JPH0470201A - Scan antenna - Google Patents

Scan antenna

Info

Publication number
JPH0470201A
JPH0470201A JP2183650A JP18365090A JPH0470201A JP H0470201 A JPH0470201 A JP H0470201A JP 2183650 A JP2183650 A JP 2183650A JP 18365090 A JP18365090 A JP 18365090A JP H0470201 A JPH0470201 A JP H0470201A
Authority
JP
Japan
Prior art keywords
paraboloid
reflecting mirror
rotor
rotating
reflected
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.)
Pending
Application number
JP2183650A
Other languages
Japanese (ja)
Inventor
Kazuo Sato
和夫 佐藤
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.)
Hitachi Unisia Automotive Ltd
Nippon Denshi Kiki Co Ltd
Original Assignee
Japan Electronic Control Systems Co Ltd
Nippon Denshi Kiki 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 Electronic Control Systems Co Ltd, Nippon Denshi Kiki Co Ltd filed Critical Japan Electronic Control Systems Co Ltd
Priority to JP2183650A priority Critical patent/JPH0470201A/en
Publication of JPH0470201A publication Critical patent/JPH0470201A/en
Pending legal-status Critical Current

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  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

PURPOSE:To simplify a rotary mechanism, to simplify the connection of a radiating element with an external part and to set a system to be with stand considerable shift or vibration by rotating only a reflecting mirror. CONSTITUTION:The rotation of a motor 16 is transmitted to the inner gear 14 of a rotor 13 through a gear 17 fixed to a motor shaft and the rotor 13 rotates. An electromagnetic wave generated in a radar circuit reaches the primary radiating element 7 in the focus of a paraboloid 1 through a transmission line 8, is radiated toward the paraboloid 1, is reflected and converged on the paraboloid 1 and is emitted toward the direction of the center line of the paraboloid 1 with maintaining sharp directivity. Since the paraboloid 1 forms a part of the rotor 13 and is continuously rotating, the electromagnetic wave reflected on the paraboloid 1 and emitted in scan space is in a direction where a conical surface at a vertical angle 2theta as against the rotary center line of the rotor 13, namely, the flight direction of a flying body is set to be a locus. The electromagnetic wave discharged in scan space reaches an investigating object and a reflected wave from the investigating object is reflected on the paraboloid 1, is converged on the primary radiating element 1 in the focus of the paraboloid 1 and is guided to a radar circuit through the transmission line 8.

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は、ミサイル1砲弾等の飛翔体に搭載される標的
検出用の走査アンテナに関する。
DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention relates to a scanning antenna for target detection mounted on a flying object such as a missile shell.

(従来の技術) 従来この種の装置としては、固定された円錐形ホーンと
、回転する反射鏡とよりなるレーダ用アンテナ装置(実
開昭59−61615号公報)、固定されている1次放
射系に対応して、曲面反射鏡を所定の軌道に沿って移動
させる空中線装置(特開昭61−74402号公報)、
球面形状を有する主反射鏡と2枚の補助反射鏡を設け、
この補助反射鏡を回転させる球面鏡アンテナ(特開昭5
2= 73655号公報)なとがmxされていた。
(Prior Art) Conventionally, this type of device includes a radar antenna device (Japanese Utility Model Application Publication No. 59-61615) consisting of a fixed conical horn and a rotating reflector, and a fixed primary radiation An antenna device that moves a curved reflecting mirror along a predetermined trajectory in accordance with the system (Japanese Patent Laid-Open No. 61-74402);
A main reflecting mirror with a spherical shape and two auxiliary reflecting mirrors are installed.
A spherical mirror antenna that rotates this auxiliary reflector (Japanese Unexamined Patent Publication No. 5
2 = Publication No. 73655) was mxed.

