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    Augmenter For Compound Compression Engine
    1.
    发明申请
    Augmenter For Compound Compression Engine 有权
    复合压缩发动机增压器

    公开(公告)号：US20100269782A1

    公开(公告)日：2010-10-28

    申请号：US12830604

    申请日：2010-07-06

    Applicant: Alan B. Minick ,  Alfred Little

    Inventor： Alan B. Minick ,  Alfred Little

    IPC: F02B53/10

    CPC classification number: F02B53/00 ,  F01C1/22 ,  F01C11/004 ,  F02B41/06 ,  Y02T10/17

    Abstract: A rotary engine has a first rotary unit and a second rotary unit. The first rotary unit has a chamber containing a remaining compressed air charge. After combustion in the second rotary unit, the resulting second unit exhaust is in fluid communication with said remaining compressed air charge via a second passageway. An injector is in fluid communication with said remaining compressed air charge in the first rotary unit. The injector injects fuel into the mixture containing the remaining compressed air charge in the first rotary engine and the second unit exhaust from the second rotary engine. This mixture is combusted either with a spark or via auto (diesel) ignition. In this way, the engine produces additional useful work by combusting the remaining compressed air charge and additional fuel. Alternatively, the injector described in the first rotary unit may be located in the second passageway. The injector in the first rotary unit or in the second passageway may be selectively activated throughout the engine's mission.

    Abstract translation: 旋转发动机具有第一旋转单元和第二旋转单元。 第一旋转单元具有包含剩余压缩空气装料的室。 在第二旋转单元燃烧之后，所得到的第二单元排气通过第二通道与所述剩余的压缩空气进料流体连通。 喷射器与第一旋转单元中的所述剩余压缩空气进料流体连通。 喷射器将燃料喷入含有第一旋转发动机中剩余的压缩空气的混合物和来自第二旋转发动机的第二单元排气的混合物中。 该混合物通过火花或汽油（柴油）点火燃烧。 以这种方式，发动机通过燃烧剩余的压缩空气装料和附加燃料来产生额外的有用功。 或者，第一旋转单元中描述的喷射器可以位于第二通道中。 在整个发动机的使命中，可以选择性地启动第一旋转单元或第二通道中的喷射器。

    Augmenter for compound compression engine
    2.
    发明授权
    Augmenter for compound compression engine 有权
    复合压缩发动机增压器

    公开(公告)号：US08839761B2

    公开(公告)日：2014-09-23

    申请号：US12830604

    申请日：2010-07-06

    Applicant: Alan B. Minick ,  Alfred Little

    Inventor： Alan B. Minick ,  Alfred Little

    IPC: F02B53/08 ,  F02B53/04 ,  F02B53/00 ,  F02B41/06 ,  F01C11/00 ,  F01C1/22

    CPC classification number: F02B53/00 ,  F01C1/22 ,  F01C11/004 ,  F02B41/06 ,  Y02T10/17

    Abstract: A rotary engine includes a first rotary unit operable to provides a first phase of compression to a fresh air charge drawn in through an inlet port to the first rotary unit. A second rotary unit in communication with the first rotary unit through a first passage, the second rotary unit operable to provide a second phase of compression to the first phase of compression, a combustion phase and a first phase of expansion, the second rotary unit in communication with the first rotary unit through a second passage such that the first rotary unit provides a second phase of expansion to the first phase of expansion and an exhaust phase that exhausts the first rotary unit via an exhaust port. A first fuel injector is in communication with the second rotary unit operable to initiate the combustion phase and a second fuel injector is in communication with the first rotary unit operable to selectively initiate augmented operation.

    Abstract translation: 旋转发动机包括第一旋转单元，其可操作以将第一相压缩提供给通过第一旋转单元的入口吸入的新鲜空气。 第二旋转单元，其通过第一通道与第一旋转单元连通，第二旋转单元可操作以向第一压缩阶段，燃烧阶段和第一膨胀阶段提供第二压缩阶段，第二旋转单元 通过第二通道与第一旋转单元连通，使得第一旋转单元向第一膨胀阶段提供第二膨胀阶段，以及通过排气口排出第一旋转单元的排气相。 第一燃料喷射器与可操作以启动燃烧阶段的第二旋转单元连通，并且第二燃料喷射器与第一旋转单元连通，可操作以选择性地启动增强操作。

    COMPRESSED GASEOUS OXIDIZER ENERGY STORAGE SYSTEM
    4.
    发明申请
    COMPRESSED GASEOUS OXIDIZER ENERGY STORAGE SYSTEM 审中-公开
    压缩式气体氧化剂能源储存系统

    公开(公告)号：US20110195368A1

    公开(公告)日：2011-08-11

    申请号：US12702251

    申请日：2010-02-08

    Applicant: Alfred Little

    Inventor： Alfred Little

    IPC: F23Q11/00

    CPC classification number: F02C6/16 ,  F03D9/17 ,  Y02E10/72 ,  Y02E60/15

    Abstract: A compressed gaseous oxidizer energy storage (COES) system includes a catalyst system in communication with a compressed gaseous oxidizer storage system and a compressed gas fuel storage system.

