Deprecated: The each() function is deprecated. This message will be suppressed on further calls in /home/zhenxiangba/zhenxiangba.com/public_html/phproxy-improved-master/index.php on line 456
JPS5836732B2 - Radio and sonic shared exploration device - Google Patents
[go: Go Back, main page]

JPS5836732B2 - Radio and sonic shared exploration device - Google Patents

Radio and sonic shared exploration device

Info

Publication number
JPS5836732B2
JPS5836732B2 JP663579A JP663579A JPS5836732B2 JP S5836732 B2 JPS5836732 B2 JP S5836732B2 JP 663579 A JP663579 A JP 663579A JP 663579 A JP663579 A JP 663579A JP S5836732 B2 JPS5836732 B2 JP S5836732B2
Authority
JP
Japan
Prior art keywords
radio
wave
radio wave
sound
sonic
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.)
Expired
Application number
JP663579A
Other languages
Japanese (ja)
Other versions
JPS5599036A (en
Inventor
健蔵 笠牧
錦一郎 秋田
洋右 石井
円 福島
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Japan Radio Co Ltd
Original Assignee
Japan Radio Co Ltd
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 by Japan Radio Co Ltd filed Critical Japan Radio Co Ltd
Priority to JP663579A priority Critical patent/JPS5836732B2/en
Publication of JPS5599036A publication Critical patent/JPS5599036A/en
Publication of JPS5836732B2 publication Critical patent/JPS5836732B2/en
Expired legal-status Critical Current

Links

Landscapes

  • Measuring Temperature Or Quantity Of Heat (AREA)

Description

【発明の詳細な説明】 本発明はたとえば大気温度垂直分布を遠隔測定する電波
音波共用探査装置(Radio andAcousti
c Sounding System:RASS,以下
ラスと略称する。
DETAILED DESCRIPTION OF THE INVENTION The present invention is directed to a radio and acoustic exploration device that remotely measures the vertical distribution of atmospheric temperature, for example.
c Sounding System: RASS, hereinafter abbreviated as RASS.

)に関する。従来のラスは音波放射器ビーム中心と電波
空中線ビーム中心が離れた別々の軸内にあるため受信信
号強度が低く高い高度までの探査が難かしい欠点があっ
た。
) regarding. Conventional laths had the disadvantage that the sonic emitter beam center and the radio antenna beam center were located on separate axes, which resulted in low received signal strength and difficulty in surveying to high altitudes.

従来のラスの動作を第1図に従い説明する。The operation of a conventional lath will be explained with reference to FIG.

第1図において1は音波放射器、2は電波送信空中線、
3は電波受信空中線、4は電波送信機、5は減衰器、6
は混合器、7は増幅器、8はドブラ計測回路、9は処理
回路、10は記録器、11は音波送信機、12は同期信
号発生器である。
In Figure 1, 1 is a sound wave radiator, 2 is a radio wave transmitting antenna,
3 is a radio wave receiving antenna, 4 is a radio wave transmitter, 5 is an attenuator, 6
1 is a mixer, 7 is an amplifier, 8 is a Dobra measurement circuit, 9 is a processing circuit, 10 is a recorder, 11 is a sound wave transmitter, and 12 is a synchronization signal generator.

以下の説明において測定対象の気体として大気を例をと
って述べる。
In the following explanation, the atmosphere will be described as an example of the gas to be measured.

音波放射器1は音波送信機11の可聴帯域のパルス出力
が加えられ、パルス音波を放射する。
The sound wave radiator 1 receives the audible pulse output of the sound wave transmitter 11 and emits pulsed sound waves.

放射されたパルス音波はほぼ球面状の空気の粗密を形或
して大気中を伝搬し、この空気の粗密による比誘電率の
周期的な不均一により電波送信空中線2から放射される
電波の一部が反射される。
The emitted pulsed sound waves propagate through the atmosphere in the form of almost spherical air density, and due to the periodic non-uniformity of the relative dielectric constant due to the air density, one of the radio waves emitted from the radio wave transmitting antenna 2 is part is reflected.

送信電波の波長は音波波長のほぼ2倍に選び上記反射波
が音波の波面によって次々に反射されてコヒーレントに
加算され、電波受信空中線3で受信される。
The wavelength of the transmitted radio wave is selected to be approximately twice the wavelength of the sound wave, and the reflected waves are successively reflected by the wave front of the sound wave, coherently added, and received by the radio wave receiving antenna 3.

