Intelligent monitoring method for airplane heavy landing

A technology of intelligent monitoring and heavy landing, applied in aircraft parts, ground installations, transportation and packaging, etc., can solve the problems of manpower and material resources, time-consuming, unscheduled flight test and field training, etc., to improve work efficiency and accuracy. High, reduce the effect of manual data analysis time

Inactive Publication Date: 2016-08-31
XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
View PDF6 Cites 7 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the sinking speed of the aircraft is not easy to measure accurately. Usually, it is only based on the landing weight to determine whether to carry out the overload inspection, which requires a large amount of data analysis after the flight.
However, judging only by the weight of the aircraft will add a lot of additional inspection items that are not actually necessary, and consume a lot of manpower and material resources.
For example, after a key model modified aircraft in China is equipped with a new type of guided weapon, its landing weight has exceeded the design landing weight. According to the existing treatment method, overload inspection and maintenance can only be carried out after each landing. The load exceeding the structural use accounted for only a small part, which caused some unnecessary work to be carried out and took up a lot of time, resulting in the failure of its test flight and field training to be carried out on schedule

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Intelligent monitoring method for airplane heavy landing
  • Intelligent monitoring method for airplane heavy landing

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0020] In order to make the objectives, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be described in more detail below in conjunction with the drawings in the embodiments of the present invention. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the invention. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention. Embodiments of the present invention will be described in detail b...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

PUM

No PUM Login to view more

Abstract

The invention relates to an intelligent monitoring method for airplane heavy landing. The method includes the steps that firstly, according to the characteristics of an airplane, the relationship between the airplane flight parameter and the airplane structure bearing parameter is obtained through analysis, wherein the airplane flight parameter comprises the sinking speed, and the airplane structure bearing parameter comprises the airplane landing weight; secondly, the overload judgment parameters and a threshold value are determined, wherein the overload judgment parameters comprise the airplane landing design weight and the maximum landing weight; and thirdly, a landing diagnostic model is established and judges whether the airplane landing process is a landing overload process or not. By the adoption of the intelligent monitoring method for airplane heavy landing, whether the airplane landing process is a heavy landing process or not can be effectively judged, an effective early warning can be given, the manual data analysis time and the unnecessary overhaul and maintenance time are greatly shortened, the work efficiency is improved, and accuracy is high.

Description

technical field [0001] The invention belongs to the field of aircraft maintenance design, in particular to an intelligent monitoring method for heavy landing of an aircraft. Background technique [0002] Foreign countries have been involved in early warning of overloaded landings. For example, most aircraft of Boeing and Airbus have flight quality monitoring systems, which include the monitoring of heavy landings. According to the report of the FAA (Federal Aviation Administration, the full name is the Federal Aviation Administration of the United States), through the monitoring of the heavy landing event, the inspection of the heavy landing of the aircraft is reduced, the safety level is improved, and the maintenance time and cost are saved at the same time. China started relatively late in the field of overload landing warning. Although there are relevant theoretical studies, no domestically-made aircraft has truly realized overload landing monitoring. In addition to the c...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

Application Information

Patent Timeline
no application Login to view more
Patent Type & Authority Applications(China)
IPC IPC(8): B64F5/00
CPCB64F5/00
Inventor 华卫江杨小斌陈全礼刘希美
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products