The invention discloses a serial helicopter cockpit with a variable configuration. A front cabin and a rear cabin are sequentially arranged from front to back to form a serial structure; the rear cabin floor is erected and installed through a rear cabin structural framework and a rear cabin wall plate in the rear cabin windshield assembly, so that the height of the rear cabin floor is adjusted, and the rear cabin floor is higher than the front cabin floor. The front cabin windshield assembly, the front cabin instrument assembly and the rear cabin instrument assembly are adjustable in the height direction and the heading direction, the rear cabin floor and the rear cabin windshield assembly are adjustable in the height direction, and the front cabin seat and the rear cabin seat are adjustable in the height direction and the heading direction. Control boards and control lever systems in the front cabin control assembly and the rear cabin control assembly are adjustable; by adjusting the height, front-back position or roll angle of each component in the tandem helicopter cockpit, the tandem helicopter cockpit is placed in a to-be-assessed configuration for implementation of assessment. According to the method, the problem that instance evaluation and onboard verification are difficult to perform on the appearance of the cockpit and the arrangement of cockpit equipment at the initial stage of design is solved.
本发明公开一种可变构型的串列式直升机驾驶舱,前舱和后舱以前后依次排布的形式布局为串列式结构;后舱地板通过后舱风挡组件中的后舱结构骨架和后舱壁板架设安装,使得后舱地板进行高度调节、且高于前舱地板;前舱风挡组件、前舱和后舱仪表组件均具有在高度和航向方向上的可调性,后舱地板和后舱风挡组件具有在高度方向上的可调性,前舱和后舱座椅具有在高度、航向方式上的可调性,前舱和后舱操纵组件中的操纵台和操纵杆系均具有可调性;通过调节串列式直升机驾驶舱中各部件的高度,前后位置或横滚角,将串列式直升机驾驶舱置于待评估构型以实施评估。本发明解决了难以在设计初期对驾驶舱外形和驾驶舱设备布置进行实例评估及机上验证的问题。
Configuration-variable tandem helicopter cockpit
一种可变构型的串列式直升机驾驶舱
2025-02-11
Patent
Electronic Resource
Chinese
Multimission helicopter cockpit displays
SPIE | 1996
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