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Wing test piece and processing method thereof

A test piece and wing technology, which is applied in the field of aircraft wing performance testing, can solve the problems of high production cost and high wing stiffness, achieve high flexibility, meet the needs of large deformation, and low processing cost

Active Publication Date: 2021-10-19
中电科芜湖通用航空产业技术研究院有限公司 +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Based on the problems of the above-mentioned background technology, the application provides a wing test piece, which solves the problems of high rigidity and high manufacturing cost of the finished wing

Method used

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  • Wing test piece and processing method thereof
  • Wing test piece and processing method thereof
  • Wing test piece and processing method thereof

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Embodiment Construction

[0027] The technical solutions of the present application are clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present application. Apparently, the described embodiments are part of the embodiments of the present application, not all of them. Based on the embodiments in this application, all other embodiments obtained by those skilled in the art without making creative efforts belong to the scope of protection of this application.

[0028] refer to figure 1 , is a wing test piece disclosed in the embodiment of the present application, including a spar 1 , a rib 2 , a skin 3 and an airfoil foam 4 . In order to show the internal structure of the wing test piece more clearly, figure 1 Part of the skin3 was removed from one end of the

[0029] refer to figure 1 and figure 2 , the section of the spar 1 is I-shaped, which includes an upper edge plate 11, a lower edge plate 12 and a web 13, the upper edge plate 11 and...

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Abstract

The invention relates to a wing test piece and a processing method thereof. The test piece comprises a spar which comprises an upper margin plate, a lower margin plate parallel to the upper margin plate, and a web plate vertically connected between the upper margin plate and the lower margin plate, wing ribs which comprise end ribs arranged at the two ends of the spar respectively and a plurality of middle ribs evenly distributed in the length direction of the spar, skin and wing-shaped foams, wherein the end ribs and the middle ribs are fixedly connected with the spar and are perpendicular to the spar; the skin wraps the outer sides of the spar and the wing ribs; the wing-shaped foams are a plurality of independent unit bodies and are respectively filled in each closed space formed by the spar, the wing ribs and the skin; the two ends of the spar respectively protrude out of the corresponding end ribs, and the first end of the spar is used for being connected with a test tool; and a first loading connector is arranged at the second end of the spar and used for being connected with a loading system. The wing test piece provided by the invention can meet the flexibility required by a deformation test, does not need to generate an additional mold, and has the advantage of low processing cost.

Description

technical field [0001] The present application relates to the technical field of aircraft wing performance detection, in particular to a wing test piece and a processing method thereof. Background technique [0002] The wings of the aircraft will bend and deform during flight, which may affect the safety status of the aircraft. Therefore, the deformation monitoring of the aircraft wings is very necessary, and the deformation monitoring of the aircraft wings is realized through sensors. When developing the deformation monitoring sensor, it is necessary to use the wing test piece as the basic platform for test verification. The sensor is pasted and fixed on the wing test piece, and the load is applied to deform the wing test piece. The shape of the test piece is monitored by the sensor. Variables, and then test and verify the performance of the sensor. [0003] At present, the wing test pieces used for deformation monitoring sensor testing mainly come from the wings of mature...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01B21/32G01M13/00
CPCG01B21/32G01M13/00Y02T50/40
Inventor 吕万韬冷崇富熊俊赵新新严飞石春森刘照琳
Owner 中电科芜湖通用航空产业技术研究院有限公司
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