改进型节能单维内燃机
    1.
    发明申请

    公开(公告)号:WO2016145931A1

    公开(公告)日:2016-09-22

    申请号:PCT/CN2016/000086

    申请日:2016-02-19

    Applicant: 陈小辉

    Inventor: 陈小辉

    Abstract: 一种内燃机,包括压缩机、燃烧室(8)、管道、喷管(9)、加油器(23)、驱动装置、第一保险装置、第二保险装置、电点火装置(22)、机架、设置在机架顶部的第一支架、设置在机架上部的第二支架、设置在机架下部的第三支架和设置在机架左部的第四支架;压缩机包括内壳和外壳(18),内壳包括上压板(15)和圆筒板(19),外壳的左部的上端开有进油口(1702),外壳的右部的上端开有进气口(1701),外壳的部分底部向下凸起形成与圆筒板(19)相对应的圆筒板槽(13),圆筒板(19)可在圆筒板槽(13)内上下运动,外壳的底部的非凸起部分上开有出口(7)。这种内燃机结构简单、效率高。

    HYBRID HIGH TEMPERATURE FUEL CELL VOLUME EXPANSION HEAT ENGINE
    2.
    发明申请
    HYBRID HIGH TEMPERATURE FUEL CELL VOLUME EXPANSION HEAT ENGINE 审中-公开
    混合高温燃料电池体积膨胀热发动机

    公开(公告)号:WO02056397A2

    公开(公告)日:2002-07-18

    申请号:PCT/US0200177

    申请日:2002-01-04

    CPC classification number: H01M8/04014 H01M8/04097 H01M8/0612

    Abstract: A power plant includes a high temperature fuel cell (6), a volume expansion heat engine (11) producing mechanical energy, and a combustion chamber (9) coupled to receive from said fuel cell at least a portion of unconsumed fuel and apply high pressure combusted gases to the engine. A reformer (3) can feed fuel to said fuel cell. A distributor (8) distributes fuel cell exhaust fuel selectively to the reformer and the combustion chamber and varies the ratio of exhaust fuel fed to the reformer and combustion chamber in accordance with predetermined power desired from said fuel cell and engine.

    Abstract translation: 发电厂包括高温燃料电池(6),产生机械能的体积膨胀热机(11)和燃烧室(9),所述燃烧室联接成从所述燃料电池接收未消耗燃料的至少一部分并施加高压 燃烧的气体到发动机。 重整器(3)可以将燃料供给到所述燃料电池。 分配器(8)将燃料电池排出燃料选择性地分配到重整器和燃烧室,并根据所需燃料电池和发动机所需的预定功率改变供给重整器和燃烧室的排气燃料的比例。

    CONVERSION OF SUPERCRITICAL WATER ENERGY INTO ELECTRICAL POWER

    公开(公告)号:WO2021179018A1

    公开(公告)日:2021-09-10

    申请号:PCT/US2021/070246

    申请日:2021-03-05

    Abstract: In a general aspect, a system can include a reactor for combusting fuel and producing high-temperature, high-pressure liquid as a byproduct, and at least one vessel defining a cavity to be partially filled with water, with an air pocket within the cavity above the water. The system can further include respective valves to control admission of liquid from the reactor into the air pocket when the air pocket has a pressure lower than an operating pressure of the reactor, and to control emission of the water from the at least one vessel through of the vessel after the water in the at least one vessel has been pressurized by the liquid from the reactor. The system can also include a hydroelectric drive system for receiving water emitted from the cavity, and for converting energy in the received water into electrical energy.

    IMPROVED THRUST VECTORING IGNITION CHAMBER ENGINE WITH MULTI PURPOSE MULTI H-SLOT SCOTCH-YOKE ACTUATOR

    公开(公告)号:WO2020240583A1

    公开(公告)日:2020-12-03

    申请号:PCT/IN2020/050468

    申请日:2020-05-26

    Abstract: This patent discloses three improvements in thrust vectoring ignition chamber engine described in my indian patent 201821027867 which uses multipurpose double action scotch yoke actuator. First is substituting bilaterally operated bipartitioned slot with quad-laterally operated (quad-partitioned) H-slot in scotch yoke actuator. Second is employing multiple slots instead of single slot in the scotch yoke actuator in conjunction with appropriate modification in the operation mechanism. Third is making arrangement in the scotch yoke operation mechanism which can allow mounting of crank farther from cam gear mounted on ignition chamber without increasing the size of cam follower gear. This patent discloses four models implementing above mentioned improvements. These improvements overcome drawbacks like sideward thrust, wear due to friction, etc. prevalent in conventional scotch yoke actuator.

    THRUST VECTORED IGNITION CHAMBER ENGINE WITH TWO PHASE AXIAL FUEL SUCTION SYSTEM

    公开(公告)号:WO2020021570A1

    公开(公告)日:2020-01-30

    申请号:PCT/IN2019/050542

    申请日:2019-07-25

    Abstract: This patent discloses thrust vectoring ignition chamber engine in which ignition chamber is an annular cylinder having nozzles mounted such that during fuel suction phase they are sealed and during ignition of fuel they are unsealed so that hot jets of ignited fuel escaping through nozzles cause coupled rotatory motion on the ignition chamber. Engine uses specially designed dwell barrel cam mechanism for two phase suction and compression of fuel which facilitates the separation of fuel valve from ignition chamber. Flywheel mounted on extension of ignition chamber functions as output of the engine. Timing of electrically controlled nozzle seal and fuel valve can be adjusted so that each half rotation of flywheel completes three phases namely fuel/air suction, compression and combustion, instead of two rotations as required in engine according to prior art. This engine can give improved power boost by firing for every half revolution.

