A system composition and operation method for towing an aircraft taxiing to a port
An operation method and aircraft technology, applied in the fields of instruments, data processing applications, calculations, etc., can solve the problems of high price of rodless tractors, inability to save fuel, and high maintenance costs, to avoid wrong roads and taxiing conflicts, safety Improve and reduce the effect of consumption
Inactive Publication Date: 2016-02-24
CIVIL AVIATION UNIV OF CHINA
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Problems solved by technology
The price of the rodless tractor is relatively high, and the maintenance cost is also relatively high
If only following the push operation process, the total number of rodless tractors required remains the same, but the relative cost is relatively high, which cannot make due contribution to the fuel saving of flight ground taxiing
Method used
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Embodiment Construction
[0037] The system composition and operation method for towing an aircraft taxiing to a port provided by the present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.
[0038] Such as figure 1 As shown, the system composition and operation method of the traction flight aircraft taxiing provided by the present invention include the following steps performed in order:
[0039] Step (1) Obtain fleet information: the user obtains the flight schedule from the airport operation management department through the network, and determines the required number of rodless tractors;
[0040] Step (2) Obtain aircraft type information: Obtain the aircraft type and total weight from the airport operation management department, so as to select and equip the corresponding rodless tractors, so that most aircraft have appropriate tractors to tow, and select the required type of rodless tractors. Rod tractor matches the aircraft;
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Provided is a composition and operation method for a system for towing arrival flight airplanes to slide. The composition and operation method comprises the steps that airplane team information is obtained; airplane type information is obtained; the number of towing vehicles is optimized, and the towing vehicles are combined; the towing vehicles are prepared according to the maximum airplane arrival peak value, and margins are sufficiently prepared and guaranteed; the rodless towing vehicles are used for towing the arrival airplanes. The system which is used for towing the arrival flight airplanes to slide and constructed through the composition and operation method for the system for towing the arrival flight airplanes to slide is composed of the rodless towing vehicles of the proper number and the flight airplanes, and a temporary rodless towing vehicle and airplane combined moving system is formed and used in round trips. Flight ground operation cost can be obviously lowered, ground aviation fuel consumption of the airplanes can be reduced, emission and noise can be reduced, the service quality of an airport can be improved, and the quality of air near a terminal building can be improved.
Description
technical field [0001] The invention belongs to the technical field of airport towing, and in particular relates to a system composition and an operation method for towing an aircraft taxiing to a port. Background technique [0002] (1) Existing technology: at present, all arriving flight planes taxi to the parking stand by themselves, which is a common method at present, and all airports are currently operating in this way. [0003] (2) Existing various types of fixed-wing aircraft, including turboprop aircraft, perform flights, including passenger transport and freight transport, all rely on their own engines as power to taxi to the parking position with idle power and speed, and the fuel consumption rate is average. 15 kilograms per minute, 5-15 minutes of gliding time does not wait, and this is current common practice, and its cost accounts for 1-2%, and the inventor thinks that this part expense can be saved. Fuel is consumed and carbon dioxide is emitted at the same t...
Claims
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IPC IPC(8): B64F1/10G06Q50/30
CPCY02T50/80
Inventor 赵文智杨亚坤曹书波王彬朱新华秦岩李晓津付涛
Owner CIVIL AVIATION UNIV OF CHINA