JPH0235386A - Radar apparatus - Google Patents

Radar apparatus

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Publication number
JPH0235386A
JPH0235386A JP63183979A JP18397988A JPH0235386A JP H0235386 A JPH0235386 A JP H0235386A JP 63183979 A JP63183979 A JP 63183979A JP 18397988 A JP18397988 A JP 18397988A JP H0235386 A JPH0235386 A JP H0235386A
Authority
JP
Japan
Prior art keywords
signal
beam scanning
pulse
signal processing
pulse compression
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
JP63183979A
Other languages
Japanese (ja)
Other versions
JP2668966B2 (en
Inventor
Hidekazu Kiuchi
木内 英一
Akira Ikeda
明 池田
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.)
NEC Corp
Original Assignee
NEC Corp
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 NEC Corp filed Critical NEC Corp
Priority to JP63183979A priority Critical patent/JP2668966B2/en
Publication of JPH0235386A publication Critical patent/JPH0235386A/en
Application granted granted Critical
Publication of JP2668966B2 publication Critical patent/JP2668966B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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  • Radar Systems Or Details Thereof (AREA)

Abstract

PURPOSE:To conduct beam scanning matched with the purpose of use by making it possible to specify the number of hits and the period of the beam scanning freely for each area according to various conditions. CONSTITUTION:An operator specifies the form of compression of a pulse, the form of a signal processing and the period of beam scanning for each small area from an operation panel 420. A system control computer 500 delivers a beam scanning control signal 501 to a cylindrical active phased array antenna 100, a pulse compression form selection signal 502 to a pulse expander 210 and a pulse compressor 220, and a signal processing form selection signal to a signal processing device 300, and conducts an operational control of an entire radar system. Receiving a transmission IF signal 151 from the expander 210 and the scanning control signal 501, the antenna 100 emits a transmission beam and outputs a reception IF signal 152 to the compressor 220. A compression IF signal 225 of the compressor 220 is converted into a video signal 250 and processed by the processing device 300.

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明はレーダ装置に関し、特に3次元空間の任意の方
向に、任意の時間にビームを照射てきる2次元電子走査
フェースドアレーレーダに関する。
DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention relates to a radar device, and particularly to a two-dimensional electronically scanned face array radar that can irradiate a beam in any direction in three-dimensional space at any time.

(発明の背景) 防衛レーダにおいては、航空機、誘導飛翔体等の高速飛
行能力の向上、高旋回能力の向上に伴い一層短時間で全
捜索空間を走査(スキャン)することが要求されている
。一方マイクロ波吸収材料の採用およびマイクロ波の反
射を回避する形状の採用等により、要捕捉航空機や誘導
飛翔体の反射断面積は減少の一途を辿っており、これに
対処するためレーダは一層のエネルギーと多くの送信パ
ルスの放射を余儀なくされつつある。
(Background of the Invention) Defense radars are required to scan the entire search space in a shorter time due to improvements in high-speed flight capabilities and high turning capabilities of aircraft, guided flying vehicles, and the like. On the other hand, due to the adoption of microwave-absorbing materials and shapes that avoid microwave reflection, the reflection cross-section of aircraft and guided flying objects to be captured continues to decrease, and in order to cope with this, radars are becoming more sophisticated. It is being forced to emit energy and many transmitted pulses.

(発明が解決しようとする課題) しかしながら、スキャン時間の短縮と特定方位あたりの
送信パルス数(以下ヒツト数という)の増大とは互いに
摺入れない要求条件であり、航空管制に使用されている
ような機械回転形レーダてはビーム走査角速度が一定で
あるため、スキャン時間を短縮しようとすればヒッl〜
数の減少を招き、要求に応えることは不可能である。
(Problem to be solved by the invention) However, shortening the scan time and increasing the number of transmitted pulses per specific direction (hereinafter referred to as the number of hits) are mutually exclusive requirements, and as used in air traffic control, Since the beam scanning angular velocity of a mechanical rotary radar is constant, trying to shorten the scanning time will result in a hit.
This will lead to a decrease in the number of people and it will be impossible to meet the demand.

