用于制造薄壁和高肋部件的重载荷无模成型机的混合位置-进给力控制

IF 6.3 1区 工程技术 Q1 AUTOMATION & CONTROL SYSTEMS IEEE/ASME Transactions on Mechatronics Pub Date : 2025-10-01 Epub Date: 2024-10-21 DOI:10.1109/TMECH.2024.3468463
Fangyan Zheng;Xinghui Han;Lin Hua;Wuhao Zhuang
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引用次数: 0

摘要

薄壁高肋件作为一种承重结构,在航空航天设备中得到了广泛的应用。提出了一种新的包络成形工艺,并提出了一种基于并联运动机构的包络成形机构。为了实现高成形性,必须同时跟踪刀具运动和成形力。然而,现有的力-位置控制方法采用弹性接触模型(弹簧-阻尼系统),无法对塑性成形力进行建模,使得现有的力-位置控制方法在塑性成形过程中失效。因此,为了实现沿进给方向的力控制和沿其他方向的位置控制,提出了一种适用于包皮成形过程的位置-力混合进给控制方法。考虑进给运动引起的连杆位姿变化和成形载荷引起的连杆变形,建立了高精度运动跟踪的刚柔耦合动力学模型。通过证明法向成形力与接触面积呈近似线性关系,并假设连续控制周期内的摩擦成形力参数恒定,建立了基于当前力状态和锥盘塑性变形假设的成形载荷实时预测模型,实现了快速响应力跟踪。通过对成形载荷的实时计算、成形进给速度的正演和伺服电机的三环控制,实现了一种适合重载包络成形工艺的高速成形电机。最后,高精度成形飞机伞齿轮和飞机窗框。与位置控制方法相比,该方法大大降低了零件误差、成形负荷和加工时间。结果表明,该材料具有较高的成形性,具有良好的应用前景。
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Hybrid Position-Force Feed Control of Heavy Load Forming Nonapod for Manufacturing Thin Wall and High Rib Parts
As load-bearing structures, thin wall and high rib parts (TWHRP) are widely used in aerospace equipment. A novel envelope forming process and the corresponding forming Nonapod with a parallel kinematic mechanism are developed for the manufacture of TWHRP. To realize high formability, tracking of tool motion and forming force simultaneously is necessary. However, the existing force-position control method utilizes an elastic contact model (spring-damper system), which cannot model the plastic forming force, making the existing force-position control method fail in the plastic force process. Therefore, in order to achieve force control along the feed direction and position control along other directions, a novel hybrid position-force feed control method (HPFCM) suitable for the envelope forming process is proposed. By taking into account both the change of link pose sourced from the feed motion and the deformation of the link caused by the forming load, rigid-flexible coupling dynamic model for high-precision motion tracking is established. By demonstrating that the normal forming force exhibits a near-linear relation with the contact area and assuming constant parameters for frictional forming force in consecutive control cycles, a real-time forming load prediction model based on the current force state and cone-disk plastic deformation hypothesis is developed for quick response force tracking. Through calculation of real-time forming load, forward of forming feed rate, and three-loop control of servo motors, an HPFCM is realized, tailored for the heavy load envelope forming process. Finally, aircraft bevel gears and aircraft window frames are formed with high precision. Compared to the position control method, the part error, forming load, and process time are highly reduced with HPFCM. This result shows high formability in the envelope forming of TWHRP and promising application prospects of the proposed HPFCM.
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来源期刊
IEEE/ASME Transactions on Mechatronics
IEEE/ASME Transactions on Mechatronics 工程技术-工程:电子与电气
CiteScore
11.60
自引率
18.80%
发文量
527
审稿时长
7.8 months
期刊介绍: IEEE/ASME Transactions on Mechatronics publishes high quality technical papers on technological advances in mechatronics. A primary purpose of the IEEE/ASME Transactions on Mechatronics is to have an archival publication which encompasses both theory and practice. Papers published in the IEEE/ASME Transactions on Mechatronics disclose significant new knowledge needed to implement intelligent mechatronics systems, from analysis and design through simulation and hardware and software implementation. The Transactions also contains a letters section dedicated to rapid publication of short correspondence items concerning new research results.
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