Study on Pneumatic Compatibility of Air Refueling in Propeller Transport Machine  

作　　者：YANChuanyin CHANGYingying CHENYing 

机构地区：[1]ShaanxiAircraftIndustryCo.,Ltd.,HanzhongShaanxi723000,China

出　　处：《外文科技期刊数据库(文摘版)工程技术》2022年第2期146-151,共6页

摘　　要：Air refueling is known as a multiplier of air power, and its most direct effect is to increase the range of the oil receiver and extend the battery life of the oil receiver. Different from small jets such as fighter jets and trainer aircraft, turboprop transport aircraft have the characteristics of large weight, large size, poor mobility and slow speed. When conducting air refueling, there are poor handling from formation, docking, refueling and departure, which greatly affects the success rate and safety of air refueling. The propeller transport engine uses turbine propeller engine as the power device and has unique flight characteristics during flight operation. By obtain test data, establish the six degrees of freedom simulation model and the pilot model of the pilot field of the tanker and draw out the safety area during refueling through simulation analysis.

关 键 词：tail vortex pneumatic compatibility simulation analysis safe area 

分 类 号：TB[一般工业技术]