The invention relates to a cargo loading method for an ultra-narrow engine room of a branch cargo machine. A system comprises a branch cargo aircraft, a cockpit is arranged at the front end of the branch cargo aircraft, an empennage is arranged at the rear part of the branch cargo aircraft, wings are arranged outside the branch cargo aircraft, a cabin door is arranged on a body of the branch cargoaircraft, and an ultra-narrow body cabin is arranged inside the branch cargo aircraft, a front loading area and a rear loading area are arranged in the cabin, and the gravity center of the branch cargo aircraft in a horizontal state is positioned in the rear loading area; cabin doors comprise a front cabin door and a rear cabin door, the front cabin door is arranged on the front half portion of the front loading area, and the rear cabin door is arranged on the rear half portion of the rear loading area; and a front frame plate is arranged on the front portion of the front loading area, a rearframe plate is arranged on the rear portion of the rear loading area, and a preset distance is reserved between the gravity center of the branch cargo aircraft and the front frame plate. By using themethod and the system provided by the invention to load cargoes, the cargoes can be efficiently loaded in a gravity center balance state in the whole process, so that the method and the system can bewidely applied to the technical field of branch aviation cargo transportation.
本发明涉及一种用于支线货机超窄体机舱的货物装载方法,包括支线货机,支线货机前端设有驾驶舱,支线货机后部设有尾翼,支线货机外部设有机翼,支线货机机身上设有舱门,支线货机内部设有超窄体机舱,其特征在于,机舱内设有前置装载区和后置装载区,支线货机在水平状态下的重心位于后置装载区内;舱门包括前舱门和后舱门,其中,前舱门设于前置装载区的前半部,后舱门设于后置装载区的后半部;前置装载区前部设有前框板,后置装载区后部设有后框板,支线货机的重心与前框板之间设有预定距离。通过使用本发明提供的方法以及系统装载货物,能够保证全过程重心平衡状态下的货物高效装载,从而能够广泛应用在支线航空货物运输技术领域。
Cargo loading method and system for ultra-narrow engine room of branch cargo machine
一种支线货机超窄体机舱的货物装载方法及系统
26.06.2020
Patent
Elektronische Ressource
Chinesisch
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