Fuel injection device
    35.
    发明授权

    公开(公告)号:US10648671B2

    公开(公告)日:2020-05-12

    申请号:US15435680

    申请日:2017-02-17

    Abstract: A fuel injection device for a gas turbine combustor includes: a pilot fuel injector; a main fuel injector; a plurality of main fuel injection holes arranged in the main fuel injector to inject the fuel rearward; a main fuel injection nozzle to guide the fuel to a main air passage, protruding rearward from a circumference of the main fuel injection hole into the opening formed in a passage wall that forms the main air passage; a heat-shielding casing covering the main fuel injector; and a ring member interposed in an axial gap between the passage wall and the heat-shielding casing. The ring member covers a through-hole gap between the main fuel injection nozzle and a through-hole in the heat-shielding casing, and has a purge passage communicated with the opening to introduce air into the main air passage.

    ADJUSTING METHOD AND ADJUSTING SYSTEM FOR RESONANCE FREQUENCY OF VIBRATION ISOLATOR, VIBRATION ISOLATOR, AND DESIGNING METHOD, DESIGNING SYSTEM, AND MANUFACTURING METHOD FOR VIBRATION ISOLATOR

    公开(公告)号:US20190170209A1

    公开(公告)日:2019-06-06

    申请号:US16321002

    申请日:2017-07-25

    Abstract: Provided is an adjusting method for a resonance frequency of a vibration isolator, the vibration isolator including first to n-th elastic member groups and/or an n+1-th elastic member group, the first to n-th elastic member groups and/or the n+1-th elastic member group being located on an xy plane of an xyz coordinate system, and an xy coordinate system of the xyz coordinate system being a coordinate system obtained by, when a tensor of inertia I with respect to an XYZ coordinate system having an origin in a center of gravity of a vibration sensing side structure or a vibration source side structure is represented as I, rotating an XY coordinate system by θ=tan−1(2IXY/(IXX−IYY)) around a Z axis, the adjusting method including, when rigidity Ki of the first to n-th elastic member groups is represented as [ K i ] = [ k i  _  xx 0 0 0 k i  _  yy 0 0 0 k i  _  zz ] , rigidity Kn+1 of the n+1-th elastic member group is represented as [ K n + 1 ] = [ k n + 1  _  xx 0 0 0 k n + 1  _  yy 0 0 0 k n + 1  _  zz ] , and an x coordinate and a y coordinate of the first to n-th elastic member groups are represented as rpi_x and rpi_y, while satisfying Σki_xxrpi_x=Σki_yyrpi_y=0 and Σki_yyrpi_xrpi_y=Σki_xxrpi_xrpi_y=0, at least one step of a step of adjusting positions of the first to n-th elastic member groups such that values of Σ(ki_zzrpi_y2), Σ(ki_yyrpi_x2), and Σ(ki_zzrpi_y2+ki_yyrpi_x2) change and respectively shifting resonance frequencies of x, y, and z-axial rotational motions and a step of arranging the n+1-th elastic member group at an origin of the xyz coordinate, adjusting values of kn+1_xx, kn+1_yy, and kn+1_zz, and respectively shifting resonance frequencies of x, y, and z-direction translational motions.

    JET SYSTEM
    37.
    发明申请
    JET SYSTEM 审中-公开

    公开(公告)号:US20170276093A1

    公开(公告)日:2017-09-28

    申请号:US15466123

    申请日:2017-03-22

    CPC classification number: F02K9/56

    Abstract: Provided is a jet system capable of regulating a pressure of a jet substance without using any high-pressure gas supply subsystem. In a storage section for storing therein a jet substance such as fuel or oxidizer, a pressurizing substance such as liquefied gas is stored in addition to the jet substance, to enable the jet substance to be supplied from the storage section according to pressurization from the pressurizing substance. A jet operation is performed while an internal pressure of the storage section lowered along with discharge of the jet substance therefrom is at least partially recovered by at least a part of the pressurizing substance vaporized in the storage section.

    VAPOR JET SYSTEM
    39.
    发明申请
    VAPOR JET SYSTEM 审中-公开
    蒸汽喷射系统

    公开(公告)号:US20170036784A1

    公开(公告)日:2017-02-09

    申请号:US15304037

    申请日:2015-04-16

    Abstract: A vapor jet system includes a container for storing a sublimable solid, the container having a vapor discharge port for discharging vapor generated by sublimation of the sublimable solid; a member having an opening for jetting out the vapor to the outside of the vapor jet system; a vapor flow path between the vapor discharge port and the opening; and a filter for preventing passage of the sublimable solid and allowing the vapor to pass through, the filter being provided to the vapor flow path.

    Abstract translation: 蒸汽喷射系统包括用于储存可升华的固体的容器,该容器具有用于排出由升华性固体升华产生的蒸气的蒸汽排放口; 具有用于将蒸汽喷射到蒸气喷射系统的外部的开口的构件; 蒸气排出口与开口之间的蒸气流路; 以及用于防止可升华固体通过并允许蒸汽通过的过滤器,所述过滤器设置在蒸汽流动路径上。

    SYSTEM FOR FEEDING HIGH-FREQUENCY WAVES TO DEPLOYMENT STRUCTURE
    40.
    发明申请
    SYSTEM FOR FEEDING HIGH-FREQUENCY WAVES TO DEPLOYMENT STRUCTURE 审中-公开
    将高频波送到部署结构的系统

    公开(公告)号:US20160218408A1

    公开(公告)日:2016-07-28

    申请号:US14900048

    申请日:2014-06-19

    Abstract: Provided is a high-frequency wave feeding system capable of feeding microwaves with little loss and without addition of resistive noise, using a simple deployment mechanism. The system includes a first waveguide fixed to a first structure of a deployment structure and having a choke flange, and a second waveguide fixed to a second structure of the deployment structure and having a cover flange. When the deployment structure is in a deployed state, the choke flange and the cover flange face each other so that high-frequency waves are fed to the deployment structure via the first and second waveguides.

    Abstract translation: 提供了一种能够使用简单的部署机制来馈送微波损耗小且不增加电阻噪声的高频馈波系统。 该系统包括固定到展开结构的第一结构并具有扼流圈法兰的第一波导和固定到展开结构的第二结构并具有盖凸缘的第二波导。 当展开结构处于展开状态时,扼流器法兰和盖凸缘彼此面对,从而使高频波经由第一和第二波导馈送到展开结构。

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