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公开(公告)号：US20180265427A1
公开(公告)日：2018-09-20
申请号：US15920521
申请日：2018-03-14
IPC分类号： C06B43/00
摘要： The present application generally relates to hypergolic hydrocarbon fuel compositions comprising a convenient fuel and a cycloheptatriene and/or its analogs, and methods of making and using the hypergolic hydrocarbon fuel compositions.
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公开(公告)号：US09598323B2
公开(公告)日：2017-03-21
申请号：US15006652
申请日：2016-01-26
摘要： The present disclosure generally pertains to a rocket propulsion oxidizer compound that is a solution, is a homogenous and stable liquid at room temperature and includes nitrous oxide and nitrogen tetroxide. In addition, an apparatus is provided for burning a fuel and nitrous oxide/nitrogen tetroxide. The apparatus has a combustor, a catalyst, a nitrous oxide/nitrogen tetroxide supply passage for directing the nitrous oxide/nitrogen tetroxide to a contact position with the catalyst, and a fuel supply passage for supplying the fuel to the combustor. The catalyst acts to facilitate decomposition of the nitrous oxide/nitrogen tetroxide, while the combustor burns the fuel, the decomposed nitrous oxide/nitrogen tetroxide and/or nitrous oxide/nitrogen tetroxide decomposed in the reaction.
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公开(公告)号：US20140190598A1
公开(公告)日：2014-07-10
申请号：US14047499
申请日：2013-10-07
IPC分类号： C06B43/00
摘要： A hypergolic bipropellant. The hypergolic bipropellant includes a hydrazinium-based ionic liquid, a nitric acid-based oxidizer, and a catalyst.
摘要翻译： 高血压双组元推进剂。 超高压双组元推进剂包括基于腙的离子液体，基于硝酸的氧化剂和催化剂。
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公开(公告)号：US08617326B1
公开(公告)日：2013-12-31
申请号：US12567136
申请日：2009-09-25
摘要： Advanced bipropellant fuels with fast ignition upon mixing with storable oxidizer (N2O4, nitric acid) have been synthesized and demonstrated. The bipropellant fuels are based upon salts containing dicyanamide or tricyanomethanide anions and employ at least two hydrazine functionalities in the cations.
摘要翻译： 已经合成并证明了与可储存的氧化剂（N2O4，硝酸）混合时具有快速点火的先进的双组分推进剂燃料。 双组元推进剂燃料基于含有二氰胺或三氰基甲烷阴离子的盐，并且在阳离子中使用至少两个肼官能团。
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公开(公告)号：US20130205754A1
公开(公告)日：2013-08-15
申请号：US13715647
申请日：2012-12-14
摘要： The present disclosure generally pertains to a rocket propulsion oxidizer compound that is a solution, is a homogenous and stable liquid at room temperature and includes nitrous oxide and nitrogen tetroxide. In addition, an apparatus is provided for burning a fuel and nitrous oxide/nitrogen tetroxide. The apparatus has a combustor, a catalyst, a nitrous oxide/nitrogen tetroxide supply passage for directing the nitrous oxide/nitrogen tetroxide to a contact position with the catalyst, and a fuel supply passage for supplying the fuel to the combustor. The catalyst acts to facilitate decomposition of the nitrous oxide/nitrogen tetroxide, while the combustor burns the fuel, the decomposed nitrous oxide/nitrogen tetroxide and/or nitrous oxide/nitrogen tetroxide decomposed in the reaction.
摘要翻译： 本公开通常涉及作为溶液的火箭推进氧化剂化合物，在室温下是均匀且稳定的液体，并且包括一氧化二氮和四氧化氮。 此外，提供了用于燃烧燃料和一氧化二氮/四氧化氮的装置。 该装置具有燃烧器，催化剂，用于将一氧化二氮/氮氧化物引导到与催化剂接触位置的一氧化二氮/四氧化二氮供应通道，以及用于将燃料供给燃烧器的燃料供给通道。 催化剂用于促进一氧化二氮/氮氧化物的分解，同时燃烧器燃烧燃料，分解的一氧化二氮/四氧化氮和/或一氧化二氮/四氧化二氮在反应中分解。
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公开(公告)号：US20130181168A1
公开(公告)日：2013-07-18
申请号：US13745544
申请日：2013-01-18
申请人： Pioneer Astronautics
发明人： Robert M. Zubrin , David Kenneth Strott , Anthony Muscatello , Nicholas F. Jameson , Emily Bostwick-White
IPC分类号： B01J7/00
CPC分类号： B01J8/0285 , B01J7/00 , B01J23/42 , B01J23/46 , B01J23/464 , B01J23/72 , B01J23/755 , C01B13/0203 , C01B21/02 , C06B47/04 , C06D5/04 , Y02C20/10
摘要： Methods and devices for generating gas from nitrous oxide are provided as well as downstream uses for the product gas. Reactor devices of the invention are compact and incorporate a novel heat-exchange/regenerative cooling system to optimize N2O decomposition and reactor durability.
