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1. 发明申请

WO2013103427A2 LINEAR DETONATION WAVE DIVERTER 审中-公开
标题翻译：线性爆轰波分配器
公开(公告)号：WO2013103427A2
公开(公告)日：2013-07-11
申请号：PCT/US2012/060286
申请日：2012-10-15
申请人： FIRESTAR ENGINEERING, LLC , MUNGAS, Gregory S. , PETERS, Gregory H. , BINGHAM, Andrew T.
发明人： MUNGAS, Gregory S. , PETERS, Gregory H. , BINGHAM, Andrew T.
IPC分类号： F02K1/00 , F02K1/44 , F02K9/00 , F02K9/38
CPC分类号： F02K9/38 , F02K9/566 , F02K9/58
摘要： The presently disclosed linear detonation wave diverter (600) provides a structure and method for quickly and controllably venting a detonation event out of the diverter without igniting working fluid upstream of a microporous barrier (626) within the linear detonation wave diverter. Further, the detonation wave is linearly vented out of the diverter upon the failure of a burst member (682), which provides a low resistance path for detonation waves to exit the detonation wave diverter.
摘要翻译：目前公开的线性爆震波分流器（600）提供了一种结构和方法，用于快速并可控地将爆震事件排出分流器外而不会点燃线性内的微孔隔板（626）上游的工作流体爆轰波分流器。此外，当爆破构件（682）失效时，爆炸波线性地从分流器排出，这为爆震波离开爆轰波分流器提供了低阻力路径。

2. 发明申请

WO2012149462A2 VARIABLE SUCTION EXHAUST 审中-公开
标题翻译：可变吸烟排气
公开(公告)号：WO2012149462A2
公开(公告)日：2012-11-01
申请号：PCT/US2012035641
申请日：2012-04-27
申请人： FIRESTAR ENGINEERING LLC , MUNGAS GREGORY , BUCHANAN LARRY
发明人： MUNGAS GREGORY , BUCHANAN LARRY
IPC分类号： F01N13/08
CPC分类号： F01N13/082 , F01N13/20 , F01N2260/06 , F01N2270/08 , Y10T137/0329 , Y10T137/2599
摘要： A throttleable exhaust venturi (700) is described herein that generates strong suction pressures at an exhaust outlet (718) by accelerating an incoming ambient fluid stream with the aid of a venturi to high gas velocities and injecting a combustion exhaust stream into the ambient fluid stream at an effective venturi throat (728). A mixing element (544) downstream of the venturi throat ensures that the mixed fluid stream recovers from a negative static pressure up to local atmospheric pressure. A physical (724) and the effective (728) throat of the venturi (700) are designed to promote mixing and stabilize the ambient fluid flow to ensure that high velocity is achieved and the effective venturi is operable over a variety of combustion exhaust stream mass flow rates.
摘要翻译：本文描述了一种可节流的排气文丘里管（700），其通过在文氏管的帮助下将进入的环境流体流加速到高气体速度并将燃烧废气流注入到环境流体流中而在排气出口（718）处产生强吸入压力在有效的文丘里喉咙（728）。文丘里喉部下游的混合元件（544）确保混合流体流从负静压力恢复到局部大气压力。文丘里管（700）的物理（724）和有效（728）喉部被设计成促进混合和稳定环境流体流动，以确保实现高速度，并且有效文丘里管可在多种燃烧废气流质量流量。

3. 发明申请

WO2013033437A2 THERMAL PHASE SEPARATION 审中-公开
标题翻译：热相分离
公开(公告)号：WO2013033437A2
公开(公告)日：2013-03-07
申请号：PCT/US2012/053196
申请日：2012-08-30
申请人： FIRESTAR ENGINEERING, LLC , MUNGAS, Gregory
发明人： MUNGAS, Gregory
IPC分类号： F02K9/44 , B01D17/00 , F02K9/56
CPC分类号： F02K9/44 , B64G1/402 , F05D2260/20 , Y10T137/0391 , Y10T137/6416
摘要： A thermal variation source (318) (e.g., a heater or a heat sink) is used to induce a temperature gradient across an interior surface of a storage tank (302). The storage tank stores a working fluid (e.g., a fuel, and oxidizer, or a monopropellant) that may have pockets of gaseous-phase working fluid interspersed within liquid-phase working fluid, or vice versa. In the absence of gravity or other significant forces on the working fluid, the temperature gradient is sufficient to cause phase-separation of the working fluid and allow either the liquid-phase or the gaseous-phase working fluid to be withdrawn from the storage tank, as desired.
摘要翻译：使用热变化源（318）（例如，加热器或散热器）来引导跨越储罐（302）的内表面的温度梯度。存储罐存储可以具有散布在液相工作流体内的气相工作流体袋的工作流体（例如，燃料和氧化剂或单一推进剂），反之亦然。在工作流体没有重力或其他重要的力的情况下，温度梯度足以引起工作流体的相分离，并允许液相或气相工作流体从储罐中取出，如预期的。

