发明名称 Tension bolt for aircraft engine attaching device, has pin inserted in gap in radial hole of screw, and elliptical threaded crown extended by notched crown whose inner diameter is larger than base diameter of thread of nut
摘要 <p>The tension bolt has a screw (1) pierced with a radial hole (13), and a nut (2) provided with a support face (211) and an elliptical threaded crown (25) including an elliptical section, where the threaded crown is placed at an end opposite to the support face. The threaded crown is extended by a notched crown whose inner diameter is larger than base diameter of a thread of the nut. A pin (3) i.e. split pin, is inserted in gap (23) in the radial hole of the screw. An operating unit (21) is provided between the threaded crown and the support face.</p>
申请公布号 FR2955632(A1) 申请公布日期 2011.07.29
申请号 FR20100050594 申请日期 2010.01.28
申请人 AIRBUS OPERATIONS 发明人 CASSAGNE JEROME;MARTIN YVON;FAVRESSE PIERRE ANDRE
分类号 F16B39/04;B64D27/26;F16B31/00;F16B35/00;F16B39/284 主分类号 F16B39/04
代理机构 代理人
主权项
地址