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    Linear Detonation Wave Diverter
    3.
    发明申请
    Linear Detonation Wave Diverter 审中-公开
    线性爆轰波分路器

    公开(公告)号：US20130199203A1

    公开(公告)日：2013-08-08

    申请号：US13652201

    申请日：2012-10-15

    Applicant: FIRESTAR ENGINEERING, LLC

    Inventor： Gregory S. Mungas ,  Gregory H. Peters ,  Andrew T. Bingham

    IPC: F02K9/38

    CPC classification number: F02K9/38 ,  F02K9/566 ,  F02K9/58

    Abstract: The presently disclosed linear detonation wave diverter 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 within the linear detonation wave diverter. Further, the detonation wave is linearly vented out of the diverter upon the failure of a burst member, which provides a low resistance path for detonation waves to exit the detonation wave diverter.

    Abstract translation: 目前公开的线性爆轰波分流器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，而不会点燃线性爆轰波分流器内的微孔屏障上游的工作流体。 此外，当爆裂构件发生故障时，引爆波从分流器线性地排出，这提供了用于爆震波离开引爆波分流器的低电阻路径。

    Cooling Jacket with Porous Matrix
    4.
    发明申请
    Cooling Jacket with Porous Matrix 审中-公开
    多孔矩阵冷却夹克

    公开(公告)号：US20130276426A1

    公开(公告)日：2013-10-24

    申请号：US13857064

    申请日：2013-04-04

    Applicant: Firestar Engineering, LLC

    Inventor： Gregory S. Mungas ,  David J. Fisher ,  Adam Pollok London ,  Jack Merrill Fryer

    IPC: F02K9/00

    CPC classification number: F02K9/00 ,  F02K9/34 ,  F02K9/40 ,  F02K9/64 ,  F02K9/972 ,  F05D2260/20 ,  Y10T29/49346

    Abstract: The fluids and heat transfer theory for regenerative cooling of a rocket combustion chamber with a porous media coolant jacket is presented. This model is useful for calculating temperature distributions in a coolant fluid and combustion chamber or heat source as well as the associated fluid pressure drop through the coolant jacket. This model for fluids and heat transfer theory can be used to design a regeneratively cooled rocket engine.

    Abstract translation: 介绍了具有多孔介质冷却剂护套的火箭燃烧室再生冷却的流体和热传递理论。 该模型可用于计算冷却剂流体和燃烧室或热源中的温度分布以及通过冷却剂套管的相关流体压降。 该流体和热传递理论模型可用于设计再生冷却火箭发动机。

    Thermal Pressurant
    5.
    发明申请
    Thermal Pressurant 审中-公开
    热压机

    公开(公告)号：US20130196273A1

    公开(公告)日：2013-08-01

    申请号：US13754747

    申请日：2013-01-30

    Applicant: FIRESTAR ENGINEERING, LLC

    Inventor： Gregory S. Mungas

    IPC: F23K5/20 ,  B65D83/72

    CPC classification number: F23K5/20 ,  B65D83/72 ,  F02K9/50

    Abstract: The presently disclosed technology relates to using a combustion/decomposition heater fed by a working fluid stored within a storage tank to thermally pressurize the storage tank. The thermal pressurization may be used to maintain a desired pressure within the storage tank, even as the working fluid within the storage tank is drawn down. Further, a feedback mechanism may also be incorporated that varies the thermal energy added to the working fluid within the storage tank to maintain the desired pressure within the storage tank.

    Abstract translation: 目前公开的技术涉及使用由存储在储罐内的工作流体供给的燃烧分解加热器来对储罐进行热加压。 即使当储存罐内的工作流体被拉下时，也可以使用热加压来保持储罐内的所需压力。 此外，还可以引入反馈机构，其改变添加到储罐内的工作流体的热能，以保持储存罐内所需的压力。

    IN-TANK PROPELLANT MIXING
    6.
    发明申请
    IN-TANK PROPELLANT MIXING 审中-公开
    内燃机推进混合

    公开(公告)号：US20140022859A1

    公开(公告)日：2014-01-23

    申请号：US13753798

    申请日：2013-01-30

    Applicant: FIRESTAR ENGINEERING, LLC

    Inventor： Gregory S. Mungas

    IPC: B01F15/02

    CPC classification number: B01F15/0227 ,  F02K9/605 ,  F05D2250/241 ,  F05D2250/30 ,  F05D2250/36

    Abstract: Separate pressure vessels for oxidizer and fuel components in a combustion/decomposition system add weight and complexity to the system. The fuel and oxidizer can be pre-mixed within a single pressure vessel, but can be unacceptably volatile in a mixed configuration. Providing separate fuel and oxidizer compartments within a singular pressure vessel reduces the weight and complexity of the system, while maintaining the non-volatility of separately stored fuel and oxidizer. The fuel and oxidizer can be selectively mixed within the pressure vessel when desired.

    Abstract translation: 在燃烧/分解系统中用于氧化剂和燃料组分的单独的压力容器增加了系统的重量和复杂性。 燃料和氧化剂可以在单个压力容器内预混合，但在混合构型中可能是不可接受的挥发性的。 在单一压力容器内提供单独的燃料和氧化剂隔室可以降低系统的重量和复杂性，同时保持单独储存的燃料和氧化剂的不挥发性。 如果需要，燃料和氧化剂可以在压力容器内选择性地混合。

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