4. 发明申请

WO2012149462A3 VARIABLE SUCTION EXHAUST 审中-公开
公开(公告)号：WO2012149462A3
公开(公告)日：2012-11-01
申请号：PCT/US2012/035641
申请日：2012-04-27
申请人： FIRESTAR ENGINEERING, LLC , MUNGAS, Gregory , BUCHANAN, Larry
发明人： MUNGAS, Gregory , BUCHANAN, Larry
IPC分类号： F01N13/08
摘要： A throttleable exhaust venturi (700) is described herein that generates strong suction pressures at an exhaust outlet (718) by accelerating an incoming ambient fluid stream with the aid of a venturi to high gas velocities and injecting a combustion exhaust stream into the ambient fluid stream at an effective venturi throat (728). A mixing element (544) downstream of the venturi throat ensures that the mixed fluid stream recovers from a negative static pressure up to local atmospheric pressure. A physical (724) and the effective (728) throat of the venturi (700) are designed to promote mixing and stabilize the ambient fluid flow to ensure that high velocity is achieved and the effective venturi is operable over a variety of combustion exhaust stream mass flow rates.

5. 发明申请

WO2008123895A2 SPARK-INTEGRATED PROPELLANT INJECTOR HEAD WITH FLASHBACK BARRIER 审中-公开
标题翻译： SPARK集成推进式喷射器头与闪光障碍
公开(公告)号：WO2008123895A2
公开(公告)日：2008-10-16
申请号：PCT/US2007086410
申请日：2007-12-04
申请人： FIRESTAR ENGINEERING LLC , MUNGAS GREGORY S , FISHER DAVID J , MUNGAS CHRISTOPHER
发明人： MUNGAS GREGORY S , FISHER DAVID J , MUNGAS CHRISTOPHER
IPC分类号： F02K9/95 , F02K9/62 , F02K9/64
CPC分类号： F02K9/52 , F02K9/94 , F02K9/95
摘要： High performance propellants flow through specialized mechanical hardware that allows for effective and safe thermal decomposition and/or combustion of the propellants. By integrating a sintered metal component between a propellant feed source and the combustion chamber, an effective and reliable fuel injector head may be implemented. Additionally the fuel injector head design integrates a spark ignition mechanism that withstands extremely hot running conditions without noticeable spark mechanism degradation.
摘要翻译：高性能推进剂流经专门的机械硬件，可以有效和安全的分解和/或燃烧推进剂。通过在推进剂进料源和燃烧室之间集成烧结金属部件，可以实现有效和可靠的燃料喷射头。另外，燃料喷射头设计集成了一种火花点火机构，其能够承受极热的运行状态，而不会引起明显的火花机械劣化。

