JPH0326695Y2 - - Google Patents

Info

Publication number
JPH0326695Y2
JPH0326695Y2 JP1984008890U JP889084U JPH0326695Y2 JP H0326695 Y2 JPH0326695 Y2 JP H0326695Y2 JP 1984008890 U JP1984008890 U JP 1984008890U JP 889084 U JP889084 U JP 889084U JP H0326695 Y2 JPH0326695 Y2 JP H0326695Y2
Authority
JP
Japan
Prior art keywords
frequency
pilot signal
signal
circuit
output
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
JP1984008890U
Other languages
Japanese (ja)
Other versions
JPS60121352U (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 JP1984008890U priority Critical patent/JPS60121352U/en
Publication of JPS60121352U publication Critical patent/JPS60121352U/en
Application granted granted Critical
Publication of JPH0326695Y2 publication Critical patent/JPH0326695Y2/ja
Granted legal-status Critical Current

Links

Landscapes

  • Stereo-Broadcasting Methods (AREA)

Description

【考案の詳細な説明】 考案の属する技術分野 本考案は、複数の低周波パイロツト信号を使用
するAMステレオ受信機内で使用するパイロツト
信号検出回路に関するものである。
DETAILED DESCRIPTION OF THE INVENTION Technical Field The present invention relates to a pilot signal detection circuit for use in an AM stereo receiver that uses a plurality of low frequency pilot signals.

従来技術と問題点 現在、米国においては、Magnavox,Kahn,
Motolora,Harrisという4種の方式によるAM
ステレオ放送が商用化されており、これら各方式
を識別するため、同順に5Hz,15Hz,25Hz,55Hz
のパイロツト信号が使用されている。
Prior art and problems Currently, in the United States, Magnavox, Kahn,
AM using four types of methods: Motorola and Harris
Stereo broadcasting has been commercialized, and in order to identify these systems, 5Hz, 15Hz, 25Hz, and 55Hz are used in the same order.
pilot signals are used.

従来これら各パイロツト信号を識別するため
に、各パイロツト信号周波数の共振回路を並列に
4個設け、各共振回路の出力を検出していた。
Conventionally, in order to identify each of these pilot signals, four resonant circuits for each pilot signal frequency were provided in parallel, and the output of each resonant circuit was detected.

しかしながら、上記従来の検出回路は、低周波
数で比較的大型の共振用素子(特にインダクタン
ス)を多数必要とし大きなスペースを占めるだけ
でなく、検出感度を上げるためにQを高めると検
出までに長時間を要するという問題があつた。
However, the conventional detection circuit described above not only requires a large number of relatively large resonance elements (especially inductances) at low frequencies and occupies a large space, but also takes a long time to detect when the Q is increased to increase detection sensitivity. There was a problem that required .

考案の目的 本考案は上記従来の欠点を改良するもので、小
型化が可能で、しかも高速かつ高感度でパイロツ
ト信号を検出することができるパイロツト信号検
出回路を提供することにある。
Purpose of the Invention The present invention aims to improve the above-mentioned drawbacks of the conventional circuit and provides a pilot signal detection circuit which can be miniaturized and which can detect pilot signals at high speed and with high sensitivity.

考案の構成 上記の目的を達成する本考案は、パイロツト信
号を含む受信信号を受けて該パイロツト信号のみ
を通過せしめる低域通過ろ波器、該低域通過ろ波
器の出力を振幅制限する振幅制限回路、該振幅制
限回路の出力を周波数に応じた電圧値の信号に変
換し出力する周波数/電圧変換回路、該周波数/
電圧変換回路の出力を各隣接パイロツト信号の周
波数対応電圧値の中間値を基準として比較する複
数個の比較回路、該各比較回路の比較結果を組合
せて現在受信中のパイロツト信号を決定するデコ
ーダを備えるように構成されている。
Structure of the invention The present invention, which achieves the above objects, includes a low-pass filter that receives a received signal including a pilot signal and passes only the pilot signal; a limiting circuit, a frequency/voltage conversion circuit that converts the output of the amplitude limiting circuit into a signal with a voltage value corresponding to the frequency and outputs the signal;
A plurality of comparison circuits that compare the outputs of the voltage conversion circuits with reference to the intermediate value of the frequency-corresponding voltage values of each adjacent pilot signal, and a decoder that combines the comparison results of the respective comparison circuits to determine the pilot signal currently being received. It is configured to be equipped.

