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    • 6. 发明公开
    • LIFTING TOOL FOR ROTARY SHAFT AND LIFTING METHOD FOR ROTARY SHAFT
    • 设备起重起重旋转轴的旋转轴和方法
    • EP3009617A4
    • 2017-02-15
    • EP14810235
    • 2014-06-09
    • MITSUBISHI HITACHI POWER SYS
    • YAMASUE SHINGOKATAOKA MASAHITOMORIMOTO HITOSHI
    • F16C17/24F01D25/28F16C17/03F16C41/04
    • B66F3/24B66F17/00F01D25/285F16C17/03F16C17/24F16C41/04F16C2237/00F16C2360/23
    • A lifting tool (1) for a rotary shaft (S4) in a rotary machine, said lifting tool being inserted between the rotary shaft (54) and a bearing stand (2) which surrounds at least the lower part of the outer circumference of the rotary shaft (54). This lifting tool (1) for a rotary shaft (54) has a pedestal (8) that is supported by the inner circumferential surface (2a) of the bearing stand (2), and a jack part (9) that is provided between the pedestal (8) and the outer circumferential surface of the rotary shaft (54), and that expands/contracts in the radial direction. The size of the pedestal (8) in the radial direction is smaller than the gap between the rotary shaft (54) and the bearing stand (2) in the radial direction, and a rotor bearing (10) having a cylindrical surface corresponding to the outer circumferential surface of the rotary shaft (54) is provided between the jack part (9) and the rotary shaft (54), Multiple support members (11) oriented in a direction other than the direction of the jack part (9) are provided on the rotor bearing (10).
    • 的提升工具(1)一种用于在旋转机械的旋转轴(S4)轴,插入所述旋转(54)和轴承之间所述提升工具架(2),其围绕至少的外周的下部 旋转轴(54)。 这对于旋转轴(54)提升工具(1)具有一个底座(8)那样,通过内周面(2a)的所述轴承的支架(2)和一个插口部分(9)并在之间设置有支撑 基座(8)和旋转轴(54)的外周表面,并没有在径向方向上膨胀/收缩。 在径向方向上的基座(8)轴的尺寸比旋转(54)与轴承之间的间隙更小的支架(2)在径向方向上,并具有一个圆柱形表面对应于所述的转子轴承(10) 在插孔部分(9)和在比所述插孔部的方向之外的方向上取向的旋转轴(54),多个支撑构件(11)之间,设置在旋转轴的外圆周表面(54)(9)被提供 在转子轴承(10)。
    • 8. 发明公开
    • TILTING PAD THRUST BEARING AND TILTING PAD THRUST BEARING ASSEMBLY
    • KIPPSEGMENT-SCHUBLAGER UND KIPPSEGMENT-SCHUBLAGERANORDNUNG
    • EP3037685A1
    • 2016-06-29
    • EP15202386.7
    • 2015-12-23
    • Doosan Heavy Industries & Construction Co., Ltd.
    • BANG, Kyung Bo
    • F16C17/06F16C33/10F16C41/02F16C27/02F16C17/24
    • F16C17/24F16C17/06F16C17/243F16C27/02F16C33/1045F16C33/108F16C41/02F16C2360/00
    • A tilting pad thrust bearing (10) and a tilting pad thrust bearing assembly are provided. The tilting pad thrust bearing is configured such that when a load is concentrated on only a portion of a thrust bearing because of eccentricity or inclination of a rotating shaft, associated tilting pads are tilted so that the load can be dispersed to the other tilting pads to which comparatively small load is applied, whereby the tilting pads to which the concentrated load is applied can be prevented from being damaged. Furthermore, the tilting pads can be fixed by oil supply nozzles without using a separate fastening member, whereby the size of the tilting pad thrust bearing can be markedly reduced. The tilting pads and a plate have improved structures so that the time and cost required to manufacture the tilting pad thrust bearing or tilting pad thrust bearing assembly can be reduced.
    • 提供倾斜垫推力轴承(10)和倾斜垫推力轴承组件。 倾斜垫推力轴承构造成使得当负载集中在推力轴承的一部分上时,由于旋转轴的偏心或倾斜,相关联的倾斜垫片被倾斜,使得负载能够分散到另一个倾斜垫片 施加相对较小的载荷,由此可以防止施加集中载荷的倾斜垫被损坏。 此外,倾斜垫可以通过供油喷嘴固定而不使用单独的紧固构件,由此可以显着地减小倾斜垫推力轴承的尺寸。 倾斜垫片和板材具有改进的结构,从而可以减少制造倾斜垫推力轴承或倾斜垫推力轴承组件所需的时间和成本。
    • 9. 发明公开
    • SYSTEM FOR ISOLATING ELECTRICAL CURRENT IN A BEARING FOR USE IN AN AIRCRAFT STRUCTURE
    • SYSTEM FOR权力的仓库FOR USE IN平面结构的电绝缘
    • EP3006751A1
    • 2016-04-13
    • EP15185647.3
    • 2015-09-17
    • Roller Bearing Company of America, Inc.
    • FRUIN, John W.ANDERSON, BenSIMPSON, MauraHENN, AndrewBRYANT, Kevin
    • F16C23/04B64C9/02
    • F16C17/24B64D45/02F16C23/043F16C23/045F16C33/201F16C33/74F16C2326/43
    • A system (10) for isolating electrical current in an aircraft structure includes a first structure (30) a bearing having an outer race (22) and an inner race (24) and a liner (28) disposed therebetween, the inner race having a second structure (40) coupled thereto. A dielectric seal (26) is secured to the outer race (22) and engages the inner race (24). A conditionally non-conductive gas (60) occupies a sealed chamber (50) that defines a gap (G) between the inner race (24) and the outer race (22). The gap (G) has a predetermined magnitude sufficient to prevent electrical arcing or current leakage between the inner race (24) and the outer race (22) at a first voltage less than that voltage resulting from a lightning strike; and/or to conduct an electrical current between the inner race (24) and the outer race (22) at a second voltage greater than or equal to the voltage resulting from the lightning strike.
    • 一种用于在飞机结构中分离的电流系统(10)包括第一结构(30),其具有上外座圈(22)的轴承和衬套之间,具有内圈设在其内座圈(24)和(28) 第二结构(40)联接到其上。 电介质密封件(26)被固定到所述外座圈(22)和接合所述内圈(24)。 有条件其它非导电气体(60)占据的密封室(50)那样定义内圈(24)和外圈(22)之间的间隙(G)。 的间隙(G)具有预定的大小足以防止在内圈(24)和在第一电压小于该电压来自雷击导致的外座圈(22)之间产生电弧或漏电流; 和/或内座圈(24)和在第二电压大于或等于电压从雷击导致的外座圈(22)之间传导电流的。