TUBULAR ELASTOMER DAMPER
    141.
    发明申请
    TUBULAR ELASTOMER DAMPER 审中-公开
    管状弹性阻尼器

    公开(公告)号:WO1994015113A1

    公开(公告)日:1994-07-07

    申请号:PCT/US1993009934

    申请日:1993-10-18

    CPC classification number: B64C27/51 F16F1/379 F16F1/38

    Abstract: A tubular elastomer damper (11) has a central shaft (12) disposed within a housing (13) and surrounded by an elastomer member (14). Uniform strain is provided across the elastomer disposed between the central shaft and the housing by either tapering the length of the elastomer from an inner bonding surface (15) to an outer bonding surface (16) such that the radius times the length at each point along the elastomer is equal or by providing a first elastomer layer (28) adjacent the shaft (26) having a high fatigue strain/lower damping ability, a second elastomer layer (29) adjacent the housing (27) having a low strain higher damping ability and an intermediate elastomer layer (30) of moderate strain and damping therebetween such that from the inner to the outer radius of the elastomer member, uniform strain is achieved. By providing uniform strain from the inner to the outer radius of the tubular elastomer damper, temperature increases due to localized high strains are avoided which are detrimental to damper performance. Optionally, axial cooling passages are provided within the elastomer member to dissipate heat to assure operation within design parameters, thus extending the life of the tubular elastomer damper.

    Abstract translation: 管状弹性体阻尼器(11)具有设置在壳体(13)内并由弹性体构件(14)包围的中心轴(12)。 通过将弹性体的长度从内部接合表面(15)逐渐缩小到外部接合表面(16),使得半径乘以在每个点沿着的长度,均匀的应变被设置在设置在中心轴和壳体之间的弹性体上 弹性体相等或通过提供具有高疲劳应变/较低阻尼能力的相邻于轴(26)的第一弹性体层(28),邻近壳体(27)的第二弹性体层(29)具有低应变较高阻尼能力 以及中间弹性体层(30),其间具有适度的应变和阻尼,使得从弹性体构件的内径到外半径获得均匀的应变。 通过从管状弹性体阻尼器的内半径到外半径提供均匀的应变,避免了由于局部高应变引起的温度升高,这对阻尼器性能是不利的。 可选地,轴向冷却通道设置在弹性体构件内以散发热量以确保在设计参数内操作,从而延长管状弹性体阻尼器的寿命。

    GAS TURBINE BLADE SEAL
    145.
    发明申请
    GAS TURBINE BLADE SEAL 审中-公开
    气体涡轮叶片密封

    公开(公告)号:WO1994012772A1

    公开(公告)日:1994-06-09

    申请号:PCT/US1993010682

    申请日:1993-11-04

    CPC classification number: F01D11/006 F01D5/22 Y10S416/50

    Abstract: An underplatform damper (52) contact portion (54) is rigid, and provides a loose seal between the underplatform cooling air (36) and the gas stream (40). At the aft end of the blade platform the pressure difference increases and a more effective seal is provided by a snap-in flexible seal (72).

    Abstract translation: 底板式阻尼器(52)接触部分(54)是刚性的,并且在底板冷却空气(36)和气流(40)之间提供松散的密封。 在叶片平台的后端,压力差增加,并且通过卡入式柔性密封件(72)提供更有效的密封。

    ROTOR BLADE WITH COOLED INTEGRAL PLATFORM
    147.
    发明申请
    ROTOR BLADE WITH COOLED INTEGRAL PLATFORM 审中-公开
    具有冷却整体平台的转子叶片

    公开(公告)号:WO1994012765A1

    公开(公告)日:1994-06-09

    申请号:PCT/US1993010937

    申请日:1993-11-12

    CPC classification number: F01D5/18 F01D5/145 F05D2240/81 F05D2260/202

    Abstract: A rotor blade (28) having a cooled integral platform (34) is disclosed. Various construction details are developed which disclose a rotor blade (28) platform (34) having a first cooling hole (56) for directing rotor blade core cooling fluid over a first portion of the platform and a second cooling hole (58) for directing under-platform cavity cooling fluid over a second portion of the platform (34). In a particular embodiment, a rotor blade (28) platform (34) includes a plurality of first cooling holes (56) and a plurality of second cooling holes (58). The first cooling holes (56) extend between a core cooling passage within the blade (28) and the platform (34) outer surface (52). The second cooling holes (58) extend between a damper cavity (62) and the platform (34) outer surface (52). Both sets of cooling holes (56, 58) are oriented to direct a film of cooling fluid over the platform (34) outer surface (52) and individual cooling holes (56, 58) are aligned which flow streamlines of an interblade vortices to encourage the development of a film of cooling fluid.

