空客公司成功的机翼设计Ⅰ——A300及A310机翼设计  

Wings Design of Success for the Airbus Ⅰ——Wings Design of A300 and A310

作　　者：江永泉 Jiang Yong Quan(Shanghai Aircraft Design and Research Institute,Shanghai 201210,China)

机构地区：[1]上海飞机设计研究院,上海201210

出　　处：《民用飞机设计与研究》2018年第4期1-5,共5页Civil Aircraft Design & Research

摘　　要：空客公司的成功离不开其先进的机翼设计,其机翼由英国宇航公司负责设计和生产。空客飞机机翼先进的空气动力设计,包括尖峰后加载翼型、超临界翼型、先进跨声速机翼设计——超临界机翼设计、机翼与机身的干扰、翼梢小翼设计、增升装置设计,机翼低重量设计、机翼构型与载荷,详细设计,结构设计和低成本设计等。作为系列论文之一,综述A300及A310的机翼设计特点。The commercial success of the Airbus family owes much to the design of its wings,for which British Aerospace has been reponsible.This article describes advanced aerodynamic design of wings (including peaky-rear loading section,supecritical airfoil,advanced transonic wing design --supercritical wing design,wing-fuselage interference,winglet design,High-Lift device design),design for low weight,wing configuration and loads,detail design,structural design and low cost design.As one part of the article,this paper describes the wings design of A300 and A310.

关 键 词：机翼 空气动力学 载荷 结构 成本 

分 类 号：V214.11[航空宇航科学与技术—航空宇航推进理论与工程]