A method for measuring noise in an aircraft cabin
An aircraft cabin and noise technology, applied in the field of measuring the noise in the aircraft cabin, can solve the problems of huge cost investment, less raw data, and lag in research and development work, and achieve the effects of high measurement accuracy, lower experimental thresholds, and low test costs.
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Embodiment 1
[0020] A method for measuring noise in an aircraft cabin, characterized in that it comprises the following processes:
[0021] Miniature model production: Make a real aircraft into a scale model, and the scale of the model depends on the size of the wind tunnel.
[0022] Microphone layout: 6 microphones are arranged in the model cabin, and the equidistant arrays of microphones are distributed on the same spherical surface. The specific positions of the microphones in the model cabin are placed according to the parts where the noise needs to be measured.
[0023] Microphone model: 1 / 2-inch microphone 46AE from G.R.A.S; frequency: 3.15Hz (±2dB); dynamic response: 14dBA re.20μPa; sensitivity: 50mV / Pa (at 250Hz).
[0024] Noise detection: including cabin sound pressure level SPL before correction m and wind tunnel background noise sound pressure level SPLw;
[0025] Data correction: adopted Correction for the effect of wind tunnel background noise, SPL c is the corrected soun...
Embodiment 2
[0029] A method for measuring noise in an aircraft cabin, characterized in that it comprises the following processes:
[0030] Miniature model production: Make a real aircraft into a scale model, and the scale of the model depends on the size of the wind tunnel.
[0031] Microphone layout: Arrange 12 microphones in the model cabin, and the microphones are distributed in an equidistant array on the same spherical surface. The specific position of the microphone in the model cabin depends on the position where the noise needs to be measured.
[0032] Microphone model: 1 / 2-inch microphone 46AE from G.R.A.S; frequency: 20kHz (±2dB); dynamic response: 135dBA re.20μPa; sensitivity: 50mV / Pa (at 250Hz).
[0033] Noise detection: including cabin sound pressure level SPL before correction m and wind tunnel background noise sound pressure level SPLw;
[0034] Data correction: adopted Correction for the effect of wind tunnel background noise, SPL c is the corrected sound pressure lev...
experiment example
[0037] In the table, the noise value in the cabin of the aircraft measured in the wind tunnel and the noise value in the cabin of the aircraft in actual use are counted under different frequencies through the patented technology.
[0038] Frequency / HZ 200 500 1000 2000 5000 10000 Test / dB(A) 65.4 73.8 79.4 76.4 71.8 61.2 Measured / dB(A) 63.1 70.2 78.1 79.3 74.3 58.2
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