以下、本構成の更に詳細を実施例によつて説明
する。
Further details of this configuration will be explained below using examples.

考案の実施例 第1図は本考案の一実施例の構成ブロツク図で
あり、10は受信入力端子、20は低域通過ろ波
器、30は振幅制限回路、40は周波数/電圧変
換回路、50は比較回路群、60は論理回路であ
る。
Embodiment of the invention FIG. 1 is a block diagram of an embodiment of the invention, in which 10 is a reception input terminal, 20 is a low-pass filter, 30 is an amplitude limiting circuit, 40 is a frequency/voltage conversion circuit, 50 is a comparison circuit group, and 60 is a logic circuit.

図示しない受信回路に連なる受信入力端子10
上の受信信号は、低域通過ろ波器20に供給さ
れ、ここを通過した低周波のパイロツト信号だけ
が振幅制限回路30に供給される。ここで振幅制
限を受けたパイロツト信号は、次段の周波数/電
圧変換回路40に供給される。この周波数/電圧
変換回路40に供給されたパイロツト信号は、入
力抵抗41、利得1のオペアンプ42及び帰還用
コンデンサ43から成り1Hz程度の遅延時間を有
する低域通過ろ波器を通過したのち、ダイオード
44と平滑用コンデンサ45から成る整流回路で
整流される。この周波数/電圧変換回路40の周
波数/電圧変換特性は、第2図に例示するよう
に、周波数が高くなるに従つて出力電圧が直線的
に減少するようなものである。
Reception input terminal 10 connected to a reception circuit (not shown)
The above received signal is supplied to a low pass filter 20, and only the low frequency pilot signal that has passed through this filter is supplied to an amplitude limiting circuit 30. The pilot signal whose amplitude has been limited here is supplied to the frequency/voltage conversion circuit 40 at the next stage. The pilot signal supplied to this frequency/voltage conversion circuit 40 is made up of an input resistor 41, an operational amplifier 42 with a gain of 1, and a feedback capacitor 43, and passes through a low-pass filter having a delay time of about 1 Hz, and then passes through a diode. 44 and a smoothing capacitor 45. The frequency/voltage conversion characteristic of this frequency/voltage conversion circuit 40 is such that the output voltage decreases linearly as the frequency increases, as illustrated in FIG.

電圧に変換されたパイロツト信号は次段の比較
回路群50に供給される。この比較回路群は4個
の比較回路51,52,53及び54から構成さ
れており、各々の基準電圧V1〜V4は各隣接パイ
ロツト信号の周波数対応電圧値の中間値となるよ
うに設定されている。即ち、第2図に示すよう
に、比較回路51の基準電圧V1は、前述した4
種のパイロツト信号の周波数のうち最も低周波数
の5Hz(Magnavox方式)とこれに隣接する15Hz
(Kahn方式)の中間の周波数である10Hzの電圧に
対応した値に設定されている。また、比較回路5
2の基準電圧V2は、15Hz(Kahn方式)とこれに
隣接して1段高周波の25Hz(Motolora方式)の
中間の周波数である20Hzの電圧に対応した値に設
定され、以下同様にして比較回路53,54の基
準電圧V3,V4はそれぞれ40Hz,70Hzの周波数に
対応した電圧値に設定されている。
The pilot signal converted into a voltage is supplied to a group of comparison circuits 50 at the next stage. This comparison circuit group is composed of four comparison circuits 51, 52, 53, and 54, and each reference voltage V1 to V4 is set to be an intermediate value of the frequency-corresponding voltage values of each adjacent pilot signal. There is. That is, as shown in FIG. 2, the reference voltage V1 of the comparator circuit 51 is
The lowest frequency of the seed pilot signal frequency is 5Hz (Magnavox method) and the adjacent 15Hz.
(Kahn method) is set to a value corresponding to a voltage of 10Hz, which is the intermediate frequency. In addition, the comparison circuit 5
The reference voltage V2 of No. 2 is set to a value corresponding to a voltage of 20Hz, which is an intermediate frequency between 15Hz (Kahn method) and the adjacent first-stage high frequency 25Hz (Motolora method). Reference voltages V3 and V4 of 53 and 54 are set to voltage values corresponding to frequencies of 40Hz and 70Hz, respectively.

