首页> 外国专利> Coupling device for coupling modules, aircraft with coupling device, method for coupling and decoupling of modules

Coupling device for coupling modules, aircraft with coupling device, method for coupling and decoupling of modules

机译:用于耦合模块的耦合装置,具有耦合装置的飞机,用于耦合和解耦合模块的方法

摘要

Coupling device (2, 2 ') for coupling modules (1, 1') having a coupling surface (3), a primary coupling element (6, 6 ') and at least two secondary coupling elements (8a, 8a', 8b, 8b ') having. The primary coupling element (6, 6 ') is arranged on the coupling surface (3). By the primary coupling element (6, 6 ') extends a coupling axis (4, 4'), which is arranged parallel to a direction of action of the gravitational acceleration. The at least two secondary coupling elements (8a, 8a ', 8b, 8b') are complementary to each other and arranged on the coupling side (3) and each have a predetermined distance from the coupling axis (4a, 4b).
机译:用于具有耦合表面(3),初级耦合元件(6、6')和至少两个次级耦合元件(8a,8a',8b)的耦合模块(1、1')的耦合装置(2、2'), 8b')具有。初级联接元件(6、6')布置在联接表面(3)上。通过主联接元件(6、6')延伸联接轴线(4、4'),该联接轴线平行于重力加速度的作用方向布置。至少两个次级联接元件(8a,8a',8b,8b')彼此互补并且布置在联接侧(3)上,并且每个均与联接轴线(4a,4b)具有预定距离。

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
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