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Measuring device for folding angle of wing

A measuring device and technology of wings, applied in the field of wings, can solve the problems of wing folding angle error, wing folding failure, stuck, etc., and achieve the effect of facilitating dynamic monitoring

Pending Publication Date: 2020-12-15
CHENGDU KANGTUO XINGYE TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Judging the wing folding situation by the approximate value of the wing folding angle, there will be errors in the judgment of the wing folding angle, resulting in failure or sticking of the wing folding

Method used

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  • Measuring device for folding angle of wing
  • Measuring device for folding angle of wing

Examples

Experimental program
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Embodiment

[0021] Such as figure 1 and figure 2 As shown, the device for measuring the folding angle of the wing 13 provided in this embodiment includes a mounting part 1, one side of the mounting part 1 is a clamping part 2, and the clamping part 2 is a C-shaped clamping part for clamping. Groove or U-shaped groove, the inner wall of the clamping part 2 matches the outer wall of the locking nut 12 on the folding rotating shaft 11 of the wing 13. The locking nut 12 in this embodiment is a hexagonal nut, and the clamping part 2 is directly clamped Connected to the outer wall of the lock nut 12, after the clamping, the clamping part 2 is fixed on the lock nut 12 by screws; the other side of the installation part 1 is the fixing plate 3 parallel to the clamping direction of the clamping part 2, and the fixing plate 3 is parallel to the side of the locking nut 12, and the clamping part 2 and the fixed plate 3 are connected and fixed by an arc-shaped plate, and the outer contour and inner c...

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Abstract

The invention discloses a measuring device for the folding angle of a wing. The measuring device comprises an installation part, one side of the installation part is a clamping part used for being connected and fixed with a wing folding rotating shaft, the other side of the installation part is a fixing plate, and the side, away from the installation part, of the fixing plate is equipped with an encoder; a measuring shaft of the encoder penetrates through the fixing plate and is located on the side, close to the installation part, of the fixing plate; a connecting arm is fixedly connected withthe measuring shaft of the encoder in a sleeving mode, and an adjusting plate is connected with the end, away from the encoder, of the connecting arm; and a wing surface connecting plate attached toa wing surface of a movable wing surface is arranged on the adjusting plate. According to the measuring device for wing folding angle, after installation, the wing surface connecting plate is ensuredto be attached to the surface of the wing, so that the wing drives the wing surface connecting plate to rotate in the folding process, a wing surface rotating plate drives the measuring shaft of the encoder to rotate through the connecting arm, thus the purpose of accurately measuring the folding angle of the wing is achieved through the encoder, and subsequent dynamic monitoring of wing folding can be realized conveniently.

Description

technical field [0001] The invention belongs to the technical field of wings, and in particular relates to a measuring device for wing folding angles. Background technique [0002] At present, due to the flight requirements of large unmanned aerial vehicles or fixed-wing aircraft, their wings are designed to be very long, and they occupy a large area when parked on ships. Therefore, large fixed-wing aircraft or long-wing aircraft parked on ships UAVs need to fold the wings after docking. The wings need to be folded accurately to the corresponding station before they can be locked and fixed. If there is an error in the wing folding angle, it will cause The wing is stuck or the wing lock fails. [0003] The wing folding process of the existing large fixed-wing aircraft or long-wing-span UAV is realized through the movement of the actuator on the wing under the action of hydraulic pressure, and the folding angle of the wing is currently also based on the actuating It is calcu...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D45/00B64F5/60
CPCB64D45/0005B64F5/60B64U10/25
Inventor 杜波周锐程志
Owner CHENGDU KANGTUO XINGYE TECH CO LTD
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