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AUTOMATIC DRILLING AND RIVETING ACTUATING MECHANISM AND METHOD SUITABLE FOR RIVETING ROCKET CABIN BODY

机译:适用于铆接火箭舱体的自动钻孔和铆接致动机理和方法

摘要

Provided are an automatic drilling and riveting actuating mechanism and a method suitable for riveting a rocket cabin body, comprising a rivet injection module (1), a rivet inserting and pressing module (2), a drilling and countersinking module (3), a switching module (4) and a pressed ranging module (5); wherein, the pressed ranging module (5) presses the rocket cabin body, the drilling and countersinking module (3) completes drilling or countersinking on the surface of the cabin body, meanwhile, the rivet injection module (1) injects a rivet (159) into the tail end of the rivet inserting and pressing module (2), the switching module (4) realizes the position exchange of the drilling and countersinking module (3) and the rivet inserting and pressing module (2), and the rivet inserting and pressing module (2) inserts the rivet (159) into a prepared hole position and completes riveting. The pressed ranging module (5) measures the position of the cabin body, feeds back and corrects the feed amount of the hole making and countersinking, and accommodates the roundness error of the cabin body. The actuating mechanism can realize automatic rivet feeding and inserting of multiple models of rivets, and can detect each process, thereby avoiding the occurrence of no rivet and crooked rivets, and form an effective protection for the rocket cabin body.
机译:提供了一种自动钻孔和铆接致动机构,并且一种适合于铆接火箭舱体的方法,包括铆钉喷射模块(1),铆钉插入和按压模块(2),钻孔和柜台模块(3),切换模块(4)和压缩模块(5);其中,压制的测距模块(5)按压火箭舱体,钻孔和钻孔模块(3)在驾驶室主体的表面上完成钻孔或倒孔,同时铆钉喷射模块(1)注入铆钉(159)进入铆钉插入和按压模块(2)的尾端,切换模块(4)实现钻孔和埋头孔(3)的位置交换和铆钉插入和压制模块(2),以及铆钉插入和铆钉按压模块(2)将铆钉(159)插入制备的孔位置并完成铆接。按下的测距模块(5)测量驾驶室主体的位置,回来并校正孔制作的进给量和倒计时,并容纳机舱体的圆度误差。致动机构可以实现自动铆钉进给和插入多种铆钉型号,并且可以检测每个过程,从而避免出现铆钉和弯曲铆钉,并为火箭舱体形成有效的保护。

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