従つて、この受信機が5Hzのパイロツト信号を
使用するMagnavox方式の放送波を受信した場合
には、全ての比較回路51〜54の出力がハイに
なる。また、この受信機が15Hzのパイロツト信号
を使用するKahn方式の放送波を受信した場合に
は、比較回路51の出力だけがローになり、他の
3個の比較回路52〜54の出力は全てハイにな
る。同様にして、この受信機が25Hzのパイロツト
信号を使用するMotolora方式の放送波を受信し
た場合には、比較回路51と52の出力がローに
なり、比較回路53と54の出力はハイになる。
この受信機が55Hzのパイロツト信号を使用する
Harris方式の放送波を受信した場合には、比較
回路54の出力だけがハイになり、他の3個の比
較回路の出力は全てローになる。
Therefore, when this receiver receives broadcast waves of the Magnavox system using a 5 Hz pilot signal, the outputs of all comparison circuits 51 to 54 become high. Furthermore, when this receiver receives a Kahn system broadcast wave that uses a 15Hz pilot signal, only the output of the comparison circuit 51 becomes low, and all the outputs of the other three comparison circuits 52 to 54 become low. Get high. Similarly, when this receiver receives Motorola broadcast waves that use a 25Hz pilot signal, the outputs of comparison circuits 51 and 52 become low, and the outputs of comparison circuits 53 and 54 become high. .
This receiver uses a 55Hz pilot signal.
When a Harris system broadcast wave is received, only the output of the comparison circuit 54 becomes high, and the outputs of the other three comparison circuits all become low.

上記4個の比較回路51〜54のハイ/ロー出
力は、3個のアンドゲート61〜63と3個のイ
ンバータ64〜66からな成るデコーダ60でデ
コードされ、4個の端子67〜70に検出結果を
出力する。即ち、出力端子67だけにハイ信号が
出力され場合にはMagnavox方式の放送波の受信
が検出され、出力端子68だけにハイ信号が出力
された場合にはKahn方式の放送波の受信が検出
され、出力端子68だけにハイ信号が出力された
場合にはMotolora方式の放送波の受信が検出さ
れ、出力端子69だけにハイ信号が出力された場
合にはHarris方式の放送波の受信が検出される。
The high/low outputs of the four comparison circuits 51-54 are decoded by a decoder 60 consisting of three AND gates 61-63 and three inverters 64-66, and detected at four terminals 67-70. Output the results. That is, if a high signal is output only to the output terminal 67, reception of a Magnavox broadcast wave is detected, and if a high signal is output only to the output terminal 68, reception of a Kahn broadcast wave is detected. If a high signal is output only to output terminal 68, reception of Motorola system broadcast waves is detected, and if a high signal is output only to output terminal 69, reception of Harris system broadcast waves is detected. Ru.

上記実施例では、周波数/電圧変換回路として
低域通過ろ波器と整流回路の組合せを使用した
が、これに代えて他の適宜な周波数/電圧変換回
路を使用することもできる。
In the above embodiment, a combination of a low-pass filter and a rectifier circuit is used as the frequency/voltage conversion circuit, but other appropriate frequency/voltage conversion circuits may be used instead.

考案の効果 本考案は上述のような構成であるから、小型化
が可能で、しかも高速かつ高感度でパイロツト信
号を検出することができるという利点がある。
Effects of the Invention Since the present invention has the above-described configuration, it has the advantage of being miniaturized and being able to detect pilot signals at high speed and with high sensitivity.

