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    • 2. 发明公开
    • INTERNAL DETONATION ENGINE, HYBRID ENGINES INCLUDING THE SAME, AND METHODS OF MAKING AND USING THE SAME
    • 内部爆燃发动机,包括该发动机的混合动力发动机,以及制造和使用该发动机的方法
    • EP2877716A1
    • 2015-06-03
    • EP13823051.1
    • 2013-07-19
    • Lee, Brent Wei-Teh
    • Lee, Brent Wei-Teh
    • F01L7/06
    • F01L7/06F01B21/04F01L1/02F01L5/045F02B69/06F02C5/02F02C5/12F02K7/06F05B2220/302Y02T50/671
    • Hybrid internal detonation-gas turbine engines incorporating detonation or pulse engine technology (such as an internal detonation engine), and methods of manufacturing and using the same are disclosed. The internal detonation engine includes a detonation chamber having a fuel igniter therein, a stator at one end of the detonation chamber having at least a first opening to receive fuel, a rotor adjacent to the stator, and an energy transfer mechanism configured to convert energy from igniting or detonating the fuel to mechanical energy. The detonation chamber and fuel igniter are configured to ignite or detonate a fuel in the detonation chamber. Either the stator or the detonation chamber has a second opening to exhaust detonation gas(es). The rotor has one or more third openings therein configured to overlap with at least the first opening as the rotor rotates.
    • 公开了结合了爆震或脉冲发动机技术的混合式内部爆轰气体涡轮发动机(例如内部爆震发动机)以及制造和使用该发动机的方法。 内部爆震发动机包括其中具有燃料点火器的爆震室,位于爆震室一端的定子至少具有用于接收燃料的第一开口,与定子相邻的转子,以及能量传递机构, 点燃或引爆燃料为机械能。 爆震室和燃料点火器构造成点燃或引爆爆震室中的燃料。 定子或爆震室具有第二开口以排出爆炸气体。 转子在其中具有一个或多个第三开口,该第三开口构造成随着转子旋转而与至少第一开口重叠。
    • 3. 发明公开
    • ROTARY JET, POWER GENERATION SYSTEMS AND MOTORS INCLUDING THE SAME, AND METHODS OF USING THE SAME
    • 旋转射流,发电系统和包括该发动机的电动机以及使用该电动机的方法
    • EP3219907A1
    • 2017-09-20
    • EP17158934.4
    • 2017-03-02
    • Lee, Brent Wei-Teh
    • Lee, Brent Wei-Teh
    • F01D1/32F02K7/00F02C3/16
    • F02K7/005B63H2011/082F01D1/32F02C3/165Y02T50/671
    • A rotary device (e.g., a rotary jet), power generation system, and methods of using the same are disclosed. The rotary jet (100) includes a central axle or shaft (101), an inlet (105) configured to receive at least one fluid, and a plurality of radial arms (110a-d) in fluid communication with the inlet, configured to rotate around the central axle or shaft. Each radial arm has a nozzle (115a-d) at a distal end thereof and an arc between the inlet and the nozzle. The radial arms extend radially from the central axle or shaft at least in part, and are configured to rotate when the fluid enters the inlet and passes through the radial arms, or when a rotational force is applied to the central axle or shaft. Each nozzle may have an opening facing away from a direction of rotation of the radial arms or facing in a direction parallel with the central axle or shaft.