(発明が解決しようとする課It) これらの提案は、おおむね構造が複雑であり、機械的堅
牢さに乏しいため、飛翔体用のアンテナ装置としては好
ましくないという欠点を伴っていた。
(Problem to be Solved by the Invention) These proposals generally have a complicated structure and lack mechanical robustness, so they have the disadvantage that they are not suitable as antenna devices for flying objects.

本発明は上記の欠点を改善し、簡単な駆動機構で作動し
、かつ可撓性伝送路を必要とせず、しかし飛翔体などの
極度の移動に対しても耐えうる走査アンテナを提供する
ことを目的とする。
The present invention aims to improve the above-mentioned drawbacks and provide a scanning antenna that operates with a simple drive mechanism, does not require a flexible transmission path, and yet can withstand extreme movements such as those of a flying object. purpose.

(課題を解決するための手段) 上記の目的を達成するため、本発明は放物面の形状と一
致する反射鏡と、前記放物面の焦点を通り、かつ前記°
放物面の中心軸と、一定の角度をもつ軸を回転軸として
前記反射鏡を回転せしめる手段と、前記放物面の焦点に
設けた輻射器と、前記回転軸と反射鏡とが交わる位置に
おいて、前記反射鏡に設けた孔を遺して、前記輻射器と
接続される伝送路とを備えることを特徴とする走査アン
テナを発明の要旨とするものである。
(Means for Solving the Problems) In order to achieve the above object, the present invention includes a reflecting mirror that matches the shape of a paraboloid, and a mirror that passes through the focal point of the paraboloid and the angle
A means for rotating the reflecting mirror about an axis having a fixed angle with the central axis of the paraboloid, a radiator provided at the focal point of the paraboloid, and a position where the rotating axis and the reflecting mirror intersect. The gist of the invention is a scanning antenna characterized in that the scanning antenna is provided with a transmission line connected to the radiator except for the hole provided in the reflecting mirror.

さらに、本発明は電波透過体よりなるドームを備えてな
る外殼と、前記外殼の内部に設けられ、かつドームの軸
方向に延び、中心に伝送路を収めるだめの孔を設けた軸
部を有する保持体と、一方の端面側に放物面が形成され
、他方の端面側には前記保持体に設けられた回転手段に
よって回転させる回転部と、前記放物面の中心線と、前
記回転体の回転軸とは所定の角度をもって配置されると
共に、前記放物面の焦点に配置された1次輻射器と接続
され、前記回転軸の中心に設けられた孔を貫通して配置
されでいる伝送路とを備えることを特徴とする走査アン
テナを発明の要旨とするものである。
Furthermore, the present invention has an outer shell comprising a dome made of a radio wave transmitting material, and a shaft portion provided inside the outer shell, extending in the axial direction of the dome, and having a hole in the center for accommodating a transmission path. a holder, a rotating part having a paraboloid formed on one end surface and rotated by a rotation means provided on the holder on the other end surface, a center line of the paraboloid, and the rotating body. is arranged at a predetermined angle with the rotation axis, is connected to a primary radiator placed at the focal point of the paraboloid, and is placed through a hole provided at the center of the rotation axis. The gist of the invention is a scanning antenna characterized by comprising a transmission path.

(作用) 本発明は叙上のように反射鏡のみを回転させるのみであ
るので、回転機構を簡単化することができ、かつ輻射器
と外部との接続も簡単であり、かつ極度の移動あるいは
震動にも耐えることができる。
(Function) As described above, the present invention only rotates the reflecting mirror, so the rotating mechanism can be simplified, and the connection between the radiator and the outside is also simple, and it is possible to avoid extreme movement or It can also withstand vibrations.

(実施例1) 次に本発明の実施例について説明する。(Example 1) Next, examples of the present invention will be described.

