首页> 外国专利> Rotating machine arrangement for turbomachine of aircraft, has oil lubrication circuit with oil conveying conduit that is extended from aperture toward fixed central axle and rollers

Rotating machine arrangement for turbomachine of aircraft, has oil lubrication circuit with oil conveying conduit that is extended from aperture toward fixed central axle and rollers

机译:用于飞机涡轮机的旋转机装置,具有带有油输送管路的油润滑回路,该油输送管路从孔向固定的中心轴和滚子延伸

摘要

The arrangement has a case (2) surrounding and turning around a fixed central axle (1). An oil lubrication circuit (7) serves as rollers (4, 5) in the case. The oil lubrication circuit includes an oil conveying conduit provided with an oil inlet aperture to be opened in a case unobstructed annular volume (6) covering the oil. The conduit is extended from the aperture toward the axle and the rollers. The annular volume is defined by an external wall of the case. The conduit includes a bend portion (12) extended under an envelope of a rotating machine, which is exposed to an exterior.
机译:该装置具有围绕固定的中心轴(1)并围绕其旋转的壳体(2)。油润滑回路(7)在壳体中用作滚子(4、5)。该油润滑回路包括设置有油入口孔的油输送导管,该油入口孔在覆盖油的无阻碍的环形容积(6)的情况下打开。导管从孔口朝向轴和滚轴延伸。环形容积由壳体的外壁限定。该导管包括弯曲部分(12),该弯曲部分在旋转机器的外壳下方延伸,该外壳暴露于外部。

著录项

相似文献

  • 专利
  • 外文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号