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    • 1. 发明授权
    • Hot forming process
    • 热成型工艺
    • US5694683A
    • 1997-12-09
    • US49533
    • 1993-04-20
    • J. Michael TeetsDouglas R. Burnham
    • J. Michael TeetsDouglas R. Burnham
    • B21K3/04B23P15/04F01D5/28B23P15/00
    • B21D53/78B21K3/04B23P15/04F01D5/288F04D29/324F05D2240/303Y10T29/49336Y10T29/49341
    • A process is provided for forming a metallic edge having a three dimensional internal configuration by preparing a metallic edge blank having a two dimensional internal configuration; attaching a flange to the sides of the blank; preheating the blank, forming mandrel and receiver dies to a temperature at which the metal is in a malleable state, with the forming mandrel having an external surface which corresponds to the three dimensional internal configuration of the formed metallic edge; and hot forming the metallic edge by securing the blank within the receiver dies and advancing the mandrel into the inner cavity of the blank through use of a drive means which rotates the mandrel as it advances into the blank while maintaining the blank, mandrel and receiver dies at the malleable temperature.
    • 提供一种通过制备具有二维内部构造的金属边缘坯料来形成具有三维内部构造的金属边缘的方法; 将凸缘附接到坯件的侧面; 预热坯料,将芯棒和接收器模具成形为金属处于可延展状态的温度,成形心轴具有对应于形成的金属边缘的三维内部构造的外表面; 并且通过将所述坯件固定在所述接收器模具内并且通过使用驱动装置将所述心轴推进到所述坯料的内部空腔中而热成型所述金属边缘,所述驱动装置使得当所述心轴进入所述坯件时旋转所述心轴,同时保持所述坯料, 在可塑的温度下。
    • 2. 发明授权
    • Turbine engine with combustor premix system
    • 具有燃烧器预混系统的涡轮发动机
    • US4429527A
    • 1984-02-07
    • US275157
    • 1981-06-19
    • J. Michael Teets
    • J. Michael Teets
    • F23R3/38F02C7/224
    • F23R3/38
    • A turbine engine having a combustor premix system for mixing fuel and air to provide increased efficiency by reducing temperature peaks in the combustor. The system includes a primary mixing chamber for mixing compressed air and atomized fuel and a secondary mixing chamber located between the primary mixing chamber and the combustor for mixing additional compressed air to the fuel-air mixture. The secondary mixing chamber comprises a plurality of tubes with air metering ports in the walls thereof and a control assembly to vary the air flow to the ports for off design engine operating conditions, and optimizes fuel-air mixtures for the combustor at all engine operating speeds improving fuel economy and exhaust pollution control. The primary mixing chamber is located adjacent to and between the compressor for the air and the combustor so that the fuel-air mixture flowing therethrough tends to cool the compressor and the chamber itself shields the compressor from radiant heat from the combustor.
    • 一种涡轮发动机,其具有用于混合燃料和空气的燃烧器预混物系统,以通过降低燃烧器中的温度峰值来提高效率。 该系统包括用于混合压缩空气和雾化燃料的主混合室和位于主混合室和燃烧器之间的二次混合室,用于将额外的压缩空气与燃料 - 空气混合物混合。 二次混合室包括在其壁中具有空气计量端口的多个管和控制组件,用于改变用于设计发动机运行条件的端口的空气流,并且在所有发动机运转速度下优化用于燃烧器的燃料 - 空气混合物 改善燃油经济性和废气污染控制。 主混合室位于空气与燃烧器附近并位于压缩机之间,使得流过其中的燃料 - 空气混合物倾向于冷却压缩机,并且室本身屏蔽压缩机免受来自燃烧器的辐射热。
    • 10. 发明授权
    • Atomizer for a combustor
    • 用于燃烧器的雾化器
    • US06698208B2
    • 2004-03-02
    • US10017917
    • 2001-12-14
    • J. Michael Teets
    • J. Michael Teets
    • F02C722
    • F23R3/28F05B2250/15F23D11/107F23R3/50
    • An atomizer for use with a combustor in a gas turbine has a body with a fuel passageway extending through the center of the body. A plurality of channels extends within the body about the passageway centerline, and are oriented along a circumferential angle about the passageway centerline to deliver air at the discharge end of the passageway with an axially whirling motion. The channels are simultaneously oriented along an axial angle about the passageway centerline, thereby directing the flow of air to converge toward the passageway centerline, mix with the fuel, and then at least in part diverge from the passageway centerline. The whirling air intersects with the fuel at the exit of the nozzle to effectively atomize both the air and fuel thereby providing a homogeneous air/fuel mixture to the combustion chamber.
    • 用于燃气轮机中的燃烧器的雾化器具有主体,其具有延伸穿过主体中心的燃料通道。 多个通道在主体内围绕通道中心线延伸,并且沿着围绕通道中心线的圆周角度定向,以在轴向排出端部处以轴向旋转运动输送空气。 通道同时沿着围绕通道中心线的轴向定向,从而引导空气流朝向通道中心线会聚,与燃料混合,然后至少部分地离开通道中心线。 旋转空气与喷嘴出口处的燃料相交,以有效地雾化空气和燃料,从而为燃烧室提供均匀的空气/燃料混合物。