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    OPTICAL HEAT EXCHANGER AND ASSOCIATED METHOD
    2.
    发明申请
    OPTICAL HEAT EXCHANGER AND ASSOCIATED METHOD 审中-公开

    公开(公告)号：US20180202392A1

    公开(公告)日：2018-07-19

    申请号：US15919875

    申请日：2018-03-13

    申请人： The Boeing Company

    发明人： Brian J. TILLOTSON

    IPC分类号： F02K7/08 ,  B64G1/40

    CPC分类号： F02K7/08 ,  B64G1/401 ,  B64G1/409 ,  F02K99/00 ,  F24S23/30 ,  F24S40/55 ,  F24S70/60 ,  Y02E10/44 ,  Y02T50/671

    摘要： An optical heat exchanger and an associated system and method are provided to allow a vehicle, such as an unmanned air vehicle, a rocket or the like, to deliver more payload at a lower cost. The optical heat exchanger includes a support surface defining a plurality of tapered openings. Each tapered opening tapers from the first size proximate an outwardly facing end of the opening to a second smaller size proximate an inwardly facing end of the opening. The inwardly facing end of each tapered opening is in communication with the propellant. The optical heat exchanger also includes a plurality of lenses with each lens positioned proximate the outwardly facing end of a respective opening. Each lens is configured to receive an electromagnetic energy beam and concentrate the majority of the electromagnetic energy beam through the inwardly facing end of the respective tapered opening, thereby heating the propellant.

    Propulsion motor using fine particulate material
    5.
    发明授权
    Propulsion motor using fine particulate material 失效
    推进电机采用精细颗粒材料

    公开(公告)号：US5090195A

    公开(公告)日：1992-02-25

    申请号：US602584

    申请日：1990-10-23

    申请人： Jocelyn Boily

    发明人： Jocelyn Boily

    IPC分类号： F02K99/00

    CPC分类号： F02K99/00

    摘要： A propulsion motor using a fine particulate material, having a heat content, the material being fed to a convergent portion upstream of and adjacent to the throat of a propulsion nozzle. A fluid under pressure is also fed to the convergent portion, to mix with the particulate material. The fluid is heated by the particulate material, increasing volume and speed, the particulate material and the fluid ejecting from the nozzle. A particular use of such a motor would be on the moon, or some other body, where a fine particulate material can be made available locally.

    摘要翻译： 使用具有热含量的细颗粒材料的推进马达，该材料被供给到推进喷嘴的喉部的上游和邻近的收敛部分。 在压力下的流体也被送入收敛部分，以与颗粒材料混合。 流体被颗粒材料加热，增加体积和速度，颗粒材料和流体从喷嘴喷出。 这样的电动机的特定用途将在月球上或其他可以在本地获得细颗粒材料的其它主体。

    VAPOR JET SYSTEM ENABLING JETTING FOR MANY SECONDS USING MULTIPLE KINDS OF MUTUALLY INSOLUBLE LIQUID GASES AS FUEL
    7.
    发明申请
    VAPOR JET SYSTEM ENABLING JETTING FOR MANY SECONDS USING MULTIPLE KINDS OF MUTUALLY INSOLUBLE LIQUID GASES AS FUEL 审中-公开
    蒸汽喷射系统使用多种不相容的液体气体作为燃料启动多次喷射

    公开(公告)号：US20170073089A1

    公开(公告)日：2017-03-16

    申请号：US15310419

    申请日：2015-05-11

    申请人： Japan Aerospace Exploration Agency

    发明人： Junichiro KAWAGUCHI ,  Osamu MORI ,  Takayuki YAMAMOTO ,  Norizumi MOTOOKA ,  Toshihiro CHUJO

    IPC分类号： B64G1/40 ,  F02K9/60

    CPC分类号： B64G1/401 ,  B64G1/402 ,  F02K9/50 ,  F02K9/605 ,  F02K99/00 ,  F03H99/00

    摘要： A vapor jet system to continuously jet vapors while suppressing cavitation. One vapor jet system includes a liquid storage part for separately storing two or more kinds of mutually insoluble liquids; a jet orifice; and a jet control part. Jetting the vapors is from a state where pressure in the space storing the vapors in the liquid storage part is higher than the saturated vapor pressure in any of the two or more kinds of liquids. Alternatively, a vapor jet system can include a fluid storage part storing one kind of liquid and at least one kind of inactive gas having a composition different from the liquid; a similar jet orifice; and a similar jet control part. Jetting the vapors and inactive gas(es) is (are) from a state where pressure in a vapor storing space in the fluid storage part is higher than the saturated vapor pressure in the liquid.

