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    • 1. 发明授权
    • Combustion chamber for gas turbines
    • 燃气轮机燃烧室
    • US06434926B1
    • 2002-08-20
    • US09579443
    • 2000-05-26
    • Anthony DeanLuciano MeiAlessio Miliani
    • Anthony DeanLuciano MeiAlessio Miliani
    • F02C306
    • F23R3/002F23R3/10F23R2900/03044
    • A combustion chamber for gas turbines comprises an inner liner (12) and an outer liner (11), wherein the inner liner (12) is substantially concentric relative to the outer liner (11), such as to define an annular inner space (30), and wherein a shield (13) is provided at the output of each of the burners. The specific feature of the invention consists in the fact that each of the shields (13) comprises a single metal plate part, and that the liners (11, 12) have a plurality of holes (20, 21), in sections adjacent to the longitudinal development of the shield (13), such as to define gaps (60, 61) for the circulation of air.
    • 用于燃气涡轮机的燃烧室包括内衬(12)和外衬(11),其中内衬(12)相对于外衬(11)基本上是同心的,例如以限定环形内空 ),并且其中在每个燃烧器的输出处设置有屏蔽件(13)。 本发明的具体特征在于,每个屏蔽件(13)包括单个金属板部件,并且衬垫(11,12)具有多个孔(20,21),该部分邻近 屏蔽件(13)的纵向展开,以便限定用于空气循环的间隙(60,61)。
    • 2. 发明授权
    • Pre-mixing chamber for gas turbines
    • 燃气轮机预混合室
    • US06363725B1
    • 2002-04-02
    • US09662466
    • 2000-09-15
    • Luciano MeiAlessio MilianiAnthony Dean
    • Luciano MeiAlessio MilianiAnthony Dean
    • F02C7228
    • F23D14/26F23D14/76F23D17/002F23D2206/10F23D2209/20F23D2900/00015F23D2900/14021F23R3/286F23R3/343
    • A pre-mixing chamber (10) for gas turbines, wherein the gas turbine is of the type which comprises at least one compressor connected to the turbine, and a combustion chamber, wherein the combustion chamber has a converging portion (12), positioned such as to give rise to combustion inside the combustion chamber, and wherein the pre-mixing chamber (10) has a plurality of pipes (19) provided with holes (20), which open into the combustion chamber on a front portion of the body of the pre-mixing chamber (10), in order to generate a series of pilot flames, which are appropriately regulated, in order to stabilise a main flame, which is primed inside the combustion chamber, in which a front area of the converging portion (12) of the pre-mixing chamber (10) has at least one circular groove (28) provided at the holes (20) which belong to the pies (19).
    • 一种用于燃气轮机的预混合室(10),其中所述燃气涡轮机是包括连接到所述涡轮机的至少一个压缩机和燃烧室的类型,其中所述燃烧室具有会聚部分(12) 以在燃烧室内引起燃烧,并且其中所述预混合室(10)具有多个管(19),所述多个管(19)设置有孔(20),所述孔(20)在所述燃烧室的前部 预混合室(10),以便产生适当地调节的一系列引燃火焰,以便稳定在燃烧室内的主火焰(其中会聚部分的前部区域 预混合室10具有设置在属于馅饼(19)的孔(20)处的至少一个圆形凹槽(28)。
    • 3. 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。
    • 4. 发明授权
    • Method and system for efficient customized manufacture of shoes
    • 高效定制鞋子的方法和系统
    • US08595081B2
    • 2013-11-26
    • US13122705
    • 2009-09-28
    • Anthony DeanThomas BerendCiro Fusco
    • Anthony DeanThomas BerendCiro Fusco
    • G06Q30/00
    • A43B3/24G06Q10/06G06Q30/0621
    • Customized articles of footwear are produced by defining options that can be selected by a customer when submitting a custom order. These options typically include model options, functional options, and aesthetic options. These options are created by a design source, such as a shoe designer within a particular market, and presented to the customer when making the order. Upon a customer selecting one or more of the options at a user interface, the selected options are converted to specifications associated with the order. A work-load engine is employed to generate, based on the specifications, a work order that includes a dataflow for selecting appropriate stations on a manufacturing floor to participate in a manufacturing process, and a workflow for instructing each of the appropriate stations to perform a sequence of operations, within the manufacturing process, that result in fabricating individual components of the article of footwear according to the order.
    • 定制的鞋类物品是通过定义在客户提交定制订单时可以选择的选项来生成的。 这些选项通常包括模型选项,功能选项和审美选项。 这些选项由设计来源(例如特定市场中的鞋设计师)创建,并在订单时呈现给客户。 在客户选择用户界面中的一个或多个选项时,所选择的选项将转换为与订单相关的规格。 使用工作负载引擎来根据规格生成包括用于在制造车间选择合适的站参与制造过程的数据流的工作订单,以及用于指示每个适当的站执行一个 在制造过程中的操作顺序,其导致根据顺序制造鞋类物品的各个部件。
    • 10. 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。