JPH0246500U - - Google Patents

Info

Publication number
JPH0246500U
JPH0246500U JP12595288U JP12595288U JPH0246500U JP H0246500 U JPH0246500 U JP H0246500U JP 12595288 U JP12595288 U JP 12595288U JP 12595288 U JP12595288 U JP 12595288U JP H0246500 U JPH0246500 U JP H0246500U
Authority
JP
Japan
Prior art keywords
noise
aircraft noise
microphones
aircraft
pair
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP12595288U
Other languages
Japanese (ja)
Other versions
JP2505964Y2 (en
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed filed Critical
Priority to JP1988125952U priority Critical patent/JP2505964Y2/en
Publication of JPH0246500U publication Critical patent/JPH0246500U/ja
Application granted granted Critical
Publication of JP2505964Y2 publication Critical patent/JP2505964Y2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Landscapes

  • Obtaining Desirable Characteristics In Audible-Bandwidth Transducers (AREA)
  • Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)

Description

【図面の簡単な説明】[Brief explanation of drawings]

第1図及び第2図は本考案によるマイクロホン
装置の一実施例を示す側面図及び平面図、第3図
はその遮蔽体の詳細構成を示す拡大縦断面図、第
4図は第1図の航空機騒音判別回路31の詳細構
成を示すブロツク図、第5図は第4図の差分検出
回路の差分演算動作の説明に供する信号波形図、
第6図は実験結果として第4図のモニタ37上の
信号波形画像を示す略線図、第7図は上側及び下
側マイクロホンに到来する航空機騒音成分の説明
に供する略線図、第8図は従来の場合のモニタ画
面上の信号波形画像を示す略線図、第9図及び第
10図は本考案の他の実施例を示す断面図、第1
1図は従来のマイクロホン装置を示す略線的側面
図、第12図は第11図のマイクロホン装置に到
来する航空機騒音の説明に供する略線図である。 11…マイクロホン装置、13…主柱、15…
上側マイクロホン、16,25…防風スクリーン
、22…下側マイクロホン、24…遮蔽体、31
…航空機騒音判別回路、37…モニタ。
1 and 2 are a side view and a plan view showing one embodiment of the microphone device according to the present invention, FIG. 3 is an enlarged vertical cross-sectional view showing the detailed structure of the shielding body, and FIG. 4 is the same as that shown in FIG. 1. A block diagram showing the detailed configuration of the aircraft noise discriminating circuit 31; FIG. 5 is a signal waveform diagram for explaining the difference calculation operation of the difference detection circuit in FIG. 4;
FIG. 6 is a schematic diagram showing the signal waveform image on the monitor 37 in FIG. 4 as an experimental result, FIG. 7 is a schematic diagram for explaining the aircraft noise components arriving at the upper and lower microphones, and FIG. 9 and 10 are cross-sectional views showing other embodiments of the present invention.
FIG. 1 is a schematic side view showing a conventional microphone device, and FIG. 12 is a schematic diagram for explaining aircraft noise arriving at the microphone device of FIG. 11. 11...Microphone device, 13...Main pillar, 15...
Upper microphone, 16, 25... Windproof screen, 22... Lower microphone, 24... Shielding body, 31
...Aircraft noise discrimination circuit, 37...Monitor.

Claims (1)

【実用新案登録請求の範囲】 一対のマイクロホンから得られる騒音検出信号
に基づいて受音した騒音から航空機騒音を識別す
る航空機騒音識別装置において、 上記一対のマイクロホンの一方又は両方に反射
航空機騒音を遮音する遮蔽体を設けた ことを特徴とするマイクロホン装置。
[Scope of Claim for Utility Model Registration] In an aircraft noise identification device that identifies aircraft noise from received noise based on noise detection signals obtained from a pair of microphones, one or both of the pair of microphones is provided with reflected aircraft noise. What is claimed is: 1. A microphone device characterized by being provided with a shielding body.
JP1988125952U 1988-09-27 1988-09-27 Aircraft noise identification device Expired - Lifetime JP2505964Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1988125952U JP2505964Y2 (en) 1988-09-27 1988-09-27 Aircraft noise identification device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1988125952U JP2505964Y2 (en) 1988-09-27 1988-09-27 Aircraft noise identification device

Publications (2)

Publication Number Publication Date
JPH0246500U true JPH0246500U (en) 1990-03-29
JP2505964Y2 JP2505964Y2 (en) 1996-08-07

Family

ID=31377017

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1988125952U Expired - Lifetime JP2505964Y2 (en) 1988-09-27 1988-09-27 Aircraft noise identification device

Country Status (1)

Country Link
JP (1) JP2505964Y2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2722968C1 (en) * 2019-08-22 2020-06-05 Акционерное общество "Всероссийский научно-исследовательский институт "Градиент" Acoustic active aerial objects detection device

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5816993U (en) * 1981-07-23 1983-02-02 日本ビクター株式会社 Narrow angle directional microphone device
JPS595799A (en) * 1982-07-01 1984-01-12 Oki Electric Ind Co Ltd Vibration-resistant microphone
JPS61128895U (en) * 1985-01-30 1986-08-12

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5816993U (en) * 1981-07-23 1983-02-02 日本ビクター株式会社 Narrow angle directional microphone device
JPS595799A (en) * 1982-07-01 1984-01-12 Oki Electric Ind Co Ltd Vibration-resistant microphone
JPS61128895U (en) * 1985-01-30 1986-08-12

Also Published As

Publication number Publication date
JP2505964Y2 (en) 1996-08-07

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