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Constitution method of departure flight traction taxiing system

A technology for flights and tractors, applied in control/adjustment systems, special data processing applications, instruments, etc., to solve the problems of towbar corrosion and fracture maintenance, high accident rate, and injury to maintenance personnel, so as to avoid the wrong way and taxiing. Conflict, total cost reduction, security enhancement effect

Inactive Publication Date: 2014-08-27
CIVIL AVIATION UNIV OF CHINA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, when performing pre-flight tasks, it is necessary to manually pull the towbar for loading and unloading, which is slow and has a relatively high accident rate
For example, it is prone to problems such as injury to the maintenance personnel, corrosion and fracture of the tow bar, and the need for maintenance.
Tractors with tow bars are not suitable for the operation and management needs of energy saving, emission reduction and cost reduction, but there is still a lack of barless towing and sliding systems

Method used

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  • Constitution method of departure flight traction taxiing system
  • Constitution method of departure flight traction taxiing system

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Embodiment Construction

[0035] The method for constructing the taxiing system for towing outbound flights provided by the present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0036] The method for forming the taxiing system of the towing outbound flight provided by the present invention includes the following steps performed in sequence:

[0037] Step 1. Obtain fleet information: obtain the flight schedule from the airport operation management department, and determine the flight departure time sequence within a day;

[0038] Step 2. Obtain aircraft type information: According to the obtained flight schedule, obtain the aircraft type and total weight from the airport operation management department, so as to select and equip corresponding wheel-holding rodless tractors; make most aircraft have appropriate tractors Drag and drop, select a variety of different types of tractors to match with the aircraft, and form a flight informa...

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Abstract

The invention provides a constitution method of a departure flight traction taxiing system. The constitution method comprises the steps of obtaining fleet information, obtaining model information, optimizing the combination of the number of tractors, supplying the number of the tractors according to the maximum peak of take-off flights, waiting for traction and the like. The constitution method of the departure flight traction taxiing system has the beneficial effects that flight delay can be well handled due to planning and system improvements, and the case that flights queue up in peak periods on a taxi track to waste fuel oil can be avoided. In addition, the view of the tractors is of 360 degrees so that air pilots can be prevented from going wrong and from taxiing collision, and therefore, the safety of the flights running on the ground can be improved.

Description

technical field [0001] The invention belongs to the technical field of airport traction, and in particular relates to a method for forming a taxiing system of a towing outbound flight. Background technique [0002] In existing airports, the track system is used for departing flight aircraft, which is a common method at present, and all airports are currently operating in this way. [0003] Existing fixed-wing aircraft of various models, including turboprop aircraft, perform flights, including passenger transport and cargo aircraft, all rely on their own engine power to taxi to the take-off waiting position with idle power and speed. During the taxiing process, the average fuel consumption rate is 15 kg per minute, and the taxiing time ranges from 5 to 30 minutes. This is a common practice at present. This part of the cost accounts for about 1-2% of the total cost. It not only consumes fuel, but also emits greenhouse gases such as carbon dioxide, which affects the environmen...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F17/30
CPCG05D1/0204
Inventor 赵文智袁晶晶李晓津王彬曹书波李国栋赵辉钮钦
Owner CIVIL AVIATION UNIV OF CHINA
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