose or hydroxyalkyl-substituted gelling agent. The gel thus obtained can be handled and stored on board a rocket motor without the hazards associated with liquid monomethylhydrazine.
摘要翻译：通过在其中分散有纤维素或羟基烷基取代的胶凝剂将液体单甲基肼转化成一种硫代凝胶。由此获得的凝胶可以在火箭发动机上进行处理和储存，而不会与液体单甲基肼相关联。

4. 发明授权

US06737034B2 Nitric acid production 失效
标题翻译：硝酸生产
公开(公告)号：US06737034B2
公开(公告)日：2004-05-18
申请号：US09923254
申请日：2001-08-02
申请人： Barry D. Allan
发明人： Barry D. Allan
IPC分类号： C01B2138
CPC分类号： C01B21/36 , C01B21/38
摘要： A method process to convert inhibited red fuming nitric acid (IRFNA) and/or nitrogen tetraoxide to either dilute or concentrated (98%+) nitric acid. The method describes a process to remove all of the normal inhibitors (if required), that have been reported to been used in IRFNA. The process described will provide nitric acid free of contaminates which are undesirable when using the nitric acid in reactions to produce other products.
摘要翻译：将抑制的红色发烟硝酸（IRFNA）和/或四氧化氮转化为稀释或浓缩（98％+）硝酸的方法。该方法描述了已经报道用于IRFNA的所有正常抑制剂（如果需要）的方法。所述方法将提供没有污染物的硝酸盐，当在产生其它产物的反应中使用硝酸时，这是不希望的。

5. 发明授权

US5247000A Fiber optic adhesive 失效
标题翻译：光纤胶
公开(公告)号：US5247000A
公开(公告)日：1993-09-21
申请号：US584664
申请日：1990-09-14
申请人： Barry D. Allan
发明人： Barry D. Allan
IPC分类号： B65H55/00 , B65H71/00 , C03C25/10 , C08G18/69 , C09J175/14
CPC分类号： C08G18/69 , B65H55/00 , B65H71/00 , C03C25/104 , C03C25/1065 , C09J175/14
摘要： A fiber optic adhesive composition for applying to a fiber optic having a ffer coat thereon and subsequently, partially cured to a tacky outer surface prior to its being wound onto a bobbin from which the adhesively coated fiber optic material is to payout during use to transmit a signal to a missile in flight. The partially cured adhesive composition functions to hold the fiber optic material in place on the bobbin during storage and allows consistent payout during use of the fiber optic material. The typical composition of the fiber optic adhesive comprises hydroxyterminated polybutadiene from about 88.14 to about 92.48 percent by weight, isophorone diisocyanate from about 6.23 to about 6.42 percent by weight, a catalyst of ferric acetylacetonate or dibutyltin dilaurate in an amount from about 0.89 to about 1.15 percent by weight respectively, and a thixotropic agent in an amount of about 4.48 by weight.
摘要翻译：一种光纤粘合剂组合物，用于在其上具有缓冲涂层的光纤上施加，随后在其被缠绕到线轴上之前部分地固化到发粘的外表面，在该线轴上，粘合涂覆的光纤材料将在使用期间从其上支付以传输向飞行中的导弹发出信号。部分固化的粘合剂组合物用于在存储期间将光纤材料保持在线轴上的适当位置，并且允许在使用光纤材料期间一致地进行支付。纤维光学粘合剂的典型组成包括约88.14-约92.48重量％的羟基封端的聚丁二烯，约6.23至约6.42重量％的异佛尔酮二异氰酸酯，乙酰丙酮铁或二月桂酸二丁基锡的催化剂，其量为约0.89至约1.15 ，触变剂的量为约4.48重量％。

