首页> 外国专利> ROTOR SUPPORT WITH A THEORETICAL BREAK POINT FOR TURBOPROPULSION ENGINES.

ROTOR SUPPORT WITH A THEORETICAL BREAK POINT FOR TURBOPROPULSION ENGINES.

机译:转子支持,带有理论上的突破点,适用于涡轮推进发动机。

摘要

Rotor support (10) with a theoretical breaking point (14), especially for the rotor (16) of a turbine, which comprises a rotating bearing (12), which is arranged between a stationary bearing support (26) ) and a rotating bearing support (24); in this case, to constitute the theoretical point of rupture (14) the stationary bearing support (26) is divided into the two parts (26a, 26b), and it comprises two separation surfaces (28a, 28b), which are arranged vertically with respect to the axis of rotation (22) of the rotation bearing (12); in this case, several tensioning bolts (32) are distributed uniformly on the circumference of the bearing support in an axial alignment and with a previously determined tensile strength; This rotor support is characterized in that within several guide surfaces (34a, 34b) -which are uniformly distributed along the circumference of the bearing support (26), and they are located within the two separation surfaces (28a, 28b) opposite each other, in pairs and in the axial direction - there are guide bodies (36), inserted in these surfaces, and the two separation surfaces (28a, 28b), with the guide bodies (36 ) inserted in the guide surfaces (34a, 34b), they are being kept butt between each other - with exemption of clearances - by means of some tensioning screws (32), which are oriented in the axial direction, so that each of the guide surfaces (34a) within a separation surface (28a) is composed of a cylindrical base surface with an axial orientation as well as a conical tip which, like the vertex, is arranged next to the cylindrical surface; and this in such a way that each of the guide surfaces (34a) within the other separation surface (28b) is realized as a tapered tip with axial orientation; or in such a way that each of the guide surfaces (34a) within a separation surface (28 a) is composed of a cylindrical and axially oriented surface as well as a concave hemisphere such as the vertex; in this case, the diameter of the cylindrical base surface and the diameter of the conical hemisphere correspond to the diameter of the guided guide body (36); characterized in that each of the guide surfaces (34a) is made - within the other separation surface (28b) - in the form of a concave and axially oriented partial sphere, whose radius corresponds to the radius of the guide body (36) or is greater than the same; as well as characterized in that the guide bodies (36) are made in the form of balls, whereby the radial housing forces (44), which attack on the bearing support (26), can be converted -through the bodies guide (36), which act in conjunction with the guide surfaces (34a, 34b) - in axial tensile forces (48), which attack on the tensioning screws (32) and they lead to the breakage of the screws tensioners (32) when a maximum tensile force previously exceeded is exceeded.
机译:具有理论断裂点(14)的转子支撑件(10),特别是用于涡轮机的转子(16)的转子支撑件(10),该转子支撑件(10)包括旋转轴承(12),该旋转轴承(12)布置在固定轴承支撑(26)和旋转轴承之间支持(24);在这种情况下,为了构成理论断裂点(14),将固定轴承座(26)分为两个部分(26a,26b),它包括两个分离面(28a,28b),两个分离面垂直相对于旋转轴承(12)的旋转轴线(22);在这种情况下,几个张紧螺栓(32)沿轴向对齐并以预先确定的抗拉强度均匀地分布在轴承座的圆周上。该转子支架的特征在于,在沿轴承支架(26)的圆周均匀分布的几个导向表面(34a,34b)内,它们位于彼此相对的两个分离表面(28a,28b)内,成对并沿轴向方向-有插入这些表面的导向体(36)和两个分隔表面(28a,28b),其中导向体(36)插入导向面(34a,34b),它们通过一些沿轴向定向的张紧螺钉(32)保持彼此对接-消除了间隙,从而使分离表面(28a)内的每个导向表面(34a)由一个具有轴向方向的圆柱形底面和一个圆锥形尖端组成,该圆锥形尖端像顶点一样排列在该圆柱形表面附近;并且以这样的方式,在另一个分离表面(28b)内的每个引导表面(34a)被实现为具有轴向取向的锥形尖端。或以这样的方式,在分离表面(28a)内的每个引导表面(34a)由圆柱形且轴向定向的表面以及凹入的半球(例如顶点)组成;在这种情况下,圆柱形底表面的直径和圆锥形半球的直径对应于被引导的导向体(36)的直径。其特征在于,每个引导表面(34a)在另一个分隔表面(28b)内制成凹入且轴向定向的部分球体,其半径对应于引导体(36)的半径或大于同一个其特征还在于,导向体(36)制成球状,从而可以通过导向体(36)来转换作用在轴承座(26)上的径向壳体力(44)。 ,它们与导向表面(34a,34b)一起作用于轴向拉力(48),该轴向拉力作用在张紧螺钉(32)上,并在最大张紧力时导致螺钉张紧器(32)断裂超出了先前的超出范围。

著录项

  • 公开/公告号ES2320325T3

    专利类型

  • 公开/公告日2009-05-21

    原文格式PDF

  • 申请/专利权人 MTU AERO ENGINES GMBH;

    申请/专利号ES20020024038T

  • 发明设计人 DIEPOLDER WOLFGANG DR.;WOHRL BERNHARD DR.;

    申请日2002-10-28

  • 分类号F01D21/04;F01D25/16;F16C19/52;F16C35/04;F16D9/04;

  • 国家 ES

  • 入库时间 2022-08-21 19:23:49

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