又、方位および仰角方向にいわゆる2次元電子走査を行
うフェーズドアレーレーダがあるが、この場合にも平面
形アレーを機械回転する限りは、多少のビーム走査角速
度の制御が可能であるが、機械回転による制約から不特
定方位から到来する航空機 誘導飛翔体に充分対処する
ことはできないという問題がある。
There is also a phased array radar that performs so-called two-dimensional electronic scanning in the azimuth and elevation directions, but in this case as well, as long as the planar array is mechanically rotated, it is possible to control the beam scanning angular velocity to some extent; Due to the constraints of

本発明の目的は、3次元空間の任意の方向に任意の時間
にビーム放射できる多面形フェーズl−アレー又は円筒
形フェース1〜アレーを使用し、地形条件、気象条件、
電波環境条件およびレーク運用目的」二の各種条件等に
応じてレークオペレーダに領域毎に自由にヒラ1−数と
ビーム走査周期等を指定できる手段を提供することによ
って、運用目的に合致したビーム走査を可能とするレー
ダを提供しようとするものである。
The object of the present invention is to use a polygonal phase l-array or a cylindrical face l-array that can emit a beam in any direction in three-dimensional space at any time, and to
By providing rake operators with a means to freely specify the number of beams, beam scanning period, etc. for each region according to the various conditions described in ``Radio Wave Environment Conditions and Rake Operation Purposes'', beams that meet the operational purposes can be created. The aim is to provide a radar that enables scanning.

(課題を解決するための手段) 本発明のレーダ装置は上記の目的を達成するために次の
手段構成を有する。
(Means for Solving the Problems) The radar device of the present invention has the following means configuration to achieve the above object.

即ち、本発明のレーダ装置は、ビーム走査制御信号によ
り任意の時間に3次元空間の任意の方向に電子的に送受
信ビームを形成できるアンテナと送信パルス幅と圧縮後
のパルス幅とを対とする複数のパルス圧縮形態を内蔵し
外部からのパルス圧縮形B選択信号に応じてその内の1
つのパルス圧縮形態をリアルタイムで選択可能な受信機
と: 予めプログラムされた複数の信号処理形態の内か
ら外部からの信号処理形態選択信号に応じてその内の1
つの信号処理形態をリアルタイムで選択可能な信号処理
機と; レーダの捜索空間を、地形条件、気象条件、レ
ーダ運用上の条件によって複数の領域に分割するための
領域設定手段と;前記分割領域毎に当該領域に適用する
前記パルス圧縮形態および信号処理形態の内適切なもの
を割付けるための処理指定手段と; 前記分割領域毎に
当該領域内をビーム走査するビーム走査周期を前記分割
領域の内いずれか1つの領域の周期を基準とした相対数
て指定するビーム走査指定手段と前記領域設定手段と前
記処理指定手段と前記ビーム走査指定手段とから設定お
よび指定諸元を受けてビーム走査・送信シーケンス制御
プログラムを作成し前記アンテナ、受信機および信号処
理機に対しそれぞれビーム走査制御信号、パルス圧縮形
態選択信号および信号処理形態選択制御信号を送出する
システム制御器と; を具備することを特徴とするもの
である。
That is, the radar device of the present invention pairs an antenna capable of electronically forming a transmitting/receiving beam in any direction in three-dimensional space at any time using a beam scanning control signal, a transmitting pulse width, and a compressed pulse width. Built-in multiple pulse compression formats, one of which is selected according to an external pulse compression type B selection signal.
A receiver capable of selecting one of two pulse compression formats in real time: Select one of a plurality of pre-programmed signal processing formats in response to an external signal processing format selection signal.
a signal processor capable of selecting two signal processing formats in real time; a region setting means for dividing a radar search space into a plurality of regions according to topographical conditions, weather conditions, and radar operational conditions; processing designation means for allocating an appropriate one of the pulse compression mode and signal processing mode to be applied to the region; and a beam scanning period for beam scanning within the region for each of the divided regions; Beam scanning/transmission upon receiving settings and specified specifications from a beam scanning specifying means for specifying a relative number based on the cycle of any one area, the area setting means, the processing specifying means, and the beam scanning specifying means. a system controller that creates a sequence control program and sends a beam scanning control signal, a pulse compression mode selection signal, and a signal processing mode selection control signal to the antenna, receiver, and signal processor, respectively; It is something to do.