    摘要翻译： 一种蒸汽喷射系统，用于在抑制气蚀的同时连续喷射蒸汽。 一种蒸汽喷射系统包括用于分别存储两种或多种相互不溶解的液体的液体储存部分; 喷嘴孔; 和喷射控制部。 蒸气的喷射是从存储液体储存部分中的蒸气的空间中的压力高于两种或更多种液体中的任一种的饱和蒸气压的状态。 或者，蒸汽喷射系统可以包括存储一种液体的液体储存部分和具有不同于液体的组成的至少一种惰性气体; 类似的喷射孔; 和类似的喷射控制部分。 从液体储存部分中的蒸气储存空间中的压力高于液体中的饱和蒸气压的状态喷射蒸气和惰性气体。

    CHEMICAL-ELECTROMAGNETIC HYBRID PROPELLER WITH VARIABLE SPECIFIC IMPULSE
    9.
    发明申请
    CHEMICAL-ELECTROMAGNETIC HYBRID PROPELLER WITH VARIABLE SPECIFIC IMPULSE 有权
    具有可变特定脉冲的化学电磁混合螺旋桨

    公开(公告)号：US20150107219A1

    公开(公告)日：2015-04-23

    申请号：US14403101

    申请日：2013-05-07

    申请人： Beijing Institute of Spacecraft Environment Engineering

    发明人： Hua Zhao ,  Zhong Yi ,  Yuming Liu ,  Yenan Liu ,  Lifei Meng ,  Chao Zhang ,  Qi Xiao ,  Jipeng Sun ,  Yanlin Xu

    IPC分类号： F03H1/00

    CPC分类号： F03H1/0081 ,  F02K9/42 ,  F02K9/76 ,  F02K99/00 ,  F03H1/0012 ,  F03H1/0093

    摘要： A chemical-electromagnetic hybrid propeller with variable specific impulse. Fuel gas ejected out from a spraying tube of the chemical propeller through chemical propulsion enters an ionization chamber through a first magnetic mirror tube for ionization. The fuel gas after ionization is heated up by radio-frequency ion cyclotron waves in an ion cyclotron wave heating chamber so as to improve the kinetic energy. Then a second magnetic mirror tube is used, so that ions in the fuel gas after the ionization are heated up many times in a reciprocating manner between the magnetic mirror tubes, and ejected to generate forward propulsion force. By means of the propeller, the propulsion force and the specific impulse are greatly increased.

    摘要翻译： 具有可变比冲量的化学电磁混合推进器。 通过化学推进从化学螺旋桨的喷射管喷出的燃料气体通过用于电离的第一磁镜管进入电离室。 电离后的燃料气体通过离子回旋加热室中的射频离子回旋波加热，从而提高动能。 然后使用第二磁镜管，使得电离后的燃料气体中的离子在磁镜管之间以往复方式加热多次，并被喷射以产生向前推进力。 通过螺旋桨，推进力和比冲击大大增加。

    Propulsion device with enclosed plenum
    10.
    发明授权
    Propulsion device with enclosed plenum 有权
    带封闭气室的推进装置

    公开(公告)号：US07458201B2

    公开(公告)日：2008-12-02

    申请号：US11614067

    申请日：2006-12-20

    申请人： Joseph Brady

    发明人： Joseph Brady

    IPC分类号： F02K9/66

    CPC分类号： F03H99/00 ,  F02K99/00 ,  F03G3/00 ,  Y02T50/671

    摘要： A propulsion device contains a working mass within an enclosed plenum, where the working mass is recirculated through the plenum to produce a net force vector. The working mass is accelerated around a first bend or change in direction within the plenum by a working mass driver. The temperature of the working mass is then reduced and the working mass is slowed. The working mass is then accelerated around a second bend or change in direction within the plenum resulting in two opposing force vectors. When combined, the two opposing force vectors produce a net force, and thus, acceleration of the propulsion device. The propulsion device may be used in connection with a space vehicle or satellite.

    摘要翻译： 推进装置包含在封闭的通风室内的工作质量，其中工作质量通过通风室再循环以产生净力向量。 工作质量通过工作质量驱动器围绕第一弯曲或在集气室内的方向改变。 然后，工作质量的温度降低，工作质量减慢。 然后，工作质量在第二弯曲处加速或者在集气室内的方向上改变，导致两个相反的力向量。 当组合时，两个相反的力矢量产生净力，因此产生推进装置的加速度。 推进装置可以与空间飞行器或卫星结合使用。