公开(公告)号：US20220088731A1

公开(公告)日：2022-03-24

申请号：US17424392

申请日：2020-02-17

Applicant: DALIAN UNIVERSITY OF TECHNOLOGY

Inventor： Jiang GUO ,  Bin WANG ,  Chuanping SONG

IPC: B23Q3/08 ,  B23Q3/06 ,  B23C3/00

Abstract: A supporting device and method for a large thin-walled part is disclosed. The supporting device comprises a processing device and a supporting device. A workpiece is positioned between the processing device and the supporting device and is clamped at a periphery in a flexible clamping mode. A cutter in the processing device is connected with an iron core. A coil is wound on the iron core. When the coil is energized, a magnetic field is generated around the coil. A blade part of the cutter is in contact with a processing side of the workpiece. The supporting method combines the magnetorheological fluid technology with the jet supporting technology, and uses a jet impact force to offset part of a milling force. The current magnitude and winding mode of the coil are changed to control magnetic field intensity. The magnetorheological fluid is cured instantly to support the workpiece.

公开(公告)号：US20160187230A1

公开(公告)日：2016-06-30

申请号：US14781941

申请日：2014-02-12

Applicant: DALIAN UNIVERSITY OF TECHNOLOGY

Inventor： Bo WANG ,  Peng HAO ,  Gang LI ,  Kuo TIAN ,  Zeng MENG ,  Kaifan DU ,  Yan ZHOU ,  Xi ZHANG ,  Xiaohan TANG ,  Bin WANG ,  Hongzhi LUO

IPC: G01M99/00

CPC classification number: G01M99/007 ,  B64C1/068 ,  G06F17/5018 ,  G06F2217/16 ,  G06F2217/46

Abstract: A method for determining a reduction factor of a bearing capacity of an axial load cylindrical shell structure relates to stability checking of main bearing strength thin-walled members of aerospace and architectural structures. Different from experiment experience-based conventional defect sensitivity evaluating method represented by NASA SP-8007, a depression defect is introduced in a manner of applying a radial disturbance load. First, an influence rule of a depression defect amplitude of a single point to an axial load bearing capacity is analyzed by using numerical values, so as to determine a load amplitude range; then, defect sensitivity analysis is performed on depression defects of multiple points; then, experiment design sampling is performed by using load amplitude values and load position distribution as design variables; and finally, based on optimizing technologies such as an enumeration method, a genetic algorithm and a surrogate model, the most disadvantageous disturbance load of the multiple points that limits the defect amplitude is searched for, and a reduction factor of the bearing capacity of the axial load cylindrical shell structure is determined, so as to establish a more physical method for evaluating the defect sensitivity and the bearing performance of the axial load cylindrical shell structure.

Abstract translation: 用于确定轴向负载圆柱形壳结构的承载能力的减小因子的方法涉及航空航天和建筑结构的主轴承强度薄壁构件的稳定性检查。 与NASA SP-8007代表的基于实验经验的常规缺陷灵敏度评估方法不同，以施加径向干扰负荷的方式引入凹陷缺陷。 首先，通过使用数值分析单点到轴向载荷能力的凹陷缺陷幅度的影响规律，以确定载荷幅度范围; 然后对多个点的抑郁缺陷进行缺陷敏感性分析; 然后，通过使用负载幅度值和负载位置分布作为设计变量进行实验设计采样; 最后，基于枚举方法，遗传算法和代理模型等优化技术，搜索限制缺陷幅度的多个点的最不利的干扰负载，并且轴向承载能力的减小因子 确定负载圆柱壳结构，以建立更为物理的方法来评估轴向负载圆柱壳结构的缺陷灵敏度和轴承性能。