6. 发明申请

WO2011152912A3 SUPERSONIC COMBUSTOR ROCKET NOZZLE 审中-公开
标题翻译：超声波燃烧器口袋喷嘴
公开(公告)号：WO2011152912A3
公开(公告)日：2014-03-27
申请号：PCT/US2011028400
申请日：2011-03-14
申请人： FIRESTAR ENGINEERING LLC , MUNGAS GREGORY S
发明人： MUNGAS GREGORY S
IPC分类号： F02C5/02 , F02K7/14
CPC分类号： F02K9/97 , F05D2210/30 , F05D2250/232
摘要： A supersonic combustor as a component of a rocket nozzle offers improved utilization of available chemical energy that may be released from combustion gasses flowing through the rocket nozzle. A subsonic combustor compresses and sub-sonically accelerates an exothermically reacting combustion gas up to a nozzle throat. The supersonic combustor expands and super-sonically accelerates the exothermically reacting combustion gas beyond the nozzle throat. The dimensions of the supersonic combustor may be selected such that the supersonic combustor achieves a slow rate of cooling of the combustion gasses without creating Shockwaves within the supersonic combustor. A supersonic discharge expands and super-sonically accelerates the now substantially non-reacting combustion gas through a supersonic discharge of the rocket nozzle. The momentum of the combustion gas leaving the supersonic discharge propels the rocket nozzle in the opposite direction due to the principle of conservation of momentum.
摘要翻译：作为火箭喷嘴的组件的超音速燃烧器提供了可以从流过火箭喷嘴的燃烧气体释放的可用化学能的改进的利用。亚音速燃烧器压缩和超声加速放热反应燃烧气体直到喷嘴喉部。超音速燃烧器膨胀并超声波加速了放热反应的燃烧气体超过喷嘴喉部。可以选择超音速燃烧器的尺寸，使得超音速燃烧器实现缓慢的燃烧气体冷却速率，而不会在超音速燃烧器内产生冲击波。超音速放电通过火箭喷嘴的超音速放电扩展并超声波加速现在基本上不反应的燃烧气体。离开超音速放电的燃烧气体的动量由于动量守恒的原理而使火箭喷嘴向相反方向推进。

7. 发明申请

WO2013105988A2 CLUSTERED, FIXED CANT, THROTTLEABLE ROCKET ASSEMBLY 审中-公开
标题翻译：集合式，固定式CANT，可折叠式摇摆组件
公开(公告)号：WO2013105988A2
公开(公告)日：2013-07-18
申请号：PCT/US2012/025308
申请日：2012-02-15
申请人： FIRESTAR ENGINEERING, LLC , FISHER, David , MUNGAS, Gregory
发明人： FISHER, David , MUNGAS, Gregory
IPC分类号： F02K9/00 , F02K9/30 , F02K9/26 , F02K9/42
CPC分类号： F02K9/00 , F02K9/58 , F02K9/82 , F02K9/88 , F05D2240/40 , F05D2250/314
摘要： A clustered, fixed cant, throttleable rocket assembly (102) is used to propel and a steer a vessel (100) in terrestrial or extraterrestrial applications. The fixed cant of each of at least three individual rocket engines (104, 106, 108) in the cluster provides the steering input to the overall assembly (102). More specifically, by changing the propellant flow rate to the individual rocket engines (104, 106, 108) relative to one another, the overall thrust vector of the rocket assembly (102) may be selected to provide a desired steering input to the vessel (100). A measured vessel orientation may be compared with a desired vessel orientation to determine what steering input is required to achieve the desired vessel orientation.
摘要翻译：聚集的，固定的倾斜可控制的火箭组件（102）用于推进和引导在陆地或地球外应用中的船只（100）。群集中的至少三个单独的火箭发动机（104,106,108）中的每一个的固定倾斜物提供了到整个组件（102）的转向输入。更具体地，通过相对于彼此改变到各个火箭发动机（104,106,108）的推进剂流量，可以选择火箭组件（102）的总推力向量以向船舶提供期望的转向输入（ 100）。可以将测量的血管取向与期望的血管方向进行比较，以确定实现所需血管方向所需的转向输入。

