直升机尾桨卡滞后着陆的操控分析  

Control Analysis on Landing of Helicopter Tail Rotor Seized

作　　者：费景荣 张朋[2] FEI Jingrong;ZHANG Peng(School of Basic Science for Aviation,Naval Aviation University,Yantai 264001,China;Chinese People's Liberation Army Unit 92522,Huludao 125001,China)

机构地区：[1]海军航空大学航空基础学院,山东烟台264001 [2]中国人民解放军92522部队,辽宁葫芦岛125001

出　　处：《直升机技术》2022年第4期50-53,58,共5页Helicopter Technique

摘　　要：在简述直升机尾桨卡滞后着陆的主要风险点与风险管控对策的基础上,分析了直-X系列直升机返场、接地速度及着陆方法;重点研究了无风、侧风条件下尾桨卡滞后着陆的有关问题;最后得出了该型机尾桨卡滞后着陆操控的结论。所得结论对其他无涵道尾桨的单旋翼直升机有一定参考价值。Based on the brief description of the main risk points and risk control countermeasures of the helicopter tail propeller truck lag landing,the return,grounding speed and landing method of helicopter were analyzed,and the problems related to the lagging landing of the tail propeller card under windless and crosswind conditions were mainly studied.Finally,the conclusion was drawn that the tail propeller card of this type was delayed in landing control.The conclusions obtained had certain reference value for other single-rotor helicopters without a bypass tail rotor.

关 键 词：直升机尾桨卡滞 操控要领 飞行条件 飞行安全 

分 类 号：V328[航空宇航科学与技术—人机与环境工程]