公开(公告)号：US20140231592A1

公开(公告)日：2014-08-21

申请号：US14232247

申请日：2012-07-06

Applicant: Simon Topping ,  Christopher Payne ,  Llifon Williams ,  Martin Mayneord ,  David Belfourd ,  Xavier Hue

Inventor： Simon Topping ,  Christopher Payne ,  Llifon Williams ,  Martin Mayneord ,  David Belfourd ,  Xavier Hue

IPC: B64C13/34

CPC classification number: B64C13/34 ,  B64C9/02 ,  B64C9/22

Abstract: 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.

Abstract translation: 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。

公开(公告)号：US20120181730A1

公开(公告)日：2012-07-19

申请号：US13426130

申请日：2012-03-21

Applicant: Martin Edwards ,  Risto Kallinen ,  Simon Topping

Inventor： Martin Edwards ,  Risto Kallinen ,  Simon Topping

IPC: B06B1/10 ,  B29C67/00

CPC classification number: B23B51/0413 ,  B23B47/34 ,  B23B49/026 ,  B23B2226/27 ,  B23B2251/087 ,  B23B2270/62 ,  B23Q11/0046 ,  B26F1/16 ,  B26F1/32 ,  B26F1/3846 ,  Y10T408/03 ,  Y10T408/44 ,  Y10T408/892 ,  Y10T408/8953 ,  Y10T408/909

Abstract: A cutting tool has: a rotatable hollow tube with an inlet at a distal end of the tube and a cutting edge at the perimeter of the inlet, the tube being arranged so as to rotate when in use so as to cut a work piece with the cutting edge; and an auger housed within the hollow tube, the auger being arranged so as to rotate when in use so as to feed cut material from the inlet along the hollow tube, wherein a distal end of the auger is set back from the cutting edge of the tube.

Abstract translation: 切割工具具有：可旋转的中空管，其具有在管的远端处的入口和在入口的周边处的切割边缘，所述管被布置成在使用时旋转，以便在其中切割工件 前沿; 以及容纳在所述中空管内的螺旋推运器，所述螺旋推运器布置成在使用时旋转，以沿着所述中空管从所述入口供给切割材料，其中所述螺旋钻的远端从所述中空管的切割边缘 管。

公开(公告)号：US20090269152A1

公开(公告)日：2009-10-29

申请号：US12415101

申请日：2009-03-31

Applicant: Martin EDWARDS ,  Risto KALLINEN ,  Simon TOPPING

Inventor： Martin EDWARDS ,  Risto KALLINEN ,  Simon TOPPING

IPC: B23B51/08

CPC classification number: B23B51/0413 ,  B23B47/34 ,  B23B49/026 ,  B23B2226/27 ,  B23B2251/087 ,  B23B2270/62 ,  B23Q11/0046 ,  B26F1/16 ,  B26F1/32 ,  B26F1/3846 ,  Y10T408/03 ,  Y10T408/44 ,  Y10T408/892 ,  Y10T408/8953 ,  Y10T408/909

Abstract: A cutting tool comprising: a rotatable hollow tube with an inlet at a distal end of the tube and a cutting edge at the perimeter of the inlet, the tube being arranged so as to rotate when in use so as to cut a work piece with the cutting edge; and an auger housed within the hollow tube, the auger being arranged so as to rotate when in use so as to feed cut material from the inlet along the hollow tube, wherein a distal end of the auger is set back from the cutting edge of the tube.A method of drilling a hole in a dry fibre assembly, the method comprising engaging the dry fibre assembly with a cutting tool comprising a hollow tube with an inlet at a distal end of the tube and a cutting edge at the perimeter of the inlet; and rotating the hollow tube so as to cut the dry fibre assembly with the cutting edge.

Abstract translation: 一种切割工具，包括：可旋转中空管，其具有在所述管的远端处的入口和在所述入口的周边处的切割边缘，所述管被布置成在使用时旋转，以便在所述管中切割工件 前沿; 以及容纳在所述中空管内的螺旋推运器，所述螺旋推运器布置成在使用时旋转，以沿着所述中空管从所述入口供给切割材料，其中所述螺旋钻的远端从所述中空管的切割边缘 管。 一种在干纤维集合体中钻孔的方法，所述方法包括使干纤维组件与包括中空管的切割工具接合，所述中空管具有在所述管的远端处的入口和在所述入口的周边处的切割边缘; 并旋转中空管，以便用切割刃切割干纤维组件。

公开(公告)号：US09169000B2

公开(公告)日：2015-10-27

申请号：US14232247

申请日：2012-07-06

Applicant: Simon Topping ,  Christopher Payne ,  Llifon Williams ,  Martin Mayneord ,  David Belfourd ,  Xavier Hue

Inventor： Simon Topping ,  Christopher Payne ,  Llifon Williams ,  Martin Mayneord ,  David Belfourd ,  Xavier Hue

IPC: B64C13/34 ,  B64C9/02 ,  B64C9/22

CPC classification number: B64C13/34 ,  B64C9/02 ,  B64C9/22

Abstract: 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.

Abstract translation: 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。