    Abstract translation: 公开了一种具有冷却的一体式平台(34)的转子叶片(28)。 公开了具有第一冷却孔(56)的转子叶片(28)平台(34)的各种结构细节,所述第一冷却孔用于将转子叶片芯冷却流体引导到所述平台的第一部分上;以及第二冷却孔(58) 平台腔冷却流体在平台(34)的第二部分上。 在特定实施例中,转子叶片(28)平台(34)包括多个第一冷却孔(56)和多个第二冷却孔(58)。 第一冷却孔(56)在叶片(28)内的芯冷却通道和平台(34)外表面(52)之间延伸。 第二冷却孔(58)在阻尼腔(62)和平台(34)外表面(52)之间延伸。 这两组冷却孔(56,58)被定向成将冷却流体膜引导到平台(34)外表面(52)上,并且各个冷却孔(56,58)对准,从而促使叶片间旋涡流动,从而鼓励 开发冷却液膜。

    AUGMENTOR FLAME HOLDER CONSTRUCTION
    148.
    发明申请
    AUGMENTOR FLAME HOLDER CONSTRUCTION 审中-公开
    AUGMENTOR火焰架构造

    公开(公告)号:WO1994010436A1

    公开(公告)日:1994-05-11

    申请号:PCT/US1992009092

    申请日:1992-10-27

    CPC classification number: F23R3/20

    Abstract: Shrouds (22, 24) are welded to support braces (20) near fuel spray ring (12). A splash shield (30) is secured to shroud (22) toward which fuel (16) is sprayed. It extends between braces protecting the shroud (22) from fuel impingement. Cracking of the structure at the shroud-brace interface is avoided.

    Abstract translation: 护罩(22,24)被焊接到燃料喷雾环(12)附近的支撑支架(20)。 防溅罩(30)固定到喷射燃料(16)的罩(22)上。 它在保护罩(22)免受燃料冲击的支架之间延伸。 避免了在护罩 - 支撑接口处的结构的破裂。

    CERAMIC COMPOSITE COATING MATERIAL
    149.
    发明申请
    CERAMIC COMPOSITE COATING MATERIAL 审中-公开
    陶瓷复合涂料

    公开(公告)号:WO1994008069A1

    公开(公告)日:1994-04-14

    申请号:PCT/US1993009038

    申请日:1993-09-23

    Abstract: A ceramic coating for a metal article includes a metallic bond coat deposited on the metal article, at least one MCrAlY/ceramic layer deposited on the bond coat, and a ceramic composite top layer deposited on the MCrAlY/ceramic layer. The M in MCrAlY stands for Fe, Ni, Co, or a mixture of Ni and Co. The ceramic in the MCrAlY/ceramic layer comprises mullite, alumina, zircon, silimanite, sodium zirconium phosphate, fused silica, cordierite, aluminum titanate, or zirconia. The ceramic composite top layer comprises a ceramic matrix and at least one secondary phase. A method of making the coating includes sequentially depositing a metallic bond coat on the metal article, at least one MCrAlY/ceramic layer on the bond coat, and a ceramic composite top layer on the MCrAlY/ceramic layer.

    Abstract translation: 用于金属制品的陶瓷涂层包括沉积在金属制品上的金属粘结涂层,沉积在粘合涂层上的至少一个MCrAlY /陶瓷层和沉积在MCrAlY /陶瓷层上的陶瓷复合顶层。 MCrAlY中的M代表Fe,Ni,Co或Ni和Co的混合物。MCrAlY /陶瓷层中的陶瓷包括莫来石,氧化铝,锆石,硅锰矿,磷酸锆钠,熔融石英,堇青石,钛酸铝或 氧化锆。 陶瓷复合顶层包括陶瓷基体和至少一个第二相。 制备涂层的方法包括在金属制品上依次沉积金属粘结涂层,在粘合涂层上至少一个MCrAlY /陶瓷层和MCrAlY /陶瓷层上的陶瓷复合顶层。

    METHOD FOR REMOVAL OF ABRADABLE MATERIAL FROM GAS TURBINE ENGINE AIRSEALS
    150.
    发明申请
    METHOD FOR REMOVAL OF ABRADABLE MATERIAL FROM GAS TURBINE ENGINE AIRSEALS 审中-公开
    从气体涡轮发动机空调中去除不可磨损材料的方法

    公开(公告)号:WO1994002287A1

    公开(公告)日:1994-02-03

    申请号:PCT/US1993006457

    申请日:1993-07-08

    Abstract: A method for removing a predetermined amount of material from the inner surface (16, 18, 20, 22) of a circular article (10) which deviates from a true circular configuration. The outer surface (32) of the article (10) is touch probed to determine its true location in space, data are then compared to engineering design data to establish the location of the surface (16, 18, 20, 22) to which material removal is desired. A control computer (70) sends commands to the machine control system, causing the machine to remove the excess material down to the desired dimension. Any deviations from circular are compensated for by moving the article (10) radially relative to the cutting tool as the article (10) moves circumferentially relative to the cutting tool.

    Abstract translation: 一种用于从圆形物品(10)的内表面(16,18,20,22)去除预定量的材料的方法,其偏离真正的圆形构造。 物品(10)的外表面(32)被探测以确定其在空间中的真实位置,然后将数据与工程设计数据进行比较,以确定表面(16,18,20,22)的位置,物料 需要移除。 控制计算机(70)向机器控制系统发送命令,使得机器将多余的材料移除到所需的尺寸。 当制品(10)相对于切割工具周向移动时,通过相对于切割工具径向地移动物品(10)来补偿任何与圆形的偏差。

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