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

第1図は本考案の一実施例の構成ブロツク図、
第2図は上記実施例の動作を説明するための概念
図である。 10……受信入力端子、20……低域通過ろ波
器、30……振幅制限回路、40……周波数/電
圧変換回路、50……比較回路群、60……デコ
ーダ。
FIG. 1 is a block diagram of an embodiment of the present invention.
FIG. 2 is a conceptual diagram for explaining the operation of the above embodiment. 10... Reception input terminal, 20... Low pass filter, 30... Amplitude limiting circuit, 40... Frequency/voltage conversion circuit, 50... Comparison circuit group, 60... Decoder.

Claims (1)

【実用新案登録請求の範囲】 複数の低周波パイロツト信号を使用するAMス
テレオ放送を受信するためのAMステレオ受信機
において、 前記パイロツト信号を含む受信信号を受けて該
パイロツト信号のみを通過せしめる低域通過ろ波
器、該低域通過ろ波器の出力を振幅制限する振幅
制限回路、該振幅制限回路の出力を周波数に応じ
た電圧値の信号に変換し出力する周波数/電圧変
換回路、該周波数/電圧変換回路の出力を各隣接
パイロツト信号の周波数対応電圧値の中間値を基
準として比較する複数個の比較回路、該各比較回
路の比較結果を組合せて現在受信中のパイロツト
信号を決定するデコーダを備えたことを特徴とす
るパイロツト信号検出回路。
[Claims for Utility Model Registration] In an AM stereo receiver for receiving AM stereo broadcasting using a plurality of low frequency pilot signals, a low frequency receiver that receives a received signal including the pilot signal and allows only the pilot signal to pass through. A pass filter, an amplitude limiting circuit that limits the amplitude of the output of the low pass filter, a frequency/voltage conversion circuit that converts the output of the amplitude limiting circuit into a signal with a voltage value corresponding to the frequency and outputs the signal, and the frequency. /a plurality of comparison circuits that compare the outputs of the voltage conversion circuits with reference to the intermediate value of the frequency-corresponding voltage values of adjacent pilot signals, and a decoder that combines the comparison results of the respective comparison circuits to determine the pilot signal currently being received. A pilot signal detection circuit comprising:
JP1984008890U 1984-01-25 1984-01-25 Pilot signal detection circuit Granted JPS60121352U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1984008890U JPS60121352U (en) 1984-01-25 1984-01-25 Pilot signal detection circuit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1984008890U JPS60121352U (en) 1984-01-25 1984-01-25 Pilot signal detection circuit

Publications (2)

Publication Number Publication Date
JPS60121352U JPS60121352U (en) 1985-08-16
JPH0326695Y2 true JPH0326695Y2 (en) 1991-06-10

Family

ID=30488590

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1984008890U Granted JPS60121352U (en) 1984-01-25 1984-01-25 Pilot signal detection circuit

Country Status (1)

Country Link
JP (1) JPS60121352U (en)

Also Published As

Publication number Publication date
JPS60121352U (en) 1985-08-16

Similar Documents

Publication Publication Date Title
US2580148A (en) Antinoise carrier receiving system
JPS6139731A (en) Noise detector
JPH0326695Y2 (en)
SU976864A3 (en) Amplitude-modulated stereophonic signal receiver
US3109896A (en) Radio receiver means employing separable complementary units
US4450590A (en) Discriminator circuit for frequency modulation receivers
US1559743A (en) Radio receiving system
US4370676A (en) Carrier regenerating circuit for a synchronous detector
US3626310A (en) Frequency discriminator
JPS6259938B2 (en)
SU1202016A1 (en) Frequency discriminator
JPS6214762Y2 (en)
JPH0448061Y2 (en)
JPS6115665Y2 (en)
JPH0810974Y2 (en) Quadrature detector
US2677050A (en) Gain control means for frequency modulation receivers
JP2538661Y2 (en) Phase shift circuit of quadracha detector
JPS6246347Y2 (en)
US3222605A (en) Low pass, low level filter
JPS6322739B2 (en)
US1853179A (en) Superheterodyne receiver control
JPH0352061Y2 (en)
JPH04342318A (en) Diversity reception system
SU1497758A1 (en) Demodulator of phase-shift keyed signals
US3339024A (en) Time sampling stereophonic receiver circuit