(実 施 例) 以下、本発明のレーダ装置の実施例を図面を参照して説
明する。
(Example) Hereinafter, an example of the radar device of the present invention will be described with reference to the drawings.

第1図は本発明のレーク装置の実施例の構成を示すブロ
ック図である。第1図において100は円筒形状をもち
、送信用パワー1〜ランジスタをアンテナ素子の1つ1
つに一体構造として組込んだ全方位電子ビーム走査の円
筒形アクティブフェーズドアレーアンテナ、200は受
信装置、300は信号処理装置、400は指揮管制装置
、500はシステム制御計算機である。又、受信装置2
00において、210はパルス伸張器、220はパルス
圧縮器、230は検波器であり、指揮管制装置400に
おいて410は表示器、420は操作盤である。
FIG. 1 is a block diagram showing the configuration of an embodiment of the rake device of the present invention. In Fig. 1, 100 has a cylindrical shape, and a transmission power of 1 to 1 is connected to one of the antenna elements.
200 is a receiving device, 300 is a signal processing device, 400 is a command and control device, and 500 is a system control computer. Also, the receiving device 2
00, 210 is a pulse stretcher, 220 is a pulse compressor, 230 is a detector, and in the command and control device 400, 410 is a display, and 420 is an operation panel.

第1図に従い、本発明の動作について説明する。The operation of the present invention will be explained with reference to FIG.

はじめに操作盤420からオペレーダが地形条件、気象
条件、電波環境条件、レーダ運用条件に応じて領域設定
を行い、全捜索方位領域を複数の小領域に分割する。
First, the operator sets the area from the operation panel 420 according to topographic conditions, weather conditions, radio wave environment conditions, and radar operation conditions, and divides the entire search direction area into a plurality of small areas.

第2図に領域の設定例を示す。次に、オペレーダは操作
盤420から小領域毎に、領域内において実施するパル
ス圧縮形態、信号処理形態をそれぞれ予め設計段階で組
込まれたメニューの中から1つを選択する形で指定し、
又、各領域毎にその領域をビーム走査する周期を比数で
指定する。
FIG. 2 shows an example of setting the area. Next, the operator specifies the pulse compression mode and signal processing mode to be implemented in each small region from the operation panel 420 by selecting one from the menus that have been incorporated in advance at the design stage,
Further, for each region, the period for scanning the region with the beam is specified by a ratio.

第1表Gとこのような指定例を示す。Table 1 G shows an example of such a specification.

第1表は、次の意図に基づいて設定された例を示してい
る。
Table 1 shows an example set up based on the following intent.

(1)遠距離程大電力を必要とするため、長い送信パル
ス幅(伸張パルス幅)を選択している。
(1) A long transmission pulse width (expanded pulse width) is selected because the longer the distance, the more power is required.

(2)近距離目標程高精度の位置計測を必要とするため
、短い圧縮パルス幅を選択している。
(2) Since the closer the target is, the more accurate position measurement is required, a shorter compression pulse width is selected.

(3)近距離には地表面反射に起因した大電力グラ第1
表 ンドクラックが存在するなめ、近距離程多ヒツトのパル
ス1〜ツプラ処理を行い、大きな信号対クラッタ電力比
改善度の実現を図る。
(3) At short distances, there is a large power graph caused by ground surface reflection.
Since surface cracks exist, the closer the distance, the more the pulse 1 to tsuppura processing is performed to achieve a large improvement in the signal to clutter power ratio.

(4)近距離の脅威目標程脅威度が高く、単位時間あた
りの方位位置変化か大きく、又、高精度の追尾性能を必
要とするため短いビーム走査周期を割当てる。
(4) A shorter beam scanning period is assigned to a threat target at a shorter distance because the threat level is higher, the azimuth position changes more greatly per unit time, and highly accurate tracking performance is required.