    Abstract translation: 压缩气体氧化器能量储存（COES）系统包括与压缩气体氧化剂储存系统和压缩气体燃料储存系统连通的催化剂系统。

    Launch abort and orbital maneuver system
    6.
    发明授权
    Launch abort and orbital maneuver system 有权
    发射中止和轨道机动系统

    公开(公告)号：US08727283B2

    公开(公告)日：2014-05-20

    申请号：US13154873

    申请日：2011-06-07

    Applicant: Dennis E. Morris ,  Alfred Little

    Inventor： Dennis E. Morris ,  Alfred Little

    IPC: B64G1/40

    CPC classification number: B64G1/40 ,  B64G1/002 ,  B64G1/12 ,  B64G1/62

    Abstract: A spacecraft includes a first engine configured to provide primary launch abort thrust and a second engine disposed radially from a center of gravity, the second engine configured to provide a secondary launch abort thrust, a primary orbital maneuvering thrust, and a primary control thrust.

    Abstract translation: 航天器包括被配置为提供主要发射中止推力的第一引擎和从重心径向设置的第二引擎，所述第二引擎被配置为提供次级发射中止推力，主轨道机动推力和主控制推力。

    LAUNCH ABORT AND ORBITAL MANEUVER SYSTEM
    7.
    发明申请
    LAUNCH ABORT AND ORBITAL MANEUVER SYSTEM 有权
    发起人和ORBITAL MANEUVER系统

    公开(公告)号：US20120312927A1

    公开(公告)日：2012-12-13

    申请号：US13154873

    申请日：2011-06-07

    Applicant: Dennis E. Morris ,  Alfred Little

    Inventor： Dennis E. Morris ,  Alfred Little

    IPC: B64G1/40

    CPC classification number: B64G1/40 ,  B64G1/002 ,  B64G1/12 ,  B64G1/62

    Abstract: A spacecraft includes a first engine configured to provide primary launch abort thrust and a second engine disposed radially from a center of gravity, the second engine configured to provide a secondary launch abort thrust, a primary orbital maneuvering thrust, and a primary control thrust.

    Abstract translation: 航天器包括被配置为提供主要发射中止推力的第一引擎和从重心径向设置的第二引擎，所述第二引擎被配置为提供次级发射中止推力，主轨道机动推力和主控制推力。

    Catalyzed hot gas heating system for concentrated solar power generation systems
    8.
    发明授权
    Catalyzed hot gas heating system for concentrated solar power generation systems 有权
    用于集中太阳能发电系统的催化燃气加热系统

    公开(公告)号：US07987844B2

    公开(公告)日：2011-08-02

    申请号：US12319894

    申请日：2009-01-13

    Applicant: Andrew J. Zillmer ,  Alfred Little

    Inventor： Andrew J. Zillmer ,  Alfred Little

    IPC: F24J2/42

    CPC classification number: F16L9/19 ,  F16L9/18 ,  F16L53/32 ,  F16L59/143 ,  F24S20/20 ,  F24S80/20 ,  F24S90/00 ,  F28D2020/0047 ,  Y02E10/46

    Abstract: A solar power generation system includes a fluid housing, a solar collector, and a heating system. The fluid housing contains a heat transfer medium. The solar collector concentrates solar energy onto the heat transfer medium. The heating system includes at least one gas tank containing a gas and fluidically connected to a first catalyst. The first catalyst is configured to catalyze gas from the gas tank to create hot gas. The heating system also includes a first hot gas pipe fluidically connected to the first catalyst and positioned with respect to the fluid housing such that hot gas flowing through the first hot gas pipe comes into thermal contact with the heat transfer medium within the fluid housing.

    Abstract translation: 太阳能发电系统包括流体外壳，太阳能收集器和加热系统。 流体壳体包含传热介质。 太阳能收集器将太阳能集中在传热介质上。 加热系统包括至少一个含有气体并与第一催化剂流体连接的气罐。 第一催化剂被配置为催化来自气罐的气体以产生热气体。 加热系统还包括流体连接到第一催化剂并相对于流体壳体定位的第一热气管，使得流过第一热气管的热气体与流体壳体内的传热介质热接触。

    Catalyzed hot gas heating system for concentrated solar power generation systems
    9.
    发明申请
    Catalyzed hot gas heating system for concentrated solar power generation systems 有权
    用于集中太阳能发电系统的催化燃气加热系统

    公开(公告)号：US20100175687A1

    公开(公告)日：2010-07-15

    申请号：US12319894

    申请日：2009-01-13

    Applicant: Andrew J. Zillmer ,  Alfred Little

    Inventor： Andrew J. Zillmer ,  Alfred Little

    IPC: F24J2/46 ,  F24J2/04 ,  F03G6/00

    CPC classification number: F16L9/19 ,  F16L9/18 ,  F16L53/32 ,  F16L59/143 ,  F24S20/20 ,  F24S80/20 ,  F24S90/00 ,  F28D2020/0047 ,  Y02E10/46

    Abstract: A solar power generation system includes a fluid housing, a solar collector, and a heating system. The fluid housing contains a heat transfer medium. The solar collector concentrates solar energy onto the heat transfer medium. The heating system includes at least one gas tank containing a gas and fluidically connected to a first catalyst. The first catalyst is configured to catalyze gas from the gas tank to create hot gas. The heating system also includes a first hot gas pipe fluidically connected to the first catalyst and positioned with respect to the fluid housing such that hot gas flowing through the first hot gas pipe comes into thermal contact with the heat transfer medium within the fluid housing.

    Abstract translation: 太阳能发电系统包括流体外壳，太阳能收集器和加热系统。 流体壳体包含传热介质。 太阳能收集器将太阳能集中在传热介质上。 加热系统包括至少一个含有气体并与第一催化剂流体连接的气罐。 第一催化剂被配置为催化来自气罐的气体以产生热气体。 加热系统还包括流体连接到第一催化剂并相对于流体壳体定位的第一热气管，使得流过第一热气管的热气体与流体壳体内的传热介质热接触。

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