一种飞机尾翼前缘除冰套安装方式  

An installation method of deicing boot on the leading edge of the wing and the tail

作　　者：杨粉蓉 陆鹏鹏 李鹏[2] YANG Fenrong;LU Pengpeng;LI Peng(Engineering Technology Center,AVIC Xi'an Civil Aircraft Co.,Ltd.,Xi'an 710089,China;Key Laboratoc of Auxiliao Chemistry&Technology for Chemical Industri,Ministo of Education,Shannxi University of Science&Technology,Xi'an 710021,China)

机构地区：[1]中航西飞民用飞机有限责任公司工程技术中心,西安710089 [2]陕西科技大学教育部轻化工助剂化学与技术重点实验室,西安710089

出　　处：《民用飞机设计与研究》2020年第1期44-48,共5页Civil Aircraft Design & Research

摘　　要：某型飞机平尾前缘除冰系统采用气动机械式除冰方式,在平尾前缘的防护区域敷设除冰套。平尾前缘采用双层金属蒙皮和玻璃纤维复合材料层压板密肋结构形式。通过某型机平尾前缘除冰套安装方式的改进和平尾前缘结构布置的确定,介绍了一种新型的机尾翼除冰套安装方式,平尾前缘结构形式简单,工艺性好,既能满足平尾前缘维修互换性要求,又能满足前缘除冰套安装和维护要求。The deicing system on the leading edge of the tail for a plane is used in the form of pneumatic mechanical method,in which deicing boot is installed at the protection area of the leading edge of the tail.The leading edge of the tail is made of double metal skin and fiber-glass reinforced composite laminate ribs.In this paper,a new installation method of deicing boot on the leading edge of the tail is introduced through improvement of the installation method of the deicing boot and confirming the structural arrangement in the leading edge of the tail The structure is simple and good in manufacture.It can meet the requirements of maintenance and interchange for the structure of the leading edge,and also meet the installation and maintenance requirements of the deicing system.

关 键 词：机尾翼前缘 结构布置 除冰系统安装 维修性 

分 类 号：V211.41[航空宇航科学与技术—航空宇航推进理论与工程] V244.15