(5)重点捜索空域(領域D)に対しては、短圧縮パル
ス幅、多ヒツトパルスドツプラ処理、類ビーム走査周期
を割当てる。
(5) Short compressed pulse width, multi-hit pulse Doppler processing, and similar beam scanning period are assigned to the priority search airspace (area D).

操作盤420からのオペレーダ指定情報450を受りて
システム制御計算機500は、はじめに各領域を1回ビ
ーム走査するのに必要なビーム走査時間を計算し、次に
各領域毎に指定されたビーム走査周期(比)に従って全
体のビーム走査プログラムを編集し、領域別ビーム走査
周期を算定して、ビーム走査プロクラム情報504を表
示器410に送出する。第2表にこのようにして算定さ
れた領域別ビーム走査周期の例を示す。オペレーダは表
示器410に表示されたビーム走査プログラムを確認し
第2表 必要に応して操作盤420から修正を行い、ビーム走査
プログラムを確定する。
Upon receiving the operator designation information 450 from the operation panel 420, the system control computer 500 first calculates the beam scanning time required to scan each region once, and then performs the beam scanning specified for each region. The entire beam scanning program is edited according to the period (ratio), the beam scanning period for each area is calculated, and the beam scanning program information 504 is sent to the display 410. Table 2 shows an example of the beam scanning period for each area calculated in this way. The operator checks the beam scanning program displayed on the display 410, makes corrections from the operation panel 420 as necessary in Table 2, and finalizes the beam scanning program.

システム制御計算機500は確定されたビーム走査プロ
グラムに従い、リアルタイムて円筒形アクティブフェー
ストアレーアンテナ100に対しビーム走査制御信号5
01を、パルス伸張器210およびパルス圧縮器220
に対しパルス圧縮形態選択信号502を、信号処理装置
300に対し信号処理形態選択信号503を、それぞれ
送出し、全レークシステムの動作制御を行う。
The system control computer 500 sends beam scanning control signals 5 to the cylindrical active face array antenna 100 in real time according to the determined beam scanning program.
01, pulse stretcher 210 and pulse compressor 220
A pulse compression mode selection signal 502 is sent to the signal processing device 300, and a signal processing mode selection signal 503 is sent to the signal processing device 300, respectively, to control the operation of the entire Rake system.

パルス伸張器210はシステム制御計算機500からの
パルス圧縮形態信号502を受けて予め組込まれた複数
のパルス伸張デバイスの中から指定の伸張パルス幅を発
生ずるものをリアルタイムて選択し送信IP倍信号51
を出力する。円筒形アクティブフェーズドアレーアンテ
ナ100は、送信IP倍信号51とビーム走査制御信号
501とを受()てリアルタイムで指定の方向に送信ビ
ームを形成し指定のパルス幅のマイクロ波エネルギーを
放射する。
The pulse stretcher 210 receives the pulse compression format signal 502 from the system control computer 500, selects one that generates a specified expanded pulse width from among a plurality of pre-installed pulse expansion devices in real time, and transmits the transmitted IP multiplication signal 51.
Output. The cylindrical active phased array antenna 100 receives a transmission IP multiplication signal 51 and a beam scanning control signal 501, forms a transmission beam in a specified direction in real time, and radiates microwave energy with a specified pulse width.

同時に指定方向に形成したビームで受信した信号を復調
し受信IF信号152を出力する。
At the same time, the signal received by the beam formed in the designated direction is demodulated and a reception IF signal 152 is output.

パルス圧縮器220は、パルス伸張器210と同期して
入力するパルス圧縮形態信号502を受けて、予め組込
まれた複数のパルス圧縮デバイスの中から指定の圧縮パ
ルス幅を発生ずるものをリアルタイムで選択し圧縮IP
倍信号25を出力する。検波器230は圧mIF信号2
25を受けて所定の検波を行い、ビデオ信号250を発
生ずる。
The pulse compressor 220 receives a pulse compression format signal 502 input in synchronization with the pulse stretcher 210, and selects in real time one of a plurality of pre-installed pulse compression devices that generates a specified compressed pulse width. Compressed IP
A double signal 25 is output. The detector 230 receives the pressure mIF signal 2
25 and performs predetermined detection to generate a video signal 250.