    THRUST VECTORING IGNITION CHAMBER ENGINE WITH AXIAL FUEL INTAKE SYSTEM

    公开(公告)号:WO2020021569A1

    公开(公告)日:2020-01-30

    申请号:PCT/IN2019/050541

    申请日:2019-07-25

    Abstract: This patent discloses thrust vectoring ignition chamber engine. Thrust vectoring ignition chamber used in this engine is an annular cylinder having nozzles mounted in a way such that during fuel suction phase they are sealed and during ignition of fuel they are unsealed so that hot jets of ignited fuel escaping through nozzles cause coupled rotatory motion on the ignition chamber. Engine uses specially designed dwell barrel cam mechanism for suction and compression of fuel. Flywheel mounted on extension of ignition chamber functions as output of the engine. Each half rotation of flywheel completes three phases namely fuel/air suction, compression and combustion. Thus this engine fires for every half revolution and therefore can give improved power boost.

    動作気体発生装置
    7.
    发明申请
    動作気体発生装置 审中-公开
    工作气体发生装置

    公开(公告)号:WO2013035367A1

    公开(公告)日:2013-03-14

    申请号:PCT/JP2012/059273

    申请日:2012-04-05

    Applicant: 中田 佳行

    Inventor: 中田 佳行

    Abstract: 【課題】動作気体を動力源とする動力装置に動作気体を供給する動作気体発生装置を提供する。 【解決手段】本発明の動作気体発生装置は、動作気体を動力源とする装置に動作気体を供給するための装置であって、シリンダヘッドと、シリンダとハウジングケースとから成るシリンダブロックと、ピストンとコンロッドと回転ローターとから成るクランク伝達機構で構成され、ピストンとコンロッドと回転ローターの連結位置と、回転ローターの軸芯位置が上死点付近で直線状となる位置から膨張行程側に10~25度進角した位置で点火し、燃焼室形成(圧縮)工程と、点火工程と、爆発・膨張行程と、掃気工程とを、ピストンが一往復サイクルで完了する構成とした手段を採る。

    Abstract translation: 提供一种将工作气体供给到具有作业气体的动力单元作为动力源的工作气体发生装置。 该工作气体发生装置用于将工作气体供给到作为动力源的工作气体的装置由气缸盖,从缸体和壳体获得的气缸体以及获得的曲柄传动机构构成, 从活塞,连杆和旋转转子。 该装置在膨胀行程一侧的10-25°点火提前位置从靠近上止点的位置点燃,其中活塞,连杆和旋转转子的连接位置和转动转子轴线的位置形成直线 线。 该装置使用一种构造成使得活塞在单个往复循环中完成燃烧室成形(压缩)过程,点火过程,爆炸/膨胀过程和清除过程的装置。

    GAS TURBINE ENGINE AND PULSE DETONATION COMBUSTION SYSTEM
    8.
    发明申请
    GAS TURBINE ENGINE AND PULSE DETONATION COMBUSTION SYSTEM 审中-公开
    气体涡轮发动机和脉冲爆震燃烧系统

    公开(公告)号:WO2012092285A1

    公开(公告)日:2012-07-05

    申请号:PCT/US2011/067406

    申请日:2011-12-27

    Abstract: One embodiment of the present invention is a unique pulse detonation combustion system. Another embodiment is a unique gas turbine engine. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for pulse detonation combustion systems, gas turbine engines, and other machines and engines. Further embodiments, forms, features, aspects, benefits, and advantages of the present application shall become apparent from the description and figures provided herewith.

    Abstract translation: 本发明的一个实施例是独特的脉冲爆震燃烧系统。 另一个实施例是独特的燃气涡轮发动机。 其他实施例包括用于脉冲爆燃燃烧系统,燃气涡轮发动机和其它机器和发动机的装置,系统,装置,硬件,方法和组合。 本申请的其他实施例,形式,特征,方面,益处和优点将从本文提供的描述和图中变得显而易见。

    REACTION CHAMBER FOR SUPERCRITICAL WATER OXIDATION REACTOR

    公开(公告)号:WO2021243346A2

    公开(公告)日:2021-12-02

    申请号:PCT/US2021/070245

    申请日:2021-03-05

    Abstract: Fuel mixed in water is combusted in a reactor having an internal operating pressure and temperature greater than 3200 psi and greater than 374°C, where the combustion of the fuel is exothermic. Air and fuel are pressurized for introduction into the reactor to a pressure greater than the internal operating pressure using energy generated from the combustion of the fuel, and the pressurized air and the pressurized fuel are injected into the reactor. Pressurized water from the reactor is injected into a drive water column that is partially filled with water to increase a pressure of the drive water column, and water at a temperature less than 100°C is injected into the reactor to replace water from the reactor that is injected into the drive water column. Pressurized water from the drive water column is used to drive a hydroelectric drive system to produce electrical power.

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