第1図は本発明の走査アンテナを示すもので、図におい
て、1は放物面であり、2はこの放物面1を回転させた
場合の中心軸、3はこの放物面の底の部分に設けられ、
回転放物面の形状と一致する反射鏡、4はこの反射鏡の
一部に形成した孔、6は前記の放物面の焦点で、5はこ
の焦点を通り、かつ中心軸2と所望の角度をもつ回転軸
で、孔4は、この回転軸5と反射鏡3とが交わる位置に
設けられている。7は放物面の焦点に設けられた1次輻
射器で、前記の孔4を遺り、輻射器7に伝送路8が接続
されている。
Figure 1 shows the scanning antenna of the present invention. In the figure, 1 is a paraboloid, 2 is the central axis when the paraboloid 1 is rotated, and 3 is the bottom of the paraboloid. provided in the part,
A reflecting mirror matching the shape of the paraboloid of revolution, 4 a hole formed in a part of this reflecting mirror, 6 the focal point of the paraboloid, 5 passing through this focal point, and aligning with the central axis 2 as desired. The rotation axis has an angle, and the hole 4 is provided at a position where the rotation axis 5 and the reflecting mirror 3 intersect. Reference numeral 7 denotes a primary radiator provided at the focal point of the paraboloid, and a transmission line 8 is connected to the radiator 7 with the hole 4 still mentioned above.

次に動作について説明する。Next, the operation will be explained.

(イ)輻射器7は回転放物面1の無点6におかれ、かつ
反射鏡3はその中心輪2と任意の角度をもつ回転軸5を
中心軸として回転する。
(a) The radiator 7 is placed at a pointless point 6 on the paraboloid of revolution 1, and the reflector 3 rotates about a rotation axis 5 having an arbitrary angle with the center ring 2 thereof.

(D)その為、反射113が回転しても、焦点6及び輻
射器7の位置は常に固定されたままである。
(D) Therefore, even if the reflector 113 rotates, the positions of the focal point 6 and the radiator 7 always remain fixed.

(71)従って、回転放物面の中心軸2は、焦点6を固
定点として円錐運動をすることになる。
(71) Therefore, the central axis 2 of the paraboloid of revolution makes a conical motion with the focal point 6 as a fixed point.

図の2’、 3’はそれぞれ180°回転したときの回
転放物面の中心軸の位置と反射鏡の位置を示す。
2' and 3' in the figure indicate the position of the center axis of the paraboloid of revolution and the position of the reflecting mirror when rotated by 180°, respectively.

この場合、伝送路8及び輻射器7は静止状態である。In this case, the transmission line 8 and the radiator 7 are in a stationary state.

(実施例2) 第3図は本発明になる走査アンテナを有する飛翔体の先
端部の断面を示す。10は飛翔体の外殼で、その先端に
は電波透過体でなるドーム11が固着されている。また
外殼IQの内部には回転機構保持体12が固定されてい
る0回転機構保持体12は中央断面が凸状に構成され、
その中心には後述する伝送路8が貫通する孔4を育する
。 13はその一端に放物面lを有する回転体で、放物
面1の中心軸2と、回転体13の中心軸5は所定の傾斜
角θを有し、且つ放物面1の焦点6は回転体130回転
輪5上に存在するように構成されて、回転機構保持体1
2に回転自由の状態で保持されている0回転体13の他
端側には内歯歯車14が構成されている。また、回転体
13の回転中心部には伝送Ws8が貫通する孔4が穿孔
されている。16はモータで、回転機構保持体12に固
定され、モータ16の回転軸には歯車17が固定されて
おり、内歯歯車14と係合している。伝送路8の一端は
放物面1の焦点にある1次輻射器7に、他端は飛翔体内
の一部に搭載されたレーザ回路(図示せず)に前述の回
転機構保持体12の孔4を経て結合されている。
(Example 2) FIG. 3 shows a cross section of the tip of a flying object having a scanning antenna according to the present invention. 10 is the outer shell of the flying object, and a dome 11 made of a radio wave transparent material is fixed to the tip of the shell. Further, the rotation mechanism holder 12 is fixed inside the outer shell IQ, and the 0-rotation mechanism holder 12 has a convex central cross section.
A hole 4 is formed in the center thereof, through which a transmission line 8 to be described later passes. Reference numeral 13 denotes a rotating body having a paraboloid l at one end, the central axis 2 of the paraboloid 1 and the central axis 5 of the rotating body 13 have a predetermined inclination angle θ, and the focal point 6 of the paraboloid 1 is configured to exist on the rotating body 130 rotating wheel 5, and the rotating mechanism holder 1
An internal gear 14 is constructed on the other end side of the zero-rotating body 13 which is held in a rotatable state by the rotor 2. Further, a hole 4 through which the transmission Ws8 passes is bored in the center of rotation of the rotating body 13. A motor 16 is fixed to the rotating mechanism holder 12, and a gear 17 is fixed to the rotating shaft of the motor 16, and is engaged with the internal gear 14. One end of the transmission line 8 is connected to the primary radiator 7 located at the focal point of the paraboloid 1, and the other end is connected to a laser circuit (not shown) mounted in a part of the flying object through the hole in the rotating mechanism holder 12. They are connected through 4.

