王秀红,贾沛颖,韩心雨,高清敏,朱格璐.基于TRIZ/专利规避集成理论的快递无人机载物装置[J].包装工程,2022,43(11):261-271.
WANG Xiu-hong,JIA Pei-ying,HAN Xin-yu,GAO Qing-min,ZHU Ge-lu.Patent Circumvention for Delivery UAV Loading Device Based on TRIZ[J].Packaging Engineering,2022,43(11):261-271. |
| 基于TRIZ/专利规避集成理论的快递无人机载物装置 |
| Patent Circumvention for Delivery UAV Loading Device Based on TRIZ |
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| DOI：10.19554/j.cnki.1001-3563.2022.11.034 |
| 中文关键词: TRIZ 专利规避 快递无人机 载物装置 |
| 英文关键词: TRIZ patent circumvention delivery drones slide device |
| 基金项目:国家自然科学基金(71974175);河南省科技攻关项目(212102310494，222102210329);河南省教育厅人文社科一般项目(2021?ZZJH?410);河南省大学生创新创业训练计划(202110485005X) |
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| 中文摘要: |
| 目的 设计一种结构简单，稳固安全性强，可根据承载物体形状进行快速调整的的快递无人机载物装置。方法 采用TRIZ/专利规避集成理论对快递无人机的载物装置进行创新设计。首先对专利库中的快递无人机载物结构进行专利分析，确定其规避对象为悬吊式无人机载物装置，采用伞形专利组合规避设计方法，建立专利−问题模型确定有用作用和问题作用，确定设计矛盾，运用40条发明原理和76个标准解建立改善后功能模型图，并对其载物装置进行设计。结果 仿真结果表明，创新产品最大工作载荷为225 N，关键部件轨道机翼最大静止状态应力为1.023×107 MPa，飞行状态应力为1.576×107 MPa。载物架最大静止状态应力为1.049×106 MPa，飞行状态应力为2.126×106 MPa。结论 与悬吊式载物装置相比，创新的产品在可载物的形状多样性、稳定性方面更好，更实用、轻便;与吊架托盘式无人机相比，该产品更稳固耐用。 |
| 英文摘要: |
| The paper aims to design an express UAV carrier device with simple structure and strong stable safety that can be quickly adjusted according to the shape of the carrying object. The TRIZ/patent circumvention integrated theory is adopted for the innovative design of the loading device of the Courier UAV. Firstly, express UAV slide structure in China's current patent library is analyzed, the evading object UAV for suspension type slide device is determined, and the umbrella patent portfolio hedge design method is adopted. Patent-function model is established to determine the useful effect and problems, and determine the design. Using the principle of 40 invention and 76 standard solution, after function model figure is built and improved. Finally, stress analysis is carried out on the designed cargo carrying device of the Courier UAV. The simulation results show that maximum workload for innovative products is 225 N, maximum stress of rail wing is 1.023×107 MPa in the static state and 1.576×107 MPa in the flight state. Maximum stress of load frame is 1.049×106MPa in the static state and 2.126×106 MPa in the flight state. Compared with the suspended UAV, the product has better capability in the shape and quality of the payload and is more practical and light. Compared with the hanger tray UAV, the product is more stable and durable. |
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