The invention discloses an assembly type modular rudder and wing locking and unlocking mechanism and a steering engine system comprising the same, and belongs to the field of folding wing type rudder systems. Through the assembly type modular design, the rudder and wing locking and unlocking mechanism is separated from a steering engine body under the condition that the functions of the rudder and wing locking and unlocking mechanism are not affected, a traditional integral forming mode is replaced, and the assembly type modular rudder and wing locking and unlocking mechanism is convenient to assemble and disassemble. And the steering engine body can be assembled with the rudder wing locking and unlocking mechanism for multiple times for use. According to the assembly type modular rudder wing locking and unlocking mechanism and the steering engine system comprising the assembly type modular rudder wing locking and unlocking mechanism, the motion trail of a locking disc in a traditional steering engine mechanism after explosion is analyzed, and the structural characteristics of a rudder wing body are matched, so that in the rising process of the locking disc, locking of the rudder wing body is relieved firstly, then the rudder wing body is pushed to be unfolded, and the rudder wing body is locked and unlocked; a traditional mode that a bottom boss impacts the rudder wing body for unfolding is replaced, and the structure of the rudder wing body is further simplified under the condition that it is guaranteed that the rudder wing body can be normally unfolded.

    本发明公开了一种装配式模块化舵翼锁紧解锁机构及包含其的舵机系统,属于折叠翼式舵系统领域,其通过装配式、模块化的设计,使得舵翼锁紧解锁机构在不影响其自身功能的情况下,脱离舵机本体设置,代替了传统一体成型的方式,使舵机本体可多次装配舵翼锁紧解锁机构进行使用。本发明的装配式模块化舵翼锁紧解锁机构及包含其的舵机系统,其通过传统舵机机构中锁紧盘在爆炸后的运动轨迹进行分析,配合舵翼本体的结构特征,使得锁紧盘在上升的过程中,先解除对舵翼本体的锁定,再顺势推动舵翼本体展开,代替了传统通过底部凸台撞击舵翼本体进行展开的方式,保证了舵翼本体可正常进行展开作业的情况下,对其结构进行了进一步简化。


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    Titel :

    Assembly type modular rudder wing locking and unlocking mechanism and steering engine system comprising same


    Weitere Titelangaben:

    一种装配式模块化舵翼锁紧解锁机构及包含其的舵机系统


    Beteiligte:
    CHEN ZIWEI (Autor:in) / YANG ZHI (Autor:in) / HUANG XINGTONG (Autor:in) / WANG JIAN (Autor:in) / PAN ZHUO (Autor:in) / WANG CHENGUANG (Autor:in) / BAI LEI (Autor:in) / DENG QIANGQIANG (Autor:in) / ZHANG KE (Autor:in) / WANG HONGSHENG (Autor:in)

    Erscheinungsdatum :

    2023-05-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    F42B EXPLOSIVE CHARGES, e.g. FOR BLASTING , Explosive Ladungen, z.B. für Sprengungen / B64U



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