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Airborne information launching system

A technology of information transmission and signal transmission, applied in transmission systems, aircraft parts, electrical components, etc., can solve problems such as difficulty in finding the exact location of the aircraft, and falling into the seabed, so as to reduce the casualty rate, improve the efficiency of search and rescue, The effect of reducing search and rescue costs

Inactive Publication Date: 2014-06-18
盖志武
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The purpose of the present invention is to solve the problem that existing existing aircraft position monitoring devices or aircraft communication systems are easily turned off by criminals and become invalid when hijacking occurs, and when an aircraft crash occurs, they are easy to fall into the seabed together with the aircraft and are difficult to find, or Because the signal transmission cycle is too long, it is difficult to determine the exact position of the aircraft. It can help relevant departments to track the position of the aircraft in real time, quickly and accurately locate the crashed or lost contact aircraft, significantly improve the efficiency of search and rescue, reduce the cost of search and rescue, and reduce the casualty rate

Method used

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Examples

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Embodiment Construction

[0011] like figure 1 , figure 2 and image 3 As shown, the airborne information transmitting system of the present invention includes an aircraft body 1, an aircraft power supply system 2, and an aircraft empennage 4. The airborne information transmitting system also includes a wire 3, a signal transmitting device 5, an electromagnet 6, a battery 8, and a power supply Line 9, wireless signal transmitting module 10, first steel plate 7, second steel plate 11; electromagnet 6 is installed in the top casing of the aircraft, the electromagnet 6 is close to the front of the aircraft empennage 4, and the wire 3 is connected to the electromagnet 6 and the aircraft power supply System 2; battery 8, power cord 9 and wireless signal transmitting module 10 are installed inside signal transmitting device 5, battery 8 and wireless signal transmitting module 10 are connected by power cord 9, first steel plate 7 is embedded in the shell bottom of signal transmitting device 5 and the secon...

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PUM

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Abstract

Disclosed is an airborne information launching system. The airborne information launching system is mounted at the tail of an aircraft, a power supply in the aircraft is used at the front end of an empennage, and a built-in independent battery is arranged. Due to the facet that the system is mounted outside a cabin, personnel in the cabin cannot shut down the system, wireless signals are periodically sent outwards in real time, the system can be automatically separated from an airframe of the aircraft and continue working independently when aircraft accidents happen or the aircraft breaks down, and the system can float on water. The problems that an existing aircraft position monitor device or a communication system is easily shut down by criminals and loses efficacy when the aircraft is hijacked or a black box falls into a water bottom and cannot be found are effectively solved. Relevant departments can be helped to track the position of the aircraft in real time, the wrecked aircraft or the aircraft with contact lost can be located accurately, search and rescue efficiency is obviously improved, and casualties are reduced.

Description

technical field [0001] The invention relates to an airborne information transmission system, which automatically sends wireless signals to the outside at regular intervals, and can automatically leave the aircraft body to continue working after an aircraft crash, so as to meet the needs of relevant departments when the aircraft fails or crashes. Finally determine the aircraft position or flight trajectory requirements. Background technique [0002] With the increasing popularity of civil aviation airliners or civil aircraft, the flight safety issues have become increasingly prominent. Since its flight route and altitude are not fixed, they will change at any time during the flight. In order to ensure the flight safety of the air target and prevent the collision of the air target, especially to determine the position of the aircraft as soon as possible after the crash, the flight situation, It is very necessary to independently monitor and determine the flight trajectory and...

Claims

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Application Information

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IPC IPC(8): H04B1/04B64D47/02
Inventor 盖志武
Owner 盖志武
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