6. 发明授权

US4664730A Tactical monopropellant 失效
标题翻译：战术单推进剂
公开(公告)号：US4664730A
公开(公告)日：1987-05-12
申请号：US848864
申请日：1986-04-07
申请人： Barry D. Allan
发明人： Barry D. Allan
IPC分类号： C06B47/08
CPC分类号： C06B47/08 , Y10S149/12 , Y10S149/122
摘要： The incorporation of methyl alcohol into a hydrazine, and hydrazine nitrateuel blend is effective in lowering the freezing point of the combination while enhancing the performance of the monopropellant blend by contributing to the total energy of the monopropellant ternary combination. Hydrazine content varies from about 58 to about 68 weight percent, the hydrazine nitrate varies from about 20 to about 25 weight percent, and the methyl alcohol varies from about 12 to about 17 weight percent. The freezing point of this monopropellant fuel blend has a freezing point from about -29.degree. F. to about -65.degree. F., which renders this monopropellant fuel blend useful as a tactical monopropellant fuel blend over a wide temperature range.
摘要翻译：将甲醇引入肼和硝酸肼燃料混合物中有效降低组合的凝固点，同时通过促进单组分推进剂三元组合的总能量来增强单组分推进剂共混物的性能。肼含量从约58％至约68％（重量）变化，硝酸肼的变化范围为约20至约25％（重量），甲醇的变化范围为约12至约17％（重量）。该单组分推进剂燃料共混物的凝固点具有约-29°F至约-65°F的凝固点，这使得该单组分推进剂燃料混合物可用作在宽温度范围内的战术单组分推进剂燃料混合物。

7. 发明授权

US4039360A Gelled monomethylhydrazine thixotropic fuel 失效
标题翻译：凝胶单甲肼触变燃料
公开(公告)号：US4039360A
公开(公告)日：1977-08-02
申请号：US179217
申请日：1971-09-09
申请人： Barry D. Allan
发明人： Barry D. Allan
IPC分类号： C06B23/00 , C06B47/08
CPC分类号： C06B23/001 , C06B47/08
摘要： A thixotropic rocket fuel composed of monomethylhydrazine, metallic fuel particles, dimethylurea, and a gellant. The particular thixotropic fuel is particularly characterized by the fact that a low gellant concentration can be used and by the fact that the metallic fuel particles can be suspended with no separation or settling out of the metallic fuel particles in the fuel even when subjected to 500 g's. The particular thixotropic rocket fuel has high density quality and high specific impulse values.
摘要翻译：由单甲基肼，金属燃料颗粒，二甲基脲和胶凝剂组成的触变性火箭燃料。具体的触变燃料的特征特征在于可以使用低胶凝剂浓度，并且由于金属燃料颗粒即使经受500g的燃料颗粒也可以悬浮在燃料中的金属燃料颗粒中而不会分离或沉淀。特定的触变式火箭燃料具有高密度质量和高比冲量值。

