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Aircraft noise monitoring method and device thereof

A technology of aircraft noise and aircraft, which is applied in the field of aircraft noise monitoring methods and devices, and can solve the problems of inability to objectively and accurately evaluate the impact of aircraft noise and noise

Inactive Publication Date: 2017-06-13
INST OF RADAR & ELECTRONICS CONFRONTATION ARMY AIR FORCE EQUIP RES INST OF PLA +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

This method can alleviate the problem that the traditional aircraft procedure noise monitoring method is accidental and cannot objectively and accurately evaluate the noise impact caused by aircraft noise.

Method used

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  • Aircraft noise monitoring method and device thereof
  • Aircraft noise monitoring method and device thereof
  • Aircraft noise monitoring method and device thereof

Examples

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no. 1 example

[0026] Please refer to figure 2 , figure 2 It is a flowchart of an aircraft noise monitoring method provided by the first embodiment of the present invention. The following will be figure 2 The process shown is described in detail, and the method includes:

[0027] Step S110: Obtain flight parameters and actual meteorological data of the aircraft in the monitoring environment. The flight parameters include aircraft type, engine power, and airport runway information. The actual meteorological data include air pressure, air temperature, relative humidity, and wind speed.

[0028] According to the regulations of ICAO (International Civil Aviation Organization), the meteorological conditions for airport noise measurement are: pressure value 1013.25 hPa, temperature 25 degrees Celsius, relative humidity 70% and no wind. However, the meteorological conditions of the airport are usually difficult to meet this standard. In actual measurement, the temperature value is 2 degrees Cel...

no. 2 example

[0051] Please refer to Figure 4 , Figure 4 It is a flowchart of an aircraft noise monitoring method provided by the second embodiment of the present invention. The following will be Figure 4 The process shown is described in detail, and the method includes:

[0052] Step S210: Obtain flight parameters and actual meteorological data of the aircraft in the monitoring environment. The flight parameters include aircraft type, engine power, and airport runway information. The actual meteorological data include air pressure, air temperature, relative humidity, and wind speed.

[0053] Step S220: Correct the flight track of the aircraft type on the airport runway based on the pre-saved broadcast and climb rules, the flight parameters and actual weather data.

[0054] Step S230: Obtain a random prediction point, and calculate the slant distance between the aircraft of the type and the random prediction point on the airport runway based on the corrected flight track.

[0055] St...

no. 3 example

[0061] Please refer to Figure 5 , Figure 5 It is a structural block diagram of an aircraft noise monitoring device provided by the third embodiment of the present invention. The following will be Figure 5 The illustrated structural block diagram is for illustration, and the illustrated apparatus 400 includes: an acquisition module 410 , a correction module 420 , a first calculation module 430 , a second calculation module 440 , a third calculation module 450 and a fourth calculation module 460 .

[0062] The obtaining module 410 is used to obtain flight parameters and actual meteorological data of the aircraft in the monitoring environment. The flight parameters include aircraft type, engine power, airport runway information, and the actual meteorological data include air pressure, air temperature, relative humidity and wind speed.

[0063] The correction module 420 is configured to correct the flight track of the aircraft type on the airport runway based on the pre-saved...

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Abstract

The invention provides an aircraft noise monitoring method and device. The method comprises the following steps of acquiring flight parameters and actual meteorological data of an aircraft in the monitoring environment, correcting a flight path of the aircraft at an airfield runway, acquiring a random predicted point, calculating a slant range between the aircraft and the random predicted point, calculating and obtaining effective perceived noise levels of the aircraft based on the maximum takeoff weight and the slant range of the aircraft, based on takeoff and landing aircraft times of each type aircraft obtained in advance at each airfield runway in a first period, calculating average values of the effective perceived noise levels of the aircraft, calculating and obtaining weighted equivalent continuous perceive noise levels based on takeoff and landing aircraft times of the aircraft in each second period and the average values of the effective perceived noise levels, a plurality of second periods are obtained in advance in the first period. By adopting the method, the problems that a traditional aircraft program noise monitoring method is accidental and can not evaluate the noise impact caused by aircraft noise objectively and accurately can be alleviated.

Description

technical field [0001] The invention relates to the field of noise monitoring, in particular to an aircraft noise monitoring method and device thereof. Background technique [0002] With the rapid growth of flight volume and the increase of new airport construction and airport expansion projects, the problem of aviation noise at airports has become increasingly prominent. The evaluation of aircraft should not only consider safety, economy and simplicity, but also pay attention to noise evaluation. Traditional aircraft noise monitoring methods mainly use the noise of a single event as an evaluation index, which is accidental and cannot objectively and accurately evaluate the noise impact of aircraft noise. Contents of the invention [0003] In view of this, the purpose of the embodiments of the present invention is to provide an aircraft noise monitoring method and device thereof. [0004] In the first aspect, an embodiment of the present invention provides a method for m...

Claims

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Application Information

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IPC IPC(8): G01H17/00G01D21/02
CPCG01H17/00G01D21/02
Inventor 李海峰李静朱永文王长春周臣唐治理付莹
Owner INST OF RADAR & ELECTRONICS CONFRONTATION ARMY AIR FORCE EQUIP RES INST OF PLA
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