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    • 61. 发明公开
    • Apparatus for mounting, and for maintaining running clearance in, a double entry radial compressor
    • 双重入口径向压缩机安装和维护运行间隙的装置
    • EP0161562A3
    • 1987-05-20
    • EP85105056
    • 1985-04-25
    • A. S. Kongsberg Väpenfabrikk
    • Mowill, Jan R.
    • F04D17/10F04D29/42F01D05/02F04D29/62F02C03/09F02C07/20
    • F04D29/052F02C7/20F04D29/0513F04D29/403F04D29/622F16D1/06
    • A gas generator having a double entry low pressure centrifugal compressor, a single entry high pressure centrifugal compressor and a radial inflow turbine positioned coaxially and coupled for interdependent rotation by a single shaft assembly for the double entry compressor mounted to the generator frame using a plurality of rigid hollow cross-over ducts which also carry diffused compressed air to the high pressure compressor, where the single shaft assembly uses two shaft portions connected by an expansible coupling having a helical spline torque transmitting device to allow the double entry compressor rotor to "follow" compressor housing axial position changer and to maintain a close running clearance despite thermal expansion in the structure between the low pressure (LP) and high pressure (HP) compressor portions of the gas generator.
    • 一种具有双入口低压离心压缩机,单入口高压离心压缩机和径向流入涡轮机的气体发生器,其同轴并联接,用于通过单个轴组件进行相互转动,用于安装到发电机框架上的双入口压缩机,其使用多个 刚性空心交叉管道,其还将高压压缩机承载扩散的压缩空气,其中单轴组件使用通过具有螺旋花键扭矩传递装置的可膨胀联接器连接的两个轴部分,以允许双入口压缩机转子“跟随” 压缩机壳体轴向位置更换器,并且尽管气体发生器的低压(LP)和高压(HP)压缩机部分之间的结构中的热膨胀,仍然保持紧密的运行间隙。
    • 62. 发明公开
    • Apparatus for mounting, and for maintaining running clearance in, a double entry radial compressor
    • 装置,用于建立与双入口的径向压缩机的工作周期的维持。
    • EP0161562A2
    • 1985-11-21
    • EP85105056.7
    • 1985-04-25
    • A. S. Kongsberg Väpenfabrikk
    • Mowill, Jan R.
    • F04D17/10F04D29/42F01D5/02F04D29/62F02C3/09F02C7/20
    • F04D29/052F02C7/20F04D29/0513F04D29/403F04D29/622F16D1/06
    • A gas generator having a double entry low pressure centrifugal compressor, a single entry high pressure centrifugal compressor and a radial inflow turbine positioned coaxially and coupled for interdependent rotation by a single shaft assembly for the double entry compressor mounted to the generator frame using a plurality of rigid hollow cross-over ducts which also carry diffused compressed air to the high pressure compressor, where the single shaft assembly uses two shaft portions connected by an expansible coupling having a helical spline torque transmitting device to allow the double entry compressor rotor to "follow" compressor housing axial position changer and to maintain a close running clearance despite thermal expansion in the structure between the low pressure (LP) and high pressure (HP) compressor portions of the gas generator.
    • 具有双条目低压离心式压缩机,一个单一的入口高压离心压缩机和用于使用多个安装到所述发电机框架的复式压缩机同轴地定位和连接用于相互依存的旋转运动通过一单个轴组件上的径流式涡轮机的气体发生器 刚性空心跨接管其因此携带扩散压缩空气到高压压缩机,其中,所述单轴组件使用由在具有螺旋花键的扭矩传递装置可膨胀耦合连接的两个轴部,以允许复式压缩机转子以“跟随” 压缩机壳体轴向位置开关和保持紧密的运行间隙,尽管在气体发生器的低压(LP)和高压(HP)压缩机部分之间的结构的热膨胀。
    • 67. 发明公开
    • RESILIENT BEARING MOUNT WITH INTEGRAL DAMPER FLUID PASSAGE FOR A GEARED TURBOFAN ENGINE
    • 用于齿轮涡轮增压发动机的具有整体阻尼流体通道的弹性轴承座
    • EP3284918A1
    • 2018-02-21
    • EP17185121.5
    • 2017-08-07
    • United Technologies Corporation
    • DiBENEDETTO, Enzo
    • F01D25/16F01D25/18F16C27/04F16C33/66
    • F04D29/0513F01D25/162F01D25/164F01D25/18F02C3/04F04D29/0563F04D29/059F04D29/083F04D29/668F05D2220/32F16C27/045F16C33/6637F16C33/6659F16C2360/23
    • A gas turbine engine (20) includes a bearing support ring (68) with a first annular body (124) and a second annular body (130) disposed radially inward of the first annular body (124). A radial spring (136) is connected to the first annular body (124) and the second annular body (130). The gas turbine engine (20) includes a frame (57) with a case (94) that extends around the first annular body (124). The frame (57) includes an annular member (96) connected to the case (94) and positioned radially between the radial spring (136) and the second annular body (130). A fluid port (98) extends radially through the annular member (96). A seal (70) is disposed around the annular member (96) and forward of the fluid port (98). A first fluid passage (146) extends through the case (94). A second fluid passage (148) is formed between the bearing support ring (68) and the frame (57) and extends from the first fluid passage (146) to the fluid port (98). A bearing outer race (102) is disposed inward of the second annular body (130).
    • 燃气涡轮发动机(20)包括轴承支承环(68),该轴承支承环具有设置在第一环形主体(124)的径向内侧的第一环形主体(124)和第二环形主体(130)。 径向弹簧(136)连接到第一环形体(124)和第二环形体(130)。 燃气涡轮发动机(20)包括具有围绕第一环形主体(124)延伸的壳体(94)的框架(57)。 框架(57)包括连接到壳体(94)并径向地定位在径向弹簧(136)和第二环形体(130)之间的环形构件(96)。 流体端口(98)径向延伸通过环形部件(96)。 密封件(70)设置在环形部件(96)周围并在流体口(98)的前方。 第一流体通道(146)延伸穿过壳体(94)。 第二流体通道(148)形成在轴承支撑环(68)和框架(57)之间并且从第一流体通道(146)延伸到流体端口(98)。 轴承外圈(102)设置在第二环形体(130)的内​​侧。