    • 公开了一种旋转装置(例如旋转喷射装置),发电系统及其使用方法。 旋转射流(100)包括中心轴或轴(101),构造成接收至少一种流体的入口(105)和与入口流体连通的多个径向臂(110a-d),构造成旋转 围绕中心轴或轴。 每个径向臂在其远端处具有喷嘴(115a-d),并且在入口与喷嘴之间具有弧形。 径向臂至少部分地从中心轴或轴径向延伸,并且构造成当流体进入入口并且穿过径向臂时或者当旋转力施加至中心轴或轴时旋转。 每个喷嘴可以具有远离径向臂的旋转方向或面向与中心轴或轴平行的方向的开口。
    • 7. 发明申请
    • ROTATING PULSE DETONATION ENGINE
    • 旋转脉冲爆震发动机
    • WO2016200698A1
    • 2016-12-15
    • PCT/US2016/035838
    • 2016-06-03
    • LEE, Brent, Wei-Teh
    • LEE, Brent, Wei-Teh
    • F01B21/04F02K7/02
    • F02K7/06F01D1/32F02C5/04F02C5/12F02K1/78F02K9/58F02K9/64F02K9/97F05D2240/35F05D2260/20F23R3/02F23R3/28Y02T50/671
    • An engine, a power generation system, and methods of manufacturing and using the same are disclosed. The engine includes a detonation/combustion chamber configured to detonate a fuel and rotate around a central rotary shaft extending from the chamber, a fuel supply inlet configured to provide the fuel to the chamber, an air supply channel configured to supply air to the chamber, at least two rotating arms extending radially from the chamber and configured to exhaust gases from detonating the fuel in the chamber and provide a rotational thrust and/or force, and a mechanical work unit configured to receive at least part of the rotational thrust and/or force. Each of the rotating arms has an exhaust nozzle at a distal end thereof, the exhaust nozzle being at or having an angle configured to provide the rotational thrust and/or force.
    • 公开了发动机,发电系统及其制造和使用方法。 引擎包括引爆/燃烧室,其被构造成引爆燃料并围绕从腔室延伸的中心旋转轴旋转;燃料供给入口,被配置为将燃料提供给腔室;空气供应通道,构造成将空气供应到腔室; 至少两个旋转臂,其从所述腔室径向延伸并且构造成排出气体以引爆所述腔室中的燃料并提供旋转推力和/或力;以及机械作业单元,其构造成容纳所述旋转推力的至少一部分和/或 力。 每个旋转臂在其远端具有排气喷嘴,排气喷嘴处于或具有构造成提供旋转推力和/或力的角度。
    • 8. 发明申请
    • INTERNAL DETONATION ENGINE, HYBRID ENGINES INCLUDING THE SAME, AND METHODS OF MAKING AND USING THE SAME
    • 内燃机,混合发动机及其制造方法及其使用方法
    • WO2014018416A1
    • 2014-01-30
    • PCT/US2013/051396
    • 2013-07-19
    • LEE, Brent, Wei-Teh
    • LEE, Brent, Wei-Teh
    • F01L7/06
    • F01L7/06F01B21/04F01L1/02F01L5/045F02B69/06F02C5/02F02C5/12F02K7/06F05B2220/302Y02T50/671
    • Hybrid internal detonation-gas turbine engines incorporating detonation or pulse engine technology (such as an internal detonation engine), and methods of manufacturing and using the same are disclosed. The internal detonation engine includes a detonation chamber having a fuel igniter therein, a stator at one end of the detonation chamber having at least a first opening to receive fuel, a rotor adjacent to the stator, and an energy transfer mechanism configured to convert energy from igniting or detonating the fuel to mechanical energy. The detonation chamber and fuel igniter are configured to ignite or detonate a fuel in the detonation chamber. Either the stator or the detonation chamber has a second opening to exhaust detonation gas(es). The rotor has one or more third openings therein configured to overlap with at least the first opening as the rotor rotates.
    • 公开了包含爆震或脉冲发动机技术的混合内爆式燃气涡轮发动机(例如内部爆震引擎)及其制造和使用方法。 内部爆震发动机包括在其中具有燃料点火器的爆炸室,在引爆室的一端处的定子至少具有用于接收燃料的第一开口,与定子相邻的转子,以及配置成将能量从 将燃料点燃或引爆到机械能。 引爆室和燃料点火器构造成点燃或引爆在引爆室中的燃料。 定子或引爆室都有一个第二个开口来排放爆震气体。 转子具有一个或多个第三开口,其中构造成在转子旋转时与至少第一开口重叠。