8. 发明申请

WO2011091162A1 INSULATED COMBUSTION CHAMBER 审中-公开
标题翻译：绝缘燃烧室
公开(公告)号：WO2011091162A1
公开(公告)日：2011-07-28
申请号：PCT/US2011/021917
申请日：2011-01-20
申请人： FIRESTAR ENGINEERING, LLC , MUNGAS, Gregory, S. , PETERS, Gregory, H. , DOYLE, Kenneth , BUCHANAN, Larry, R. , BANZON, Jose, T.
发明人： MUNGAS, Gregory, S. , PETERS, Gregory, H. , DOYLE, Kenneth , BUCHANAN, Larry, R. , BANZON, Jose, T.
IPC分类号： F02B77/11
CPC分类号： F02F3/12 , F02F3/0084 , F02F3/02 , F02F3/10 , F05C2253/04 , F05C2253/12 , F05C2253/14 , Y10T29/49252
摘要： An insulative piston or piston cap creates a highly thermally resistive path in the axial direction of the piston or piston cap toward a crank case of an engine. An insulative cylinder is configured to be positioned around the insulative piston and adjacent an insulative cylinder head, and to provide thermal resistance in the cylinder's axial direction. The insulated cylinder head is configured to resist heat flow in the axial direction away from the crank case. High temperature insulation surrounding these structures is configured to resist heat flow out of a combustion chamber of the engine. These insulative components, together, form the fully insulated combustion chamber.
摘要翻译：绝缘活塞或活塞盖在活塞或活塞帽的轴向方向上朝向发动机的曲轴箱产生高度耐热的路径。绝缘筒构造成围绕绝缘活塞定位并且邻近绝缘气缸盖，并且在气缸的轴向方向上提供热阻。隔热气缸盖构造为抵抗远离曲轴箱的轴向热流动。围绕这些结构的高温绝热被构造成抵抗从发动机的燃烧室流出的热量。这些绝缘部件一起形成完全绝缘的燃烧室。

9. 发明申请

WO2011005895A1 ALUMINUM POROUS MEDIA 审中-公开
标题翻译：铝多孔介质
公开(公告)号：WO2011005895A1
公开(公告)日：2011-01-13
申请号：PCT/US2010/041259
申请日：2010-07-07
申请人： FIRESTAR ENGINEERING LLC , MUNGAS, Gregory, S , PETERS, Gregory, H. , SMITH, Jon, A.
发明人： MUNGAS, Gregory, S , PETERS, Gregory, H. , SMITH, Jon, A.
IPC分类号： H01L21/20
CPC分类号： F02K9/566 , F16K17/366 , F16K17/40 , F23D14/82 , Y10T29/49 , Y10T156/10
摘要： Disclosed are materials of variable density or tiered porosity micro-fluidic porous media structures of sintered metal or other materials, and methods of making same. An embodiment discloses an aluminum porous media element of variable density having a tiered porosity micro-fluidic media structure. A method of making the aluminum porous media element disclosed herein includes mixing a binding agent with a metal powder to generate a first mixture, heating the first mixture to a sub metal sintering temperature to get a homogeneous composite of the metal powder and heating the homogeneous composite to a metal sintering temperature to sinter-bond the metal powder to get a porous media of first porosity.
摘要翻译：公开了烧结金属或其他材料的可变密度或分层孔隙微孔多孔介质结构的材料及其制造方法。一个实施方案公开了具有分层孔隙度微流体介质结构的可变密度的铝多孔介质元件。制造本文公开的铝多孔介质元件的方法包括将粘合剂与金属粉末混合以产生第一混合物，将第一混合物加热至亚金属烧结温度以获得金属粉末的均匀复合物并加热均匀复合物到金属烧结温度以烧结粘合金属粉末以获得第一孔隙度的多孔介质。

10. 发明申请

WO2013103427A3 LINEAR DETONATION WAVE DIVERTER 审中-公开
标题翻译：线性爆震波导
公开(公告)号：WO2013103427A3
公开(公告)日：2013-10-03
申请号：PCT/US2012060286
申请日：2012-10-15
申请人： FIRESTAR ENGINEERING LLC , MUNGAS GREGORY S , PETERS GREGORY H , BINGHAM ANDREW T
发明人： MUNGAS GREGORY S , PETERS GREGORY H , BINGHAM ANDREW T
IPC分类号： F02K1/00 , F02K1/44 , F02K9/00 , F02K9/38
CPC分类号： F02K9/38 , F02K9/566 , F02K9/58
摘要： The presently disclosed linear detonation wave diverter (600) provides a structure and method for quickly and controllably venting a detonation event out of the diverter without igniting working fluid upstream of a microporous barrier (626) within the linear detonation wave diverter. Further, the detonation wave is linearly vented out of the diverter upon the failure of a burst member (682), which provides a low resistance path for detonation waves to exit the detonation wave diverter.
摘要翻译：目前公开的线性爆轰波分流器（600）提供了一种结构和方法，用于将引爆事件快速和可控地排出分流器，而不会点燃线性爆震波分流器内微孔势垒（626）上游的工作流体。此外，当爆裂构件（682）发生故障时，引爆波从分流器线性地排出，其提供用于爆震波离开引爆波分流器的低电阻路径。

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