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Wings adjustment

A technology for a wing and an adjustment system, applied to a computing unit and a program unit, a method for adjusting a wing, and the field of computer-readable media, which can solve problems such as misadjustment of the outer end of the wing

Active Publication Date: 2009-07-08
AIRBUS OPERATIONS GMBH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, a small misadjustment in the area where the fuselage meets the wing can cause a considerable misadjustment at the outer end of the wing

Method used

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Embodiment approach

[0046] According to another exemplary embodiment of the invention, when the lower end 106 of the probe is located in the middle of the opening 107, no further alignment of the wing has to be performed. If the lower end of the probe is not in the middle of the opening, move the carriage until the lower end of the probe is in the middle of the opening. Measure the corresponding distance traveled by the trolley. Alignment of the wing is then performed based on this measured distance, so that when the carriage is moved back to its original position, the lower end of the probe is now positioned in the middle of the opening.

[0047] Figure 4 An exemplary embodiment of the lower end 106 of the probe is shown. as from Figure 4 It can be seen that the lower end 106 of the test probe can be, for example, triangular, circular or oval, rectangular or any other shape. Additionally, the lower end 106 of the test probe may include a scale 301 .

[0048] Figure 5 An exemplary embodi...

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PUM

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Abstract

The present invention is one embodiment of regulating system for regulating the wings of airplane relatively to the fuselage. The regulating system is suitable for transmitting the position information of measuring points in the wings to the measuring unit, and the measuring unit measures the position information and applies the information for regulating wings.

Description

technical field [0001] The invention relates to the field of aircraft assembly. In particular, the invention relates to an adjustment system for adjusting an aircraft wing, and also to a method, a computer-readable medium, a computing unit and a program unit for adjusting an airfoil. Background technique [0002] In order to assemble an aircraft, the wings of the aircraft must be mounted on the fuselage of the aircraft. Thus, each wing is provided on a positioning unit adapted to move the wing onto the fuselage and to adjust the wing relative to the fuselage. This adjustment can be performed with the aid of positioning holes provided on the wings and fuselage. However, a small misadjustment in the area where the fuselage and wing join can result in a considerable misadjustment at the outer end of the wing. Contents of the invention [0003] It is an object of the present invention to provide an improved method for determining aircraft wing misadjustment. [0004] Accor...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64F5/00B23P21/00B64C1/26B64F5/10
Inventor 蒂埃里·哈尔鲍特伯努瓦·马尔盖
Owner AIRBUS OPERATIONS GMBH