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1. 发明申请

US20140231592A1 LEADING EDGE RIB ASSEMBLY 有权
标题翻译：领先的边框总成
公开(公告)号：US20140231592A1
公开(公告)日：2014-08-21
申请号：US14232247
申请日：2012-07-06
申请人： Simon Topping , Christopher Payne , Llifon Williams , Martin Mayneord , David Belfourd , Xavier Hue
发明人： Simon Topping , Christopher Payne , Llifon Williams , Martin Mayneord , David Belfourd , Xavier Hue
IPC分类号： B64C13/34
CPC分类号： B64C13/34 , B64C9/02 , B64C9/22
摘要： An aircraft wing comprising a main wing element with a spar and a leading edge rib which is supported by the spar and extends forward of the spar; a high lift device which is movably mounted to the main wing element; and an actuation mechanism comprising a drive shaft and a gear train. The gear train comprising a drive cog which is carried by the drive shaft, an actuator cog which is coupled to the high lift device, and one or more intermediate cogs which are mounted to the rib and coupled in series with the drive cog and the actuator cog so as to transmit torque from the drive cog to the actuator cog which moves the high lift device between a retracted position and an extended position in which the high lift device increases the camber of the wing. The sizes of the cogs in the gear train are selected so that the drive shaft rotates at a higher rate than the high lift device.
摘要翻译：一种飞机机翼，包括具有翼梁的主翼元件和由翼梁支撑并延伸到翼梁前方的前缘肋骨; 可移动地安装到主翼元件的高升降装置; 以及包括驱动轴和齿轮系的致动机构。齿轮系包括由驱动轴承载的驱动齿轮，联接到高提升装置的致动器齿轮和一个或多个中间齿轮，其安装到肋并与驱动齿轮串联连接，并且致动器齿轮，以便将扭矩从驱动齿轮传递到致动器齿轮，致动器齿轮使高升程装置在缩回位置和伸出位置之间移动，在该位置，高升程装置增加机翼的弯度。选择齿轮系中的齿轮的尺寸，使得驱动轴以比高提升装置更高的速度旋转。

2. 发明授权

US09169000B2 Leading edge rib assembly 有权
标题翻译：前缘肋组件
公开(公告)号：US09169000B2
公开(公告)日：2015-10-27
申请号：US14232247
申请日：2012-07-06
申请人： Simon Topping , Christopher Payne , Llifon Williams , Martin Mayneord , David Belfourd , Xavier Hue
发明人： Simon Topping , Christopher Payne , Llifon Williams , Martin Mayneord , David Belfourd , Xavier Hue
IPC分类号： B64C13/34 , B64C9/02 , B64C9/22
CPC分类号： B64C13/34 , B64C9/02 , B64C9/22
摘要： An aircraft wing has a main wing element with a spar and a leading edge rib supported by the spar, a high lift device movably mounted to the main wing element, and an actuation mechanism with a drive shaft and a gear train. The gear train has a drive cog carried by the drive shaft, an actuator cog coupled to the high lift device, and one or more intermediate cogs mounted to the rib and coupled in series with the drive cog and the actuator cog so as to transmit torque from the drive cog to the actuator cog which moves the high lift device between a retracted position and an extended position in which the high lift device increases the camber of the wing. Sizes of the cogs in the gear train are selected so that the drive shaft rotates at a higher rate than the high lift device.
摘要翻译：飞机机翼具有带翼梁的主翼元件和由翼梁支撑的前缘肋，可移动地安装到主翼元件的高升降装置以及具有驱动轴和齿轮系的致动机构。齿轮系具有由驱动轴承载的驱动齿轮，联接到高提升装置的致动器齿轮和安装到肋上并与驱动齿轮和致动器齿轮串联耦合的一个或多个中间齿轮，以便传递扭矩从驱动齿轮到致动器齿轮，该致动器齿轮在缩回位置和伸出位置之间移动高升程装置，在该位置，高升力装置增加机翼的外倾角。选择齿轮系中的齿轮的尺寸，使得驱动轴以比高举升装置更高的速度旋转。

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