空军工程大学学报(自然科学版)
空軍工程大學學報(自然科學版)
공군공정대학학보(자연과학판)
JOURNAL OF AIR FORCE ENGINEERING UNIVERSITY (NATURAL SCIENCE EDITION)
2010年
1期
15-18
,共4页
何荣光%郭定%杨俊超%史越
何榮光%郭定%楊俊超%史越
하영광%곽정%양준초%사월
直升机座舱%显示器周边键%振动环境%工效学实验
直升機座艙%顯示器週邊鍵%振動環境%工效學實驗
직승궤좌창%현시기주변건%진동배경%공효학실험
helicopter cockpit%keys around screen%vibration environment%ergonomics experiment
直升机座舱显示器周边键的工效学设计对于改善直升机操控性能有重要作用,在振动环境下其工效学特性的研究是该领域研究的薄弱环节.本研究在研制的直升机座舱实验平台上,设计了振动环境下直升机座舱显示器周边键的工效学实验.通过分析实验数据发现:按键反应时受按键方位和大小影响,无振动时,按键大小为10 mm即可;主振为23 Hz,振幅为人体稍感振动时,按键大小应增加25%以上,即13 mm,按键间隔以10 mm为宜;振动造成错误率上升和反应时延长,应控制在适当范围.
直升機座艙顯示器週邊鍵的工效學設計對于改善直升機操控性能有重要作用,在振動環境下其工效學特性的研究是該領域研究的薄弱環節.本研究在研製的直升機座艙實驗平檯上,設計瞭振動環境下直升機座艙顯示器週邊鍵的工效學實驗.通過分析實驗數據髮現:按鍵反應時受按鍵方位和大小影響,無振動時,按鍵大小為10 mm即可;主振為23 Hz,振幅為人體稍感振動時,按鍵大小應增加25%以上,即13 mm,按鍵間隔以10 mm為宜;振動造成錯誤率上升和反應時延長,應控製在適噹範圍.
직승궤좌창현시기주변건적공효학설계대우개선직승궤조공성능유중요작용,재진동배경하기공효학특성적연구시해영역연구적박약배절.본연구재연제적직승궤좌창실험평태상,설계료진동배경하직승궤좌창현시기주변건적공효학실험.통과분석실험수거발현:안건반응시수안건방위화대소영향,무진동시,안건대소위10 mm즉가;주진위23 Hz,진폭위인체초감진동시,안건대소응증가25%이상,즉13 mm,안건간격이10 mm위의;진동조성착오솔상승화반응시연장,응공제재괄당범위.
Ergonomics optimization design of keys around screen in helicopter cockpit is meaningful to the improvement of operating performance, but the research on its ergonomics characteristics in a vibration environment is a weak link. In this article, we take a new method to investigate this problem with a simulation platform. Through data analyses, some results are summed up as follows. The response time is affected by key size and its position. That the key size is 10 mm is preferable without vibration. And that it is 13 mm, or 25% bigger, in other words, is preferable with the vibration of 23 Hz which can be felt slightly by human body. Under vibration, it is appropriate that the interval between keys is 10 mm. The increase of mistakes and response time caused by vibration must be under suitable control. The result of this research is of some reference value to the ergonomics design and improvements of helicopter manipulating performance.