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Aircraft flight safety control method, safety control system and server

A safety control and aircraft technology, applied in the field of flight safety control of aircraft, can solve the problems of reduced reliability of aircraft, increased difficulty of aircraft, failure to meet low-cost commercial spaceborne models, etc.

Active Publication Date: 2019-09-27
BEIJING LANDSPACETECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Obviously, these additional devices will not only increase the difficulty of aircraft design, but also lead to reduced reliability and increased production costs of the aircraft, which cannot meet the requirements of low-cost, fast-cycle commercial space launch models

Method used

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  • Aircraft flight safety control method, safety control system and server
  • Aircraft flight safety control method, safety control system and server
  • Aircraft flight safety control method, safety control system and server

Examples

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Embodiment Construction

[0030] The technical solutions of the present invention will be further described below in conjunction with the accompanying drawings and through specific implementation methods. Spatially relative terms such as "below", "beneath", "under", "lower", "above", "on", "higher", etc. are used to facilitate description to explain the relative The orientation of two elements means that these terms are intended to encompass different orientations of the device in addition to orientations other than those shown in the figures. In addition, for example, "one element is on / under another element" may mean that two elements are in direct contact, or that there are other elements between the two elements. In addition, terms such as "first", "second", etc. are also used to describe various elements, regions, sections, etc. and should not be taken as limitations. Similar terms refer to similar elements throughout the description.

[0031]In the following, for the convenience of description,...

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PUM

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Abstract

The invention provides an aircraft flight safety control method and system and a server. The method comprises steps that a first safety threshold and a second safety threshold are set for at least oneflight parameter in the flight process of an aircraft; at least one flight parameter value of the aircraft in the flight process is acquired; safe operation is carried out based on the at least one flight parameter value, when the at least one flight parameter value is between the first safety threshold and the second safety threshold or equal to the second safety threshold, a blow-up system of the aircraft is released from insurance; when the at least one flight parameter value is greater than the second safety threshold, the blow-up system is made to blow up the aircraft. The method is advantaged in that through setting the safety range for the flight parameters of the aircraft in the flight process, the pipeline for guaranteeing the safe flight of the aircraft can be formed, so faultsof the flight process of the aircraft can be better handled and dealt with, and damage to ground facilities and personnel can be avoided.

Description

technical field [0001] The invention relates to the technical field of aircraft flight safety control, in particular to an aircraft flight safety control method, a safety control system and a server. Background technique [0002] During the flight of launch vehicles and other aircraft, failures of various systems may cause flight failures. Once rockets and other aircraft cannot fly normally due to malfunctions, they may fall from the sky at any time. If the location where the aircraft fails is just over a densely populated area, the wreckage of the rocket may endanger the safety of ground equipment or personnel, thereby causing serious launch accidents. [0003] Therefore, aircraft are often equipped with flight safety control systems. The function of the safety control system is to terminate the power flight of the aircraft and blow up the aircraft when the aircraft breaks down during the flight and the landing point will exceed the allowable range. [0004] In the exist...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05B23/02
Inventor 陈志愿王根荣邱靖宇赵鹏飞徐俊瑞郑然王泽宇华楠边九州康永来
Owner BEIJING LANDSPACETECH CO LTD
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