この受信々号は音速によるドブラシフトを受けている。This received signal is subjected to a Dobra shift due to the speed of sound.

次いで電波送信機4で発生する送信電力の一部を減衰器
5を通して供給された信号と混合器6によりホモダイン
検波され、ドプラ周波数が検出される。
Next, a portion of the transmission power generated by the radio wave transmitter 4 is subjected to homodyne detection with the signal supplied through the attenuator 5 by the mixer 6, and the Doppler frequency is detected.

このドプラ周波数は増幅器7で増幅された後、同期信号
発生器12で発生するパルス音波放射時刻と同期した時
刻信号を基準として一定時間間隔毎に波長計測等の方法
によるドプラ計測回路8により測定された後、処理回路
9により絶対湛度Tに換算するため下記の関係式による
計算が行われる。
This Doppler frequency is amplified by an amplifier 7 and then measured by a Doppler measurement circuit 8 using a method such as wavelength measurement at regular time intervals based on a time signal synchronized with the pulsed sound emission time generated by a synchronization signal generator 12. After that, the processing circuit 9 performs a calculation using the following relational expression in order to convert it into an absolute degree T.

ここに、Dはドプラ周波数、Kは気体の分子量、湿度等
で決まる定数である。
Here, D is the Doppler frequency, and K is a constant determined by the molecular weight of the gas, humidity, etc.

この計算処理を行われた信号は記録器10に供給され高
度対温度の関係が記録される。
The signal subjected to this calculation process is supplied to the recorder 10, and the relationship between altitude and temperature is recorded.

従来のラスは上記のように電波送信空中線2と電波受信
空中線3および音波放射器1が独立した構戒のため第2
図に示すように音波の波面の中心軸と電波が波面に入射
する角θ1が大きく、また送受信間の電波の漏洩を少な
くするため送受化空中線の間隔を大きくするとθ1はさ
らに犬となり波面からの反射がコヒーレントに加算され
る効率が低くなり、受信々号強度を著しく低下させる欠
点があった。
In the conventional lath, the radio wave transmitting antenna 2, the radio wave receiving antenna 3, and the sound wave radiator 1 are independent as described above, so the second
As shown in the figure, the angle θ1 between the central axis of the wavefront of the sound wave and the incidence of the radio wave on the wavefront is large, and if the interval between the transmitting and receiving antennas is increased to reduce the leakage of radio waves between transmitting and receiving, θ1 becomes even more narrow, and the angle θ1 becomes more narrow from the wavefront. This has the disadvantage that the efficiency with which reflections are coherently added becomes low, and the received signal strength is significantly reduced.

本発明は上記の欠点を除去するため音波放射点と電波放
射点を同一軸内に位置するように構成した音波放射器お
よび電波送信空中線を使用したもので、このような空中
線の実現と効果について以下図面により詳細に説明する
In order to eliminate the above-mentioned drawbacks, the present invention uses a sonic radiator and a radio wave transmitting antenna in which the sonic wave radiating point and the radio wave radiating point are located on the same axis. This will be explained in detail below with reference to the drawings.

第3図は本発明の実施例で、21は音波一次放射器、2
2は電波一次放射器、23は反射鏡、24は音波遮蔽筒
、25は電波吸収材である。
FIG. 3 shows an embodiment of the present invention, in which 21 is a primary acoustic wave radiator;
2 is a primary radio wave radiator, 23 is a reflecting mirror, 24 is a sound wave shielding tube, and 25 is a radio wave absorber.

これの動作は、音波一次放射器21から放射した音波は
パラボラ形反射鏡23で反射されて上方へ放射され、反
射器付ダイポールを用いた電波一次放射器22から放射
された電波は音波と共用の反射鏡23によって反射され
上方へ放射され、音波放射ビーム中心と電波放射ビーム
中心はほぼ同一軸となる。
The operation of this is that the sound waves emitted from the primary sound wave radiator 21 are reflected by the parabolic reflector 23 and radiated upward, and the radio waves emitted from the radio wave primary radiator 22 using a dipole with a reflector are shared with the sound waves. The beam is reflected by the reflecting mirror 23 and radiated upward, and the center of the sound wave radiation beam and the center of the radio wave radiation beam are approximately on the same axis.