次に本発明の詳細な説明する。モータ16の回転はモー
タ軸に固定した歯車17を介し回転体13の内歯歯車1
4に伝わり、回転体13は回転をする。レーダ回路(図
示せず)で発生した電磁波は、伝送路8を経て放物面1
の焦点にある1次輻射器7に至り、放物面1に向けて放
射され、放物面1で反射して収束し鋭い指間性を維持し
て放物面lの中心線方向に発射される。一方、放物面l
は回転体13の一部を形成して絶えず回転しているから
放物面1で反射されて走査空間に発射されるt磁波は、
回転体13の回転中心線即ち、飛翔体の飛翔方向に対し
、頂角2θでなる円錐面を軌跡とする方向となる。
Next, the present invention will be explained in detail. The rotation of the motor 16 is caused by the internal gear 1 of the rotating body 13 via a gear 17 fixed to the motor shaft.
4, and the rotating body 13 rotates. Electromagnetic waves generated by a radar circuit (not shown) pass through a transmission path 8 to a paraboloid 1.
It reaches the primary radiator 7 at the focal point of , is emitted toward the paraboloid 1, is reflected by the paraboloid 1, converges, maintains a sharp interdigitation, and is emitted in the direction of the center line of the paraboloid L. be done. On the other hand, paraboloid l
forms part of the rotating body 13 and is constantly rotating, so the t magnetic wave reflected by the paraboloid 1 and emitted into the scanning space is
This is a direction in which the locus is a conical surface having an apex angle of 2θ with respect to the rotation center line of the rotating body 13, that is, the flight direction of the flying object.

走査空間に発射される電磁波が探査物体に到達し、探査
物体からの反射波は放物面1で反射されて放物面1の焦
点にある1次輻射器7に収束され、伝送路8を経てレー
ダ回路(図示せず)に導かれることは言うまでもない。
The electromagnetic wave emitted into the scanning space reaches the object to be explored, and the reflected wave from the object is reflected by the paraboloid 1 and converged on the primary radiator 7 at the focal point of the paraboloid 1, which transmits the transmission line 8. Needless to say, the signal is guided to a radar circuit (not shown) via the radar circuit.

(実施例3) 第4図に本発明の他の実施例を示す、前の実施例と異な
る所について説明する。前の実施例では、回転体13の
一端に放物面lが、他端側に内歯歯車14が構成されて
いたが、この実施例では回転体13は一端に放物面1が
構成され、他@便には外歯歯車18が構成されている。
(Embodiment 3) FIG. 4 shows another embodiment of the present invention, and the differences from the previous embodiment will be described. In the previous embodiment, the rotating body 13 had a paraboloid L at one end and the internal gear 14 at the other end, but in this embodiment, the rotating body 13 had a paraboloid 1 at one end. An external gear 18 is configured in the other @mail.

