Patrol aircraft safety control system

A safety control and aircraft technology, applied in control/adjustment system, attitude control, non-electric variable control, etc., can solve the problems of aircraft equipment damage, low efficiency, economic loss, etc., and achieve the effect of preventing information leakage

Inactive Publication Date: 2016-11-16
天津津宇凯创航空科技发展有限公司
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  • Abstract
  • Description
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AI Technical Summary

Problems solved by technology

[0002] Inspection methods can be divided into manual inspection, manned helicopter inspection and aircraft inspection. Although manual inspection is the most commonly used inspection method, it has always had shortcomings such as slow efficiency and constraints of climate and geographical environment. Aircraft inspection is being widely researched and applied. , especially the high-efficiency feature of aircraft inspection, has more and more application value
At present, the inspection tasks for aerial vehicles are basically controlled by...

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Embodiment Construction

[0019] First of all, it should be noted that the specific structure, features and advantages of the present invention will be specifically described below by way of examples, but all descriptions are only for illustration, and should not be construed as forming any limitation on the present invention . In addition, any single technical feature described or implied in each embodiment mentioned herein, or any single technical feature shown or implied in each drawing, can still be described in these technical features (or their equivalents) ) to continue any combination or deletion, so as to obtain more other embodiments of the present invention that may not be directly mentioned herein. In addition, for the sake of simplifying the drawings, the same or similar technical features may only be marked in one place in the same drawing.

[0020] It will be understood that when a component is referred to as being "connected" to another component, it can be directly connected to the ot...

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Abstract

The invention relates to a patrol aircraft safety control system, which comprises a ground control device, an emergency air bag device, an aircraft and a main control chip and a slave control chip for controlling the aircraft, wherein the aircraft is provided with an image acquisition unit, a flight control unit, a wireless transmitting and receiving device and a memory electrically connected with the main control chip respectively; the ground control device comprises a wireless transmitting and receiving module, an aircraft remote control module and a flight path module; the aircraft is also provided with a speed sensor, a GPS positioning device, a six-axis inertial sensor and an ultrasonic sensor electrically connected with the input end of the slave control chip, and the output end of the slave control chip is electrically connected with a rotor control device, a speed reducing protection device, and a gas generating device. The aircraft can perform patrol automatically according to the made flight path, the aircraft reduces the speed once fault happens, the air bag can be ejected in time, and the process is safe and reliable.

Description

technical field [0001] The invention belongs to the field of aircraft safety control, in particular to a patrol aircraft safety control system. Background technique [0002] Inspection methods can be divided into manual inspection, manned helicopter inspection and aircraft inspection. Although manual inspection is the most commonly used inspection method, it has always had shortcomings such as slow efficiency and constraints of climate and geographical environment. Aircraft inspection is being widely researched and applied. , especially the high-efficiency feature of aircraft inspection, has more and more application value. At present, the inspection tasks for aerial vehicles are basically controlled by the ground personnel remotely and manually, which cannot be automatically operated, the efficiency is low, and it is difficult to apply to the real-time monitoring system. At the same time, the safety status of the aircraft in flight cannot be monitored. Once a failure occurs...

Claims

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Application Information

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IPC IPC(8): G05D1/08G05D1/10
CPCG05D1/0808G05D1/101
Inventor 陈鹏韩洁杰
Owner 天津津宇凯创航空科技发展有限公司
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