.従ってこの空中線は音波放射ビ・−ム中心と電波放射
ビームがほぼ同軸となるためラスにおける音波伝播と電
波反射の関係は第4図に示すようになり電波が音波波面
に入射する角度θ2は第2図に示した従来のラスにおけ
る入射角θ1の約騒トなり反射電波のコヒーレントな加
算の効率が高くなる。
.. Therefore, in this antenna, the center of the sound wave emission beam and the radio wave emission beam are almost coaxial, so the relationship between sound wave propagation and radio wave reflection in the lath is as shown in Figure 4, and the angle θ2 at which the radio wave enters the sound wave surface is As the incident angle θ1 in the conventional lath shown in FIG. 2 increases, the efficiency of coherent addition of reflected radio waves increases.

また音波遮蔽筒24の内面に電波吸収材25を張ること
により、放射電波が受信空中線に漏洩する量を少なくす
ることができ、受信感度は一層向上する。
Furthermore, by covering the inner surface of the sound wave shielding tube 24 with a radio wave absorbing material 25, the amount of radiated radio waves leaking to the receiving antenna can be reduced, and the receiving sensitivity is further improved.

なお本例では音波放射器を電波送信空中線と同一放射ビ
ーム上にくるようにしたが、音波放射器を電波受信空中
線に組み込んでそれらのビームを同一軸上にくるように
構或しても前記とほぼ同一の結果が得られる。
In this example, the sonic radiator is placed on the same radiation beam as the radio wave transmitting antenna, but it is also possible to incorporate the sonic radiator into the radio wave receiving antenna and place their beams on the same axis. Almost the same result is obtained.

さらに第3図では電波送信空中線を反射器付のダイポー
ル空中線で構威し反射鏡を設けたが、空中線はループア
ンテナ等の他のアンテナで構或し、また反射鏡を省略し
てもさしつかえない。
Furthermore, in Fig. 3, the radio wave transmitting antenna is configured with a dipole antenna with a reflector and a reflector is provided, but the antenna may be configured with another antenna such as a loop antenna, or the reflector may be omitted. .

以上の説明のように本発明によれば音波ビームの電波の
送受信ビームが同一軸にくるようになっているので、反
射電波のコヒーレントな加算の効率がよくなり精度が高
上し、空中線も小型化できる。
As explained above, according to the present invention, the transmitting and receiving beams of the radio waves of the sound wave beam are aligned on the same axis, so the efficiency of coherent addition of the reflected radio waves is improved, the accuracy is improved, and the antenna is also compact. can be converted into

さらに送受空中線を独立して電波吸収材および音波遮蔽
材で覆っているので送受のアイソレーションがよい等の
利点がある。
Furthermore, since the transmitting and receiving antennas are independently covered with a radio wave absorbing material and a sound wave shielding material, there are advantages such as good isolation between transmitting and receiving.

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

第1図は電波音波共用探査装置の系統図、第2図は従来
の電波音波共用探査装置における送受信動作説明図、第
3図は本発明の一実施例を示す図、第4図は本発明を実
施した場合の送受信動作説明図である。 1・・・音波放射器、2・・・電波送信空中線、3・・
・電波受信空中線、4・・・送信機、6・・・混合器、
8・・・ドツプラ計測器、9・・・処理回路、10・・
・記録器、11・・・音波送信機、12・・・同期信号
発生器、21・・・音波放射器、22・・・電波放射器
、23・・・反射器、24・・・音波遮蔽筒、25・・
・電波吸収材。
Fig. 1 is a system diagram of a radio/sonic probe system, Fig. 2 is an explanatory diagram of transmission/reception operations in a conventional radio/sonic probe, Fig. 3 is a diagram showing an embodiment of the present invention, and Fig. 4 is a diagram of the present invention. FIG. 4 is an explanatory diagram of transmission and reception operations when the above is implemented. 1...Sonic wave radiator, 2...Radio wave transmitting antenna, 3...
・Radio wave receiving antenna, 4...transmitter, 6...mixer,
8... Dotsupura measuring instrument, 9... Processing circuit, 10...
-Recorder, 11...Sound wave transmitter, 12...Synchronization signal generator, 21...Sound wave radiator, 22...Radio wave radiator, 23...Reflector, 24...Sound wave shield Tube, 25...
・Radio wave absorbing material.