8. 发明授权

US6165293A Thixotropic IRFNA gel 失效
标题翻译：触变性IRFNA凝胶
公开(公告)号：US6165293A
公开(公告)日：2000-12-26
申请号：US500642
申请日：1983-05-26
申请人： Barry D. Allan
发明人： Barry D. Allan
IPC分类号： C06B23/00 , C06B47/04 , C06B45/02
CPC分类号： C06B23/001 , C06B47/04 , Y10S149/11 , Y10S149/112
摘要： A thixotropic oxidizer gel comprising inhibited red fuming nitric acid (IA) as the carrier with lithium nitrate (LiNO.sub.3) suspended therein and gelled with a gellant agent of SiO.sub.2 having a mean particle size of 0.015 microns has the rheological properties which can be tailored to match those of MICOM GEL, a fuel gel.A thixotropic gelled fuel (MICOM GEL) has been of particular interest because of its increased safety, reduced sloshing, ease of pumping at zero gravity and ability to suspend high concentrations of high-energy ingredients. However, a gelled oxidizer has been desired for use with the gelled fuel to constitute a thixotropic gelled propellant system. The combination of a gelled fuel (MICOM GEL) and a gelled oxidizer is now a reality after the development of the thixotropic oxidizer gel disclosed above. Of major significance is the matching of the rheologial properties of the two gels so that an oxidizer/fuel (O/F) ratio shift does not occur with a temperature change. The development of the thixotropic oxidizer gel obviates the problems of O/F shift attributed to using a liquid IRFNA oxidizer with MICOM GEL. The combination of the thixotropic oxidizer gel comprising the carrier of IRFNA in weight percent amounts from about 55.0 to 86.0, the suspended LiNO.sub.3 in weight percent amounts from about 10.0 to 40.0, and the gellant agent of SiO.sub.2 in weight percent amounts from about 4.0 to about 5.0 with MICOM GEL fuel offers both high Isp and high density Isp which translates to significant increases in total system performance. This combination reflects a range increase to 160 percent of the present system.
摘要翻译：包含被阻止的红色发烟硝酸（IRFNA）作为载体的硝酸锂（LiNO 3）悬浮在其中并用平均粒度为0.015微米的SiO 2胶凝剂凝胶化的触变氧化剂凝胶具有流变特性，其可以被定制以匹配那些MICOM GEL，一种燃料胶。触变凝胶燃料（MICOM GEL）由于其增加的安全性，减少的晃动，在零重力下的抽吸容易性以及悬浮高浓度高能量成分的能力而特别令人感兴趣。然而，胶凝的氧化剂已经被期望与凝胶燃料一起使用以构成触变胶凝的推进剂系统。在上述公开的触变氧化剂凝胶之后，胶凝燃料（MICOM GEL）和凝胶化氧化剂的组合现在成为现实。重要的意义在于两种凝胶的流变特性的匹配，使得随温度变化不会发生氧化剂/燃料（O / F）比率的偏移。触变氧化剂凝胶的发展消除了使用液体IRFNA氧化剂与MICOM GEL引起的O / F漂移的问题。包含IRFNA载体的触变氧化剂凝胶的组合，其重量百分数为约55.0至86.0，悬浮的LiNO 3的重量百分比为约10.0至40.0，SiO 2的胶凝剂的重量百分比约为4.0至约 5.0与MICOM GEL燃料提供高Isp和高密度Isp，这意味着总系统性能显着提高。这种组合反映了现有系统的范围增加到160％。

9. 发明授权

US6063219A Higher density inhibited red fuming nitric acid (IRFNA) oxidizer gel 失效
标题翻译：更高的密度抑制红色发烟硝酸（IRFNA）氧化凝胶
公开(公告)号：US6063219A
公开(公告)日：2000-05-16
申请号：US306030
申请日：1999-05-06
申请人： Darren M. Thompson , Barry D. Allan
发明人： Darren M. Thompson , Barry D. Allan
IPC分类号： C06B47/04 , F02K9/70 , A62D9/00 , C01B21/38 , F02K9/00 , C04K3/000
CPC分类号： C06B47/04 , F02K9/70
摘要： A high density inhibited red fuming nitric acid oxidizer gel is disclosed ich results in an improvement from 0.5% to about 1.0.% in the impulse over a baseline formulation containing 14% nitrogen tetroxide. An improvement from about 3.0% to about 6.0% is achieved in the density impulse baseline formulation. The higher density inhibited red fuming nitric acid is derived by adding from about 15 percent by weight to about 45 percent by weight percent of nitrogen tetroxide to nitric acid in an amount from about 80 percent by weight to about 40 percent by weight. The other ingredient of the oxidizer gel comprise a gellant of about 0-10 percent by weight, water from about 0-4 percent by weight, and an inhibitor agent of about 0-1 percent by weight. IRFNA is inhibited with phosphoric acid, iodine compounds, or hydrogen fluoride which is present in the oxidizer gel as an additive. The higher density IRFNA oxidizer gel or liquid can be used in airbreathing propulsion systems; a bipropellant formulation is used to provide variable thrust. The oxidizer can also be used with air turbo rocket propulsion systems to augment air combustion with fuel gases. It can be used in a liquid or gel/solid system wherein the oxidizer is sprayed in contact with a solid propellant.
摘要翻译：公开了一种高密度抑制的红色发烟硝酸氧化剂凝胶，其导致在含有14％氮氧化物的基线制剂上的脉冲中0.5％至约1.0％的改善。在密度脉冲基线配方中实现了约3.0％至约6.0％的改善。通过从约80重量％至约40重量％的量向硝酸中添加约15重量％至约45重量％的四氧化氮，来产生较高密度的红色发烟硝酸。氧化剂凝胶的另一成分包含约0-10重量％的胶凝剂，约0-4重量％的水和约0-1重量％的抑制剂。作为添加剂，存在于氧化剂凝胶中的磷酸，碘化合物或氟化氢抑制IRFNA。更高密度的IRFNA氧化剂凝胶或液体可用于空气呼吸推进系统; 使用双组分推进剂制剂来提供可变推力。氧化剂也可以与空气涡轮火箭推进系统一起使用，以增加燃料气体的空气燃烧。它可以用于液体或凝胶/固体系统，其中氧化剂与固体推进剂相接触地喷雾。