信号処理装置300はビデオ信号250と信号処理形態
選択信号503とを互いに同期したタイミンクで入力し
、予め設計段階でプログラムされた複数の信号処理形態
の中から指定の処理形態をリアルタイムで選択しビデオ
信号250に対し処理する。
The signal processing device 300 inputs the video signal 250 and the signal processing mode selection signal 503 at mutually synchronized timing, selects in real time a specified processing mode from among a plurality of signal processing modes programmed in advance at the design stage, and processes the video signal. The signal 250 is processed.

このような処理を実現するため、信号処理演算素子とし
てファームウェアにより処理機能を可変できる信号処理
プロセッサを採用し、ファームウェアの中に予め設計し
た複数の信号処理形態(たとえば4ヒッ1−MTl処理
、8ヒツI〜パルスドツプラ処理、16ヒツトパルスド
ツプラ処理)をプログラムとして盛込んでおき、リアル
タイムで選択可能としておく。このようにして最終的処
理された出力信号を表示器410に表示する。
In order to realize such processing, a signal processing processor whose processing function can be changed by firmware is used as a signal processing arithmetic element, and multiple signal processing forms (for example, 4-Hi1-MTl processing, 8-Hit 1-MTl processing, Hit I ~ pulse Doppler processing, 16 hit pulse Doppler processing) are included as a program and can be selected in real time. The final processed output signal is displayed on the display 410 in this manner.

(発明の効果) 以」−説明したように、本発明のレーダ装置によれば、
従来のように設計段階で予め組込まれた運用モードくビ
ーム走査プログラム)に限定されず、電波環境条件の変
化や対象捜索空域内航空機飛行状況に適応したビーム走
査、送信パルスの割付けおよび従来レーダの機械回転周
期に対応したビーム走査周期を、レーダオペレーダの意
のままにプログラムし実施することができるという利点
がある。
(Effects of the Invention) As explained above, according to the radar device of the present invention,
It is not limited to the conventional operation mode (beam scanning program) that is pre-installed at the design stage, but it is also capable of beam scanning, transmission pulse assignment, and transmission pulse assignment that adapt to changes in radio wave environment conditions and aircraft flight conditions within the target search airspace. There is an advantage that the beam scanning period corresponding to the machine rotation period can be programmed and executed as desired by the radar operator.

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

第1図は本発明のレーダ装置の実施例の構成を示すブロ
ック図、第2図は本発明実施例装置における領域設定例
を示す図である。 100 ・・・円筒形アクティブフェース1−アレーア
ンテナ、 200・・・・・・受信装置、 210・・
曲・パルス伸張器、 220・・・・・・パルス圧縮器
、 230・・・・検波器、 300・・・信号処理装
置、 400・・・・指揮管制装置、 410・・・ 
表示器、 420・・・・・・操作盤、500・・・・
・システム制御計算機。 代理人 弁理士  八 幡  義 博
FIG. 1 is a block diagram showing the configuration of an embodiment of a radar device according to the present invention, and FIG. 2 is a diagram showing an example of area setting in the device according to the embodiment of the present invention. 100... Cylindrical active face 1-array antenna, 200... Receiving device, 210...
music/pulse stretcher, 220...pulse compressor, 230...detector, 300...signal processing device, 400...command and control device, 410...
Display, 420... Operation panel, 500...
・System control computer. Agent Patent Attorney Yoshihiro Hachiman

Claims (1)

