首页> 外国专利> MOUNTING BRACKET OF UNIT ON SHELL OF TURBOMACHINE BODY

MOUNTING BRACKET OF UNIT ON SHELL OF TURBOMACHINE BODY

机译:涡轮机壳体上单元的安装支架

摘要

FIELD: turbomachine building.SUBSTANCE: invention relates to the field of turbomachinery, mainly to aircraft engine construction, namely to the nodes connecting the units with the shell of the turbomachine body. Unit mounting bracket on the shell of the turbomachine body contains a boss, located between the body shell and the unit, with a support platform and a threaded hole for the installation of the unit. Bracket is provided with two inclined stiffening ribs located outside the lug and made extending toward the side of the body shell. Each stiffener is made of a curvilinear, convex-facing part of the body shell. One edge of the ribs is connected to the boss, and the opposite edge of the ribs is connected to the body shell.EFFECT: invention provides an increase in the rigidity of the shell of the turbomachine body at the attachment point with the bracket, which leads to an increase in the strength and reliability of the connection node in the case of dynamic loading, namely when subjected to vibration.7 cl, 1 dwg
机译:涡轮机制造技术领域本发明涉及涡轮机领域,主要涉及飞机发动机的制造,即将单元与涡轮机主体的壳体连接的节点。涡轮机壳体上的单元安装支架包括一个位于壳体和单元之间的凸台,该凸台带有一个支撑平台和一个用于安装单元的螺纹孔。支架上有两个倾斜的加劲肋,这些加劲肋位于凸耳的外侧,并朝车身外壳的侧面延伸。每个加劲肋均由车身外壳的弯曲凸面部分制成。肋的一个边缘连接到凸台,而肋的相对边缘连接到车体壳体。效果:本发明提高了涡轮机车体的壳体在与支架的附接点处的刚度,在动态载荷的情况下,即在受到振动的情况下,会导致连接节点的强度和可靠性提高。7 cl,1 dwg

著录项

  • 公开/公告号RU2017121056A3

    专利类型

  • 公开/公告日2018-12-18

    原文格式PDF

  • 申请/专利权人

    申请/专利号RU20170121056

  • 发明设计人

    申请日0000-00-00

  • 分类号F01D25/28;

  • 国家 RU

  • 入库时间 2022-08-21 11:47:09

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