直8A型机燃油附件综合试验器的研制  

THE DESIGN AND DEVELOPMENT OF TYPE 8A HELICOPTER'S FUEL ACCESSORY INTERGRATED TEST EQUIPMENT

作　　者：郑友兰[1] 叶宁武[1] 王黑云[1] 

机构地区：[1]中国直升机设计研究所,景德镇333001

出　　处：《直升机技术》2004年第4期34-37,共4页Helicopter Technique

摘　　要：本文介绍了直8A 型机燃油附件综合试验器的研制过程。概括地描述了试验器的研制概况、功能及原理、设计特点及试验验证。直8A 型机燃油附件综合试验器的研制成功,填补了行业空白。具有显著的经济效益和社会效益。This paper introduces process the design and development of type 8A helicopter's fuel accessory test equipment. Describs development general situation、function、design features and test verity.The success of type 8A helicopter's fuel ac- cessory intergrated test equipment,fill up the industry.It has evidence economy benefits and social benefits.

关 键 词：综合试验器 设计 试验 直升机 

分 类 号：V275.1[航空宇航科学与技术—飞行器设计]