会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 11. 发明申请
    • Pulse detonation assembly and hybrid engine
    • 脉冲爆震装置和混合动力发动机
    • US20060254252A1
    • 2006-11-16
    • US11129686
    • 2005-05-13
    • Adam RasheedAnthony DeanChristian Vandervort
    • Adam RasheedAnthony DeanChristian Vandervort
    • F02C5/02
    • F02K7/06F02C5/00F02K7/075F23C15/00F23R7/00Y02T50/67Y02T50/672
    • A pulse detonation (PD) assembly includes a number of PD chambers adapted to expel respective detonation product streams and a number of barriers disposed between respective pairs of PD chambers. The barriers define, at least in part, a number of sectors that contain at least one PD chamber. A hybrid engine includes a number of PD chambers and barriers. The hybrid engine further includes a turbine assembly having at least one turbine stage, being in flow communication with the PD chambers and being configured to be at least partially driven by the detonation product streams. A segmented hybrid engine includes a number of PD chambers and segments configured to receive and direct the detonation product streams from respective PD chambers. The segmented hybrid engine further includes a turbine assembly configured to be at least partially driven by the detonation product streams.
    • 脉冲爆震(PD)组件包括适于排出各个爆震产物流的多个PD室和设置在各对PD室之间的多个障碍物。 这些障碍至少部分地限定了包含至少一个PD室的多个扇区。 混合动力发动机包括多个PD室和障碍物。 混合动力发动机还包括具有至少一个涡轮级的涡轮组件,其与PD室流体连通并被构造成至少部分地被爆轰产物流驱动。 分段混合动力发动机包括多个PD室和构造成接收和引导来自相应PD室的爆轰产物流的段。 分段式混合动力发动机还包括构造成至少部分地被引爆产物流驱动的涡轮组件。
    • 12. 发明授权
    • Liquid fuel injector for burners in gas turbines
    • 用于燃气轮机燃烧器的液体燃料喷射器
    • US06334309B1
    • 2002-01-01
    • US09579510
    • 2000-05-26
    • Anthony DeanLuciano MeiAlessio Miliani
    • Anthony DeanLuciano MeiAlessio Miliani
    • F23R332
    • F23R3/12F23D11/101F23R3/286
    • The present invention relates to a liquid fuel injector (10) for burners in gas turbines, of the type used inside burners which are provided with a pre-mixing chamber (62) and an element (13) to create turbulence in the flow of compressed air obtained from the compressor of the gas turbine. The injector (10) comprises a body (11) which ends in a tip (12) and is provided with at least one duct (25) for passage of the fuel, and ducts (48, 58) for the inflow of compressed air from the compressor of the turbine, wherein the duct (25) for the fuel and the ducts (48, 58) for the compressed air end in respective outlet holes. The tip (12) of the injector (10) ends at the median part of the converging portion (61) of the pre-mixing chamber (62).
    • 本发明涉及一种用于燃气轮机中的燃烧器的液体燃料喷射器(10),其在燃烧器内部使用的类型,其设置有预混合室(62)和元件(13),以在压缩流动中产生湍流 从燃气轮机的压缩机获得的空气。 喷射器(10)包括主体(11),其终止于尖端(12)并且设置有用于燃料通过的至少一个管道(25)和用于压缩空气流入的管道(48,58) 涡轮机的压缩机,其中用于燃料的管道(25)和用于压缩空气的管道(48,58)在相应的出口孔中终止。 喷射器(10)的尖端(12)在预混合室(62)的会聚部分(61)的中间部分处结束。