従ってモータ16の回転に伴って回転体13が回転する
Therefore, as the motor 16 rotates, the rotating body 13 rotates.

また作用については、第3図の実施例とほぼ同一である
Furthermore, the operation is almost the same as that of the embodiment shown in FIG.

(実施例4) 本発明の第4の実施例を以下に示す、第5図は本発明に
なる走査アンテナを育する飛翔体の先端部の断面を示す
、10は飛翔体の外殼で、その先端には電波透過体でな
るドーム11が固着されている。
(Embodiment 4) A fourth embodiment of the present invention is shown below. Fig. 5 shows a cross section of the tip of a flying object that grows a scanning antenna according to the present invention. 10 is the outer shell of the flying object; A dome 11 made of a radio wave transparent material is fixed to the tip.

また外殼10の内部には回転機構保持体12が固定され
ている0回転機構保持体12は中央断面が凸状に構成さ
れ、その中心には後述する伝送路8が貫通する孔4を有
する。 13はその一端に放物面1を有する回転体で、
放物面1の中心線2と、回転体13の中心線5は所定の
傾斜角θを有し、且つ放物面1の焦点は回転体13の中
心線上に存在するように構成されて、回転機構保持体1
2に回転自由の状態で保持されている。 19は回転機
構保持体】2に結合された固定子である。20は回転体
13に結合された回転子で、固定子19と回転子20で
アウターロータ型のモータ幻2を構成する。
Further, a rotation mechanism holder 12 is fixed inside the outer shell 10. The zero-rotation mechanism holder 12 has a convex central section, and has a hole 4 in the center thereof through which a transmission line 8, which will be described later, passes. 13 is a rotating body having a paraboloid 1 at one end,
The center line 2 of the paraboloid 1 and the center line 5 of the rotating body 13 have a predetermined inclination angle θ, and the focal point of the paraboloid 1 is located on the center line of the rotating body 13, Rotating mechanism holder 1
2, it is held in a freely rotational state. 19 is a stator coupled to the rotating mechanism holder [2]. A rotor 20 is connected to the rotating body 13, and the stator 19 and rotor 20 constitute an outer rotor type motor 2.

このモータ■によって回転体13を回転させる。The rotating body 13 is rotated by this motor (2).

その他の作用は第3図とほぼ同様である。Other operations are almost the same as in FIG. 3.

(発明の効果) 本発明は叡上のように形成されているため、反射鏡のみ
を回転させるので、輻射器を含む伝送路から高周波回路
および信号処理回路等が全て固定することができた。
(Effects of the Invention) Since the present invention is formed as above, only the reflecting mirror is rotated, so that all the high frequency circuits, signal processing circuits, etc. can be fixed from the transmission path including the radiator.

このため、可撓性をもった伝送路を必要としなくなり、
ロータリージツイントも不要になった。
This eliminates the need for flexible transmission lines,
The rotary socket is no longer needed.

従って、耐久性に冨み、雑音発生の恐れもなくなり、反
射鏡も単純に回転連動させるだけの構造としたため、飛
翔体の発射時の加速度に耐える構造設計も容易にしうる
効果を有するものである。
Therefore, it is highly durable, eliminates the risk of noise generation, and has the effect of making it easier to design a structure that can withstand the acceleration of a flying object because the reflector is simply rotated in conjunction with the structure. .