10. 发明授权

US5394690A Constant pressure, variable thrust bipropellant engine 失效
标题翻译：恒压，可变推力双组元推动剂发动机
公开(公告)号：US5394690A
公开(公告)日：1995-03-07
申请号：US123946
申请日：1993-09-20
申请人： Jerrold H. Arszman , William M. Chew , Barry D. Allan
发明人： Jerrold H. Arszman , William M. Chew , Barry D. Allan
IPC分类号： F02K9/86 , F02K3/00 , F02K9/00
CPC分类号： F02K9/86
摘要： A pressure controlled pintle is employed in combination with a throttling quid, gel, or hybrid engine to provide a constant pressure and variable thrust from a single operating engine. As the propellants are throttled back and the chamber pressure drops, the pintle moves and closes the gap between the pintle and nozzle throat, thereby lowering the throat area and re-establishing the design chamber pressure related to pintle spring tension. By retaining the design pressure over a wide thrust range, the engine efficiency remains at the design value. This eliminates the drop of Isp due to pressure and keeps the cost of the system reasonable because only one engine is required. When a higher thrust is desired, a throttling valve in an injector increases the propellant flow rate, which causes a higher pressure in the combustion chamber. The constant pressure actuator moves the pintle to open the nozzle throat, which reduces the pressure to the design value. The design value may not be optimum. There are many size/temperature/volume trade off's relating to the missile as a whole which could move the design value from optimum. Because the pressure in the combustion chamber remains the same, the Isp is not greatly changed, but the thrust level increases because of the increase in the mass flow through nozzle. The combination provides substantially constant combustion chamber pressure for a single variable thrust bipropellant engine.
摘要翻译：与节流液体，凝胶或混合发动机组合使用压力控制枢栓，以提供来自单个操作发动机的恒定压力和可变推力。当推进剂被节流并且室压力下降时，枢轴移动并闭合枢栓和喷嘴喉部之间的间隙，从而降低喉部面积并重新建立与枢轴弹簧张力相关的设计室压力。通过在宽推力范围内保持设计压力，发动机效率保持在设计值。这样可以消除由于压力造成的Isp跌落，并且由于只需要一台发动机，因此可以保持系统的成本合理。当需要更高的推力时，喷射器中的节流阀增加推进剂流速，这导致燃烧室中的较高压力。恒压致动器移动枢轴以打开喷嘴喉部，这将压力降低到设计值。设计值可能不是最佳的。与导弹有关的许多尺寸/温度/体积的交易可以将设计值从最佳状态转移。由于燃烧室内的压力保持不变，所以Isp不会发生很大的变化，但由于喷嘴质量流量的增加，推力水平升高。该组合为单个可变推力双组元推进剂发动机提供基本恒定的燃烧室压力。

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