摘要翻译： 提供了从一氧化二氮产生气体的方法和装置以及产品气体的下游用途。 本发明的反应器装置是紧凑的并且包括一种新的热交换/再生冷却系统来优化N2O分解和反应器耐久性。
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公开(公告)号：US20120144799A1
公开(公告)日：2012-06-14
申请号：US11619674
申请日：2007-01-04
摘要： A rocket propulsion oxidizer compound that is a mixture that is a homogenous and stable liquid at room temperature that includes nitrous oxide and nitrogen tetroxide.
摘要翻译： 火箭推进氧化剂化合物，其是在室温下是均匀且稳定的液体的混合物，其包括一氧化二氮和四氧化氮。
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公开(公告)号：US20090320973A1
公开(公告)日：2009-12-31
申请号：US11292442
申请日：2005-12-02
申请人： Roberto Di Salvo
发明人： Roberto Di Salvo
IPC分类号： C06B47/00
CPC分类号： C06B47/12 , C06B47/04 , F17C2221/03 , F17C2227/0348 , F17C2227/0388 , F17C2265/025 , F17C2270/0194
摘要： The present invention is a bi-propellant system comprising a gelled liquid propane (GLP) fuel and a gelled MON-30 (70% N2O4+30% NO) oxidizer. The bi-propellant system is particularly well-suited for outer planet missions greater than 3 AU from the sun and also functions in earth and near earth environments. Additives such as powders of boron, carbon, lithium, and/or aluminum can be added to the fuel component to improve performance or enhance hypergolicity. The gelling agent can be silicon dioxide, clay, carbon, or organic or inorganic polymers. The bi-propellant system may be, but need not be, hypergolic.
摘要翻译： 本发明是一种双推进剂系统，其包括凝胶液态丙烷（GLP）燃料和凝胶MON-30（70％N2O4 + 30％NO）氧化剂。 双推进剂系统特别适用于大于3 AU的太阳外部行星任务，并且在地球和近地环境中也起作用。 可以将添加剂如硼，碳，锂和/或铝的粉末加入到燃料组分中，以改善性能或增加超高性。 胶凝剂可以是二氧化硅，粘土，碳或有机或无机聚合物。 双推进剂系统可以是但不一定是高通量的。
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公开(公告)号：US20030042719A1
公开(公告)日：2003-03-06
申请号：US09932672
申请日：2001-08-17
发明人： Karl K. Rink , Anthony M. Young , David J. Green
IPC分类号： B60R021/26
摘要： Inflation apparatuses and methods are provided wherein a hydrocarbon-containing inflation gas-producing mixture is formed via the fluid extraction of the hydrocarbon from a substrate material.
摘要翻译： 提供了充气装置和方法，其中通过烃从基底材料的流体萃取形成含烃膨胀气体产生混合物。
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公开(公告)号：US20010045248A1
公开(公告)日：2001-11-29
申请号：US09841222
申请日：2001-04-23
申请人： Quoin, Inc.
IPC分类号： C06B047/04
摘要： Batch-mode and continuous-mode decomposition of nitrous oxide is used to provide multiple ignitions of a solid-propellant gas generator and subsequently control its output gas temperature and flow rate, respectively. To reignite the solid-propellant gas generator, a controlled mass of a reactive oxidizer, such as hot nitrous oxide decomposition products, is injected into the gas generator chamber.
摘要翻译： 分配模式和连续模式分解一氧化二氮用于提供固体推进剂气体发生器的多次点火，并分别控制其输出气体温度和流量。 为了重新点燃固体推进剂气体发生器，将受控质量的反应性氧化剂（例如热氧化亚氮分解产物）注入到气体发生器室中。
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