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

第1図は本発明の走査アンテナの実施例、第2図は動作
説明図、第3図乃至第5図は本発明の他の実施例を示す
。 1・・・放物面     2・・・中心軸3・・・反射
@     4・・・孔 5・・・回転軸     6・・・焦点7・・・1次輻
射器   8・・・伝送路10・・・外殼      
11・・・ドーム12・・・回転機構保持体 13・・
・回転体14・・・内歯歯車    16・・・モータ
17・・・歯車      18・・・外歯歯車19・
・・固定子     20・・・回転子■・・・モータ 第 囚 第 図 第3図
FIG. 1 shows an embodiment of the scanning antenna of the present invention, FIG. 2 is an explanatory diagram of the operation, and FIGS. 3 to 5 show other embodiments of the present invention. 1... Paraboloid 2... Central axis 3... Reflection @ 4... Hole 5... Rotation axis 6... Focal point 7... Primary radiator 8... Transmission line 10 ...outer shell
11...Dome 12...Rotating mechanism holder 13...
・Rotating body 14...Internal gear 16...Motor 17...Gear 18...External gear 19・
...Stator 20...Rotor■...Motor Figure 3

Claims (2)

【特許請求の範囲】[Claims] (1)放物面の形状と一致する反射鏡と、前記放物面の
焦点を通り、かつ前記放物面の中心軸と、一定の角度を
もつ軸を回転軸として前記反射鏡を回転せしめる手段と
、前記放物面の焦点に設けた輻射器と、前記回転軸と反
射鏡とが交わる位置において、前記反射鏡に設けた孔を
通して、前記輻射器と接続される伝送路とを備えること
を特徴とする走査アンテナ。
(1) A reflecting mirror that matches the shape of a paraboloid, and the reflecting mirror is rotated about an axis that passes through the focal point of the paraboloid and has a constant angle with the central axis of the paraboloid. means, a radiator provided at the focal point of the paraboloid, and a transmission line connected to the radiator through a hole provided in the reflecting mirror at a position where the rotation axis and the reflecting mirror intersect. A scanning antenna featuring:
(2)電波透過体よりなるドームを備えてなる外殼と、
前記外殼の内部に設けられ、かつドームの軸方向に延び
、中心に伝送路を収めるための孔を設けた軸部を有する
保持体と、一方の端面側に放物面が形成され、他方の端
面側には前記保持体に設けられた回転手段によって回転
させる回転部と、前記放物面の中心線と、前記回転体の
回転軸とは所定の角度をもって配置されると共に、前記
放物面の焦点に配置された1次輻射器と接続され、前記
回転軸の中心に設けられた孔を貫通して配置されている
伝送路とを備えることを特徴とする走査アンテナ。
(2) an outer shell comprising a dome made of a radio wave transparent material;
A holder is provided inside the outer shell, extends in the axial direction of the dome, and has a shaft portion provided with a hole in the center for accommodating a transmission path, and a paraboloid is formed on one end surface side, and the other end surface is formed with a paraboloid. On the end face side, a rotating part rotated by a rotating means provided on the holder, a center line of the paraboloid, and a rotation axis of the rotating body are arranged at a predetermined angle, and the paraboloid a transmission line connected to a primary radiator placed at a focal point of the rotating shaft and passing through a hole provided at the center of the rotation axis.
JP2183650A 1990-07-11 1990-07-11 Scan antenna Pending JPH0470201A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2183650A JPH0470201A (en) 1990-07-11 1990-07-11 Scan antenna

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2183650A JPH0470201A (en) 1990-07-11 1990-07-11 Scan antenna

Publications (1)

Publication Number Publication Date
JPH0470201A true JPH0470201A (en) 1992-03-05

Family

ID=16139516

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2183650A Pending JPH0470201A (en) 1990-07-11 1990-07-11 Scan antenna

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6181271B1 (en) 1997-08-29 2001-01-30 Kabushiki Kaisha Toshiba Target locating system and approach guidance system
KR100395403B1 (en) * 2001-12-24 2003-08-21 유병섭 Rewinding rolling apparatus having a four head roll

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6181271B1 (en) 1997-08-29 2001-01-30 Kabushiki Kaisha Toshiba Target locating system and approach guidance system
KR100395403B1 (en) * 2001-12-24 2003-08-21 유병섭 Rewinding rolling apparatus having a four head roll

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