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A Measurement Method for High Aspect Ratio Flexible Wing

A technology of flexible wings and measurement methods, applied in measuring devices, instruments, optical devices, etc., can solve the problems of high cost, incapable of real-time deformation monitoring of wings, and easy interference of sensor data, so as to achieve low cost, The effect of high measurement accuracy

Active Publication Date: 2015-10-21
CHINA ACAD OF AEROSPACE AERODYNAMICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Obviously this method is not suitable for large aspect ratio flexible wings
[0004] Another method is to use sensors to monitor the deformation of the wing. This method can obtain the deformation of the wing in real time, but it needs to arrange more sensors on the wing body, which is expensive, and the sensor data is easy to obtain during high-altitude flight. The real-time deformation of the wing cannot be visually monitored due to interference

Method used

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  • A Measurement Method for High Aspect Ratio Flexible Wing
  • A Measurement Method for High Aspect Ratio Flexible Wing
  • A Measurement Method for High Aspect Ratio Flexible Wing

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Embodiment Construction

[0023] Combine below figure 1 The flow diagram shown further describes the invention.

[0024] (1) Installation of camera device and layout of marking points

[0025] The invention utilizes a stereoscopic imaging device composed of two camera devices to perform stereoscopic imaging of aircraft wings. The camera device needs to be installed near the central axis of the top of the fuselage, and the fixed bracket is used for high installation. After the installation is completed, the photographic baseline is kept parallel to the center line of the fuselage. The distance between the camera and the fuselage is not less than 10cm in principle to ensure that the camera The imaging quality of directional photography enables the image to distinguish the marker points arranged to improve the accuracy of subsequent data processing. The form of the mark point can be as follows figure 2 shown.

[0026] In the present invention, the photography mode is upright photography, and the incl...

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Abstract

The invention discloses a measuring method for a high aspect ratio flexible wing, which comprises the steps that mark points are distributed on the surface of a wing zone that needs a deformation detection; two photographic devices are mounted at the top of an airframe of a plane; stereoscopic imaging is conducted for the wing by the two photographic devices in a flying process to acquire stereopairs; three-dimensional coordinates of the mark points in a local coordinate system are acquired through the stereopairs; and a deformation state of the wing is confirmed according to changes of the three-dimensional coordinates of the mark points in the local coordinate system. The measuring method overcomes the difficulty that the deformation of the high aspect ratio wing is difficult to monitor in real time, and realizes a quick and accurate acquisition of the deformation state of the wing.

Description

technical field [0001] The invention belongs to the field of aircraft flight status and parameter monitoring, and relates to a method for measuring a flexible wing with a large aspect ratio. Background technique [0002] Over the past ten years, more and more attention has been paid to high-altitude and long-endurance aircraft, and it has broad development prospects in military and civilian applications such as long-term reconnaissance and monitoring, environmental monitoring, and communication relay. This type of aircraft generally has the characteristics of large aspect ratio wings, light weight structure, and great flexibility. Under the action of flight load, the wings of large-aspect-ratio aircraft will produce large bending and torsional deformations. The real-time and high-precision measurement of the large deformation of such wings can be used to evaluate the performance of the aircraft, design and structure of the aircraft. research is of great significance. [00...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01B11/16
Inventor 陈文
Owner CHINA ACAD OF AEROSPACE AERODYNAMICS