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A device for collecting aircraft shipping performance information

A technology of collecting device and aircraft, applied in the field of aircraft, can solve the problems of difficult multi-point shooting and lowering of image recognition accuracy, and achieve the effect of improving clarity and accuracy

Active Publication Date: 2021-12-03
WUHAN UNIV OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Local governments such as prefectures, defense ministries, airport management agencies, etc. sometimes monitor aircraft passing through a specific route, and collect flight performance information of aircraft passing through the route, and the collector can intercept the transponder response sent from the aircraft Signal waves and other identification waves, and identify the aircraft type based on the intercepted identification waves, and at the same time monitor the camera to take pictures, and identify the flying object from the captured images. In the process, the existing collectors in When shooting, it is difficult to take multi-point shooting, which reduces the accuracy of image recognition. Therefore, corresponding improvements are made for this problem

Method used

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  • A device for collecting aircraft shipping performance information
  • A device for collecting aircraft shipping performance information
  • A device for collecting aircraft shipping performance information

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0028] refer to Figure 1-6 , a collection device for aircraft shipping performance information, comprising a base plate 1, a first groove 2 is provided on the top of the base plate 1, a first chute 3 is provided on the inner wall at both ends of the first groove 2, and the first chute 3 slides The first slider 4 is connected, and the same first slider 5 is fixed by bolts between the two first sliders 4. The top of the first slider 5 is fixed with the collector body 6 by bolts, and the first groove 2 is a The side inner wall is provided with a mounting groove 7, and a motor 8 is fixed by a bolt in the mounting groove 7, and the output shaft of the motor 8 is connected with a screw rod 9, and the screw rod 9 and the first sliding seat 5 are connected through threads, and the bottom of the inner wall of the first groove 2 is provided with multiple Evenly distributed second grooves 10, the inner walls of both sides of the second groove 10 are provided with second sliding grooves ...

Embodiment 2

[0034] refer to Figure 1-7 , a collection device for aircraft shipping performance information, the rear end of the lens groove 17 is rotatably connected with a waterproof cylinder 27 through a bearing, and the outer wall of the waterproof cylinder 27 is fixed with a plurality of air-inducing plates 28 distributed in an annular array by bolts, and the cross-section of the air-inducing plate 28 is Set into a wedge shape.

[0035] Furthermore, the front end of the air-inducing plate 28 is provided with a plurality of resistance increasing grooves 29, the section of the resistance increasing grooves 29 is V-shaped, and the multiple resistance increasing grooves 29 are set to become smaller from the inside to the outside.

[0036] During use, the waterproof tube 27 can prolong the distance between the first eyeglass 18 and the outside, thereby effectively preventing rainwater from splashing onto the first eyeglass 18 when it rains. The rotation of the waterproof cylinder 27 can ...

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Abstract

The present invention belongs to the technical field of aircraft, in particular to a collection device for aircraft shipping performance information. Aiming at the problem of low identification degree of existing devices, the following scheme is proposed, including a bottom plate, a first groove is opened on the top of the bottom plate, and the first The inner walls at both ends of the groove are provided with a first chute, the first slider is slidably connected to the first slider, the first sliding seat is fixed between the two first sliders, and the inner wall on one side of the first groove is provided with a The installation groove, the motor is fixed in the installation groove, the output shaft of the motor is connected with the screw rod, the bottom of the inner wall of the first groove is provided with a plurality of second grooves, and the inner walls on both sides of the second groove are provided with second slide grooves. A second sliding block is slidably connected in the groove, and a clamping block is fixed on the top of the second sliding seat. In the present invention, the first sliding seat moves above the clamping block, the clamping block moves downward, the electrode sheets are in contact, the circuit is connected, and the camera shoots, so as to achieve the effect of multi-point shooting, thereby improving the accuracy of later image recognition.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to a collection device for aircraft shipping performance information. Background technique [0002] Aircraft refers to aircraft flying in the atmosphere. Including airplanes, airships, balloons and any other objects that can fly in the atmosphere by the reaction force of the air. Aircraft must overcome various resistances in the air before they can fly, and various meteorological conditions and aerodynamic forces in the atmosphere have various effects on aircraft flight. Aircraft are divided into two categories according to the different ways of obtaining lift. One is lighter-than-air aircraft, which rely on the buoyancy of the air to float in the air, such as balloons, airships, etc.; the other is heavier-than-air aircraft, including non-powered vehicles. And power drive two types. [0003] Local governments such as prefectures, defense ministries, airport management agencies, ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H04N5/225H04N7/18
CPCH04N7/18H04N23/50
Inventor 陈宣佑郑凯
Owner WUHAN UNIV OF TECH