CAJ | 학술논문

我国正在开展大型客机的研制工作，增升装置设计是其中的关键技术之一。借鉴A350和波音787的后缘增升装置及其机构特点，研究了后缘铰链襟翼气动和机构一体化的设计。后缘铰链襟翼，是利用简单铰链机构驱动的后缘单缝襟翼增升装置，该机构由于构造简单、维护方便、制造成本低等优点备受青睐。详细介绍了基于CATIA二次开发创建的后缘铰链襟翼气动机构一体化设计模块，并嵌入到原大型飞机增升装置气动机构一体化设计平台上，获得较好的效果，为我国未来大型客机增升装置设计奠定了技术储备。
아국정재개전대형객궤적연제공작，증승장치설계시기중적관건기술지일。차감A350화파음787적후연증승장치급기궤구특점，연구료후연교련금익기동화궤구일체화적설계。후연교련금익，시이용간단교련궤구구동적후연단봉금익증승장치，해궤구유우구조간단、유호방편、제조성본저등우점비수청래。상세개소료기우CATIA이차개발창건적후연교련금익기동궤구일체화설계모괴，병감입도원대형비궤증승장치기동궤구일체화설계평태상，획득교호적효과，위아국미래대형객궤증승장치설계전정료기술저비。
High-Lift device design is one of the key technologies during the development of large aircraft in Chi-na. Refered to the trailing edge high lift and its characteristic of airplane A350 and B787, aero-mechanism interg-rated design of trailing edge hinge flap is researched. Trailing edge hinge flap is one of new advance high lift de-vices which uses simple hinge device to drive trailing edge high lift system. The advantage and disadvantage of the hinge flap with good prospects for development has been discussed. Aero-mechanism intergrated design modules are introduced in detail, which intergrated design of trailing edge hinge flap has been established based on the sec-ondary development of CATIA. And the aero-mechanism intergrated design modules are set in an intergrated design platform. The platform improves efficiency for designing high lift device of large aircraft. The good results show that the design points out the development direction of high lift device on large aircraft and provides advices for further study.