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airborne sounding aircraft

A technology for an aircraft and a steering gear, applied in the field of meteorological detection, can solve the problems such as the difficulty in realizing the organic combination of detection means, the different use conditions, and the difficulty in the coordinated use of detection means, so as to meet the requirements of detection and use, and reduce the influence and response of crosswinds. fast effect

Active Publication Date: 2015-04-15
湖北航天飞行器研究所
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  • Abstract
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AI Technical Summary

Problems solved by technology

In order to give full play to the advantages of the above-mentioned detection methods, foreign countries are currently using these methods comprehensively to detect typhoons, but the different conditions of use have caused difficulties in the coordinated use of various detection methods, and it is difficult to achieve an organic combination of detection methods. For this reason, effective measures should be taken. means to realize the systematic detection of typhoon

Method used

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Embodiment Construction

[0013] Below in conjunction with accompanying drawing and example the present invention is described in further detail.

[0014] Such as figure 1 As shown, the airborne sounding aircraft provided by the present invention comprises a pitot 1, a housing 2, a detection communication device 3, a lithium battery 4, a fuel tank 5, an autopilot 6, an air inlet 7, a turbojet engine 8, a rudder Machine 9, air rudder piece 10, folding airfoil 11 and lug 12.

[0015] The casing 2 forms a sealed cavity, and the front end of the sealed cavity is connected with the pitot tube 1 . The interior of the sealed chamber is divided into three compartments, in which the detection communication device 3 and the lithium battery 4 form the first compartment, the fuel tank 5 and the autopilot 6 form the second compartment, the air intake 7, the turbojet engine 8, the steering gear 9 constitute the third compartment. The outer surface of the second compartment is provided with folding airfoils. Lugs...

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Abstract

The invention discloses an airborne sounding aircraft, which comprises a casing, a pitot tube is arranged at the front end of the casing, a folding airfoil is arranged on the outer surface of the middle part of the casing, an air rudder plate and a steering gear are placed on the outer surface of the rear end of the casing The casing is provided with a detection communication device, a battery, a fuel tank, an autopilot and a turbojet engine, the detection communication device is electrically connected to a pitot tube, and the casing is also connected to an air intake. The invention can be mounted on a high-altitude and long-endurance drone, and the drone can be used to detect the wind speed, wind direction, temperature, pressure, and humidity data inside the typhoon, and use the drone as a relay platform to transmit the data back to the command center. Realize remote, fast, accurate, safe and flexible detection of typhoon.

Description

technical field [0001] The invention belongs to the field of meteorological detection, in particular to an airborne sounding aircraft used for typhoon detection. Background technique [0002] At present, the means of typhoon detection have their pertinence and limitations. Satellites and ground radars have the advantage of long detection distances, especially meteorological satellites, which can detect and detect typhoons at the beginning of their formation. However, it is difficult for satellite and radar monitoring to obtain data on the spatial structure and changes of typhoons, which greatly hinders the development of typhoons. The theoretical understanding of its structural changes and the changing laws of wind and rain distribution will have an impact on the improvement of typhoon forecasting. In this regard, developed countries use manned / unmanned aircraft to detect the wind, temperature, pressure, and humidity data inside the typhoon using GPS dropsondes, thereby inc...

Claims

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Application Information

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IPC IPC(8): G01W1/08F42B15/08
Inventor 雷明叶雷邹勇波李运生
Owner 湖北航天飞行器研究所
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