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Posture self-adaptive sonde catapult launching device and catapult launching method

A delivery device and radiosonde technology, applied in the field of meteorological detection, can solve the problems affecting the aerodynamic characteristics and flight quality of the aircraft, large wind resistance area, large cross-sectional area, etc.

Pending Publication Date: 2021-07-06
西安万新安全技术有限公司 +1
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  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to provide a kind of posture self-adaptive radiosonde ejection delivery device, has solved the ejection mechanism structural size that exists in the prior art to cause too large cross-sectional area to cause the wind resistance area to be too large, affecting aircraft (especially small The aerodynamic characteristics and flight quality of unmanned aerial vehicles)

Method used

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  • Posture self-adaptive sonde catapult launching device and catapult launching method
  • Posture self-adaptive sonde catapult launching device and catapult launching method
  • Posture self-adaptive sonde catapult launching device and catapult launching method

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Embodiment Construction

[0033] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0034] The present invention is an attitude self-adaptive radiosonde ejection device, such as figure 1 As shown, the pod mechanism 1 is included, the pod mechanism 1 includes a pod beam 102, one end of the lower side of the pod beam 102 is connected to the rear support 111, and the other end is connected to the front support 108, and the lower side of the pod beam 102 is located at the front support 108 and the rear A middle support 109 and a radiosonde ejection mechanism support 110 for connecting the radiosonde ejection mechanism 3 are also provided between the supports 111, and the front support 108 is connected to the radiosonde ejection controller 2 and the pod beam 102 through fasteners. The top is provided with a pod hanger 103 for connecting to the aircraft platform, and a first electrical connector 106 connected to the radiosonde eje...

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Abstract

The attitude-adaptive sonde ejection throwing device comprises a pod mechanism, one end of the pod mechanism is connected with a sonde ejection controller, the top of the inner side of the pod mechanism is connected with one end of an electric mechanism, and the other end of the electric mechanism is connected with a sonde ejection mechanism; the pod mechanism, the sonde ejection mechanism and the electric mechanism are connected with the sonde ejection controller through cables. The invention further discloses a launching method of the sonde catapult launching device, and the problems that in the prior art, due to the fact that the structural size of a catapult mechanism is too large, the cross section area is too large, the wind resistance area is too large, and the aerodynamic characteristic and the flight quality of an aircraft (especially a small unmanned aerial vehicle) are affected are solved.

Description

technical field [0001] The invention belongs to the technical field of meteorological detection, and relates to an attitude-adaptive radiosonde ejection delivery device, and also relates to the aforementioned radiosonde ejection delivery method. Background technique [0002] The airsonde is a kind of meteorological data such as air temperature, humidity, air pressure, wind direction, and wind speed from the launch platform to the ground / sea surface, which is based on platforms such as airships and aircraft (manned aircraft or drones). Weather detection equipment. [0003] In order to adapt to the existing aircraft platform, the airsonde delivery system generally realizes the connection with the aircraft platform by means of an external pod. The Chinese patent with the application number 201910812179.3 discloses a multi-barrel drop sonde ejection device, delivery device and delivery method. After the invention is energized through the electromagnet, the Z-shaped push rod mov...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D1/02B64D9/00G01W1/08
CPCB64D1/02B64D9/00G01W1/08Y02A90/10
Inventor 李花韩伟王成林
Owner 西安万新安全技术有限公司
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