【特許請求の範囲】[Claims] ビーム走査制御信号により任意の時間に3次元空間の任
意の方向に電子的に送受信ビームを形成できるアンテナ
と;送信パルス幅と圧縮後のパルス幅とを対とする複数
のパルス圧縮形態を内蔵し外部からのパルス圧縮形態選
択信号に応じてその内の1つのパルス圧縮形態をリアル
タイムで選択可能な受信機と;予めプログラムされた複
数の信号処理形態の内から外部からの信号処理形態選択
信号に応じてその内の1つの信号処理形態をリアルタイ
ムで選択可能な信号処理機と;レーダの捜索空間を、地
形条件、気象条件、レーダ運用上の条件によって複数の
領域に分割するための領域設定手段と;前記分割領域毎
に当該領域に適用する前記パルス圧縮形態および信号処
理形態の内適切なものを割付けるための処理指定手段と
;前記分割領域毎に当該領域内をビーム走査するビーム
走査周期を前記分割領域の内いずれか1つの領域の周期
を基準とした相対数で指定するビーム走査指定手段と;
前記領域設定手段と前記処理指定手段と前記ビーム走査
指定手段とから設定および指定諸元を受けてビーム走査
・送信シーケンス制御プログラムを作成し前記アンテナ
、受信機および信号処理機に対しそれぞれビーム走査制
御信号、パルス圧縮形態選択信号および信号処理形態選
択制御信号を送出するシステム制御器とを具備すること
を特徴とするレーダ装置。
It has a built-in antenna that can electronically form a transmitting and receiving beam in any direction in three-dimensional space at any time using a beam scanning control signal; and a plurality of pulse compression modes that pair the transmitted pulse width with the compressed pulse width. A receiver capable of selecting one of the pulse compression formats in real time in response to an external pulse compression format selection signal; a signal processor capable of selecting one of the signal processing formats in real time according to the conditions; and an area setting means for dividing the radar search space into a plurality of areas according to topographical conditions, weather conditions, and radar operational conditions. ; processing designation means for allocating an appropriate one of the pulse compression mode and signal processing mode to be applied to each of the divided regions; and a beam scanning period for beam scanning within the region for each of the divided regions. beam scanning designation means for designating by a relative number based on the period of any one of the divided regions;
A beam scanning/transmission sequence control program is created by receiving settings and specified specifications from the area setting means, the processing specifying means, and the beam scanning specifying means, and beam scanning control is performed for the antenna, receiver, and signal processor, respectively. 1. A radar device comprising: a system controller that transmits a signal, a pulse compression mode selection signal, and a signal processing mode selection control signal.
JP63183979A 1988-07-23 1988-07-23 Radar equipment Expired - Lifetime JP2668966B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP63183979A JP2668966B2 (en) 1988-07-23 1988-07-23 Radar equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP63183979A JP2668966B2 (en) 1988-07-23 1988-07-23 Radar equipment

Publications (2)

Publication Number Publication Date
JPH0235386A true JPH0235386A (en) 1990-02-05
JP2668966B2 JP2668966B2 (en) 1997-10-27

Family

ID=16145187

Family Applications (1)

Application Number Title Priority Date Filing Date
JP63183979A Expired - Lifetime JP2668966B2 (en) 1988-07-23 1988-07-23 Radar equipment

Country Status (1)

Country Link
JP (1) JP2668966B2 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH03259772A (en) * 1990-03-09 1991-11-19 Mitsubishi Electric Corp Radar equipment
US5322112A (en) * 1992-03-04 1994-06-21 Sumitomo Heavy Industries, Ltd. Casting-thickness variable mold for continuous casting

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59211878A (en) * 1983-05-17 1984-11-30 Nec Corp Three-dimensional radar
JPS61209383A (en) * 1985-03-13 1986-09-17 Mitsubishi Electric Corp Multi-target tracking apparatus
JPS6244227A (en) * 1985-08-21 1987-02-26 株式会社東芝 Ultrasonic diagnostic apparatus

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59211878A (en) * 1983-05-17 1984-11-30 Nec Corp Three-dimensional radar
JPS61209383A (en) * 1985-03-13 1986-09-17 Mitsubishi Electric Corp Multi-target tracking apparatus
JPS6244227A (en) * 1985-08-21 1987-02-26 株式会社東芝 Ultrasonic diagnostic apparatus

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH03259772A (en) * 1990-03-09 1991-11-19 Mitsubishi Electric Corp Radar equipment
US5322112A (en) * 1992-03-04 1994-06-21 Sumitomo Heavy Industries, Ltd. Casting-thickness variable mold for continuous casting

Also Published As

Publication number Publication date
JP2668966B2 (en) 1997-10-27

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