Design method of engineered material arresting system of airfield runway

A technology for airport runways and characteristic materials, which is applied in the aviation field and can solve problems such as inapplicability and inapplicability of aircraft arresting systems.

Active Publication Date: 2014-01-01
CHINA ACAD OF CIVIL AVIATION SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, this method is mainly aimed at a single tire, and does not consider the mutual influence of each tire under the action of moving objects under the action of multiple tires, so it is not applicable to the design of an aircraft arresting system
[0005] When actua

Method used

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  • Design method of engineered material arresting system of airfield runway
  • Design method of engineered material arresting system of airfield runway
  • Design method of engineered material arresting system of airfield runway

Examples

Experimental program
Comparison scheme
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Example Embodiment

[0140] Example

[0141] Model A319, under the condition of maximum take-off weight, overruns the runway at a speed of 70kt. In the rear section, the main landing gear has brakes with a coefficient of friction of 0.25. Inside the arresting bed, without brakes. Ignore the aerodynamics of the aircraft during arrest. The initial arresting system follows figure 2 design.

[0142] 1. Quality characteristics of the aircraft of this embodiment

[0143] parameter name

[0144] aircraft maximum landing weight

[0145] 2. Airframe and Landing Gear Characteristics

[0146] parameter name

[0147] 3. The height of the engine from the ground

[0148] parameter name

[0149] 4. Mechanical properties of materials

[0150] strain = [0.05, 0.075, 0.1, 0.7, 0.725, 0.75, 0.775, 0.8, 0.825, 0.85];

[0151] Stress=1.0e6*[0.38278, 0.4006, 0.40844, 0.40844, 0.63406, 0.65841, 0.71686, 0.822761.0318, 1.4239]Pa

[0152] The simulation results obtain...

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Abstract

The invention provides a design method of an engineered material arresting system of an airfield runway. The design method includes confirming mechanical property of arresting materials according to mechanical property curve of the arresting materials, confirming force provided by the arresting materials on undercarriages at the moment according to depth of the arresting materials pressed by the undercarriages of a flight at the last moment, describing dynamic behaviour in vertical direction of the undercarriages according to kinetic simulation of shock struts of the undercarriages, confirming lift force, resistance and pitch moment on the flight at the moment through flight aerodynamic force simulation, confirming kinematic parameter of the flight through kinematic simulation of the flight, confirming stopping distance, flight kinematic parameter and force on the undercarriages by simulating until the flight shuts off, and judging whether to adjust an arresting system design scheme. On the basis of flight stopping distance, the design method is capable of accurately calculating loads on the undercarriages of the flight, so that safety of the undercarriages is convenient to evaluate in the arresting system design, and an arresting system design plan meeting requirements can be convenient to make.

Description

technical field [0001] The invention relates to a simulation method required for designing an aircraft arresting system, which is used in the design process of the characteristic material arresting system at the end of an airport runway to calculate the aircraft stop distance, aircraft motion parameters and the load on the landing gear, and belongs to the aviation category. Background technique [0002] The safety of aircraft landing gear is not only one of the symbols of aircraft safety, but also plays a decisive and important role in the effectiveness of the arresting system. Therefore, the safety assessment of landing gear is of great significance in the design of aircraft arresting system. [0003] Publication No. 100476072 of the Chinese patent "airport runway safety arresting system and its computer dynamic simulation method" disclosed an airport runway safety arresting system and its computer simulation method on October 25, 2006. This method is mainly based on the e...

Claims

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Application Information

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IPC IPC(8): G06F17/50
Inventor 姚红宇孔祥骏肖宪波史亚杰
Owner CHINA ACAD OF CIVIL AVIATION SCI & TECH
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