Claims (1)

【特許請求の範囲】 1 混度測定のため音波を気体中に発射し、次に該音波
の粗密面に対し電波を発射して該音波粗密面からの反射
電波を受信し、該送受信信号より音速によるドプラ周波
数を検出して気体の温度を測定する電波音波共用探査装
置において、音波放射器のビーム中心と電波送信空中線
(あるいは電波受信空中線)のビーム中心を同一軸上に
構成したことを特徴とする電波音波共用探査装島 2 湿度測定のため音波を気体中に発射し、次に該音波
の粗密面に対し電波を発射して該音波粗密面からの反射
電波を受信し、該送受信信号より音速によるドプラ周波
数を検出して気体の温度を測定する電波音波共用探査装
置において、音波放射器のビーム中心と電波送信空中線
(あるいは電波受信空中線)のビーム中心を同一軸上に
構或し、音波放射器および電波送信空中線(あるいは電
波受信空中線)を電波吸収材および遮音材から或る円筒
で覆ったことを特徴とする電波音波共用探査装置。
[Claims] 1. To measure the mixture, a sound wave is emitted into a gas, and then a radio wave is emitted to the surface of the sound wave, and the reflected radio wave from the surface of the sound wave is received, and from the transmitted and received signal. A radio/sonic wave shared exploration device that measures the temperature of gas by detecting the Doppler frequency due to the speed of sound, characterized in that the beam center of the sonic radiator and the beam center of the radio wave transmitting antenna (or radio wave receiving antenna) are configured on the same axis. A radio/sonic wave shared exploration island 2 emits a sound wave into the gas to measure humidity, then emits a radio wave to the surface of the sound wave, receives the reflected radio wave from the surface of the sound wave, and receives the transmitted and received signal. In a radio-acoustic shared exploration device that measures the temperature of a gas by detecting the Doppler frequency due to the speed of sound, the beam center of the sonic radiator and the beam center of the radio wave transmitting antenna (or radio wave receiving antenna) are arranged on the same axis, 1. A radio/sonic exploration device characterized in that a sonic radiator and a radio wave transmitting antenna (or a radio wave receiving antenna) are covered with a certain cylinder made of a radio wave absorbing material and a sound insulating material.
JP663579A 1979-01-23 1979-01-23 Radio and sonic shared exploration device Expired JPS5836732B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP663579A JPS5836732B2 (en) 1979-01-23 1979-01-23 Radio and sonic shared exploration device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP663579A JPS5836732B2 (en) 1979-01-23 1979-01-23 Radio and sonic shared exploration device

Publications (2)

Publication Number Publication Date
JPS5599036A JPS5599036A (en) 1980-07-28
JPS5836732B2 true JPS5836732B2 (en) 1983-08-11

Family

ID=11643818

Family Applications (1)

Application Number Title Priority Date Filing Date
JP663579A Expired JPS5836732B2 (en) 1979-01-23 1979-01-23 Radio and sonic shared exploration device

Country Status (1)

Country Link
JP (1) JPS5836732B2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP7052501B2 (en) * 2018-04-04 2022-04-12 スターライト工業株式会社 Sound wave generator for lath radar and lath radar

Also Published As

Publication number Publication date
JPS5599036A (en) 1980-07-28

Similar Documents

Publication Publication Date Title
US2416155A (en) Position locator
US3889533A (en) Acoustic wind sensor
JPH03252586A (en) Laser radar device
GB1291849A (en) Method of, and apparatus for, recording characteristics of the troposphere
US4351188A (en) Method and apparatus for remote measurement of wind direction and speed in the atmosphere
CN114280547A (en) Radar maximum acting distance estimation method based on static test
CN119044617A (en) Antenna pattern measuring device and method based on Redberg quantum effect
JPS5836732B2 (en) Radio and sonic shared exploration device
Ligthart et al. An X-band solid-state FM-CW weather radar
US3745517A (en) Distance measuring device and method
RU2855374C1 (en) Method for opto-acoustic determination of temperature of atmosphere
JPS6228430B2 (en)
Saffold et al. Radar-acoustic interaction for IFF applications
Trevor et al. Notes on propagation at a wavelength of seventy-three centimeters
SU1088512A1 (en) Method of acoustic-optical atmospheric sounding
JPH0955707A (en) Underwater ultrasonic-wave transmission equipment and ultrasonic-wave transmitting method by multiplex ultrasonic wave
JP3282777B2 (en) Phased Array Doppler Soda
JPH05240954A (en) Transmitter-receiver for doppler acoustic wave radar
SU1364868A1 (en) Method of measuring thickness of dielectric article
JPH0224350B2 (en)
SU1088513A1 (en) Method of bistatic acoustic atmospheric sounding
US3366954A (en) Spectrographical range finder
RU2835804C1 (en) Method of calibrating reversible electroacoustic transducers of current velocity meter antennae
RU2589763C2 (en) Method for guiding pulsed electromagnetic radiation to remote object
SU643817A1 (en) Ice thickness measuring method