JPH077310A - Antenna system - Google Patents

Antenna system

Info

Publication number
JPH077310A
JPH077310A JP14641693A JP14641693A JPH077310A JP H077310 A JPH077310 A JP H077310A JP 14641693 A JP14641693 A JP 14641693A JP 14641693 A JP14641693 A JP 14641693A JP H077310 A JPH077310 A JP H077310A
Authority
JP
Japan
Prior art keywords
mounting
vibration
antenna
column
mounting base
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
JP14641693A
Other languages
Japanese (ja)
Inventor
Toshihiro Mori
年博 毛利
Masaaki Yamaguchi
正昭 山口
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.)
TOKYO ELECTRON SYST KK
Toshiba Corp
Original Assignee
TOKYO ELECTRON SYST KK
Toshiba 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 TOKYO ELECTRON SYST KK, Toshiba Corp filed Critical TOKYO ELECTRON SYST KK
Priority to JP14641693A priority Critical patent/JPH077310A/en
Publication of JPH077310A publication Critical patent/JPH077310A/en
Pending legal-status Critical Current

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Abstract

(57)【要約】 (修正有) 【目的】この発明は、高性能な防振特性を確保したうえ
で、防振特性の多様化を図り得るようにして、高精度な
アンテナ特性を実現することにある。 【構成】空中線11が指向制御自在に取付けられる支柱
10を取付基台13に球面軸受を介して自在状に結合す
ると共に、弾性支持部材を介して直立状に弾性支持し、
さらに、支柱10に取付脚12を設けて、この取付脚1
2を非線形ばね及び摩擦材を組合わせたダンパーを介在
して取付基台13に設置するように構成して、所期の目
的を達成したものである。
(57) [Summary] (Modified) [Object] The present invention realizes highly accurate antenna characteristics by ensuring high-performance anti-vibration characteristics and enabling diversification of anti-vibration characteristics. Especially. [Structure] A column 10 to which an antenna 11 is attached so that its direction can be controlled is freely connected to a mounting base 13 via a spherical bearing, and elastically supported in an upright state via an elastic support member.
Further, a mounting leg 12 is provided on the column 10, and the mounting leg 1
2 is configured to be installed on the mounting base 13 with a damper, which is a combination of a non-linear spring and a friction material, interposed and the intended purpose is achieved.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】この発明は、例えば船舶や車両等
の移動体に搭載するのに好適する空中線装置に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an antenna device suitable for mounting on a moving body such as a ship or a vehicle.

【0002】[0002]

【従来の技術】従来より、船舶に搭載される空中線装置
においては、全天空に対する指向特性が要求されること
で、支柱の先端部に指向制御自在に取付けられる、いわ
ゆる倒立振子型の取付構造が採られる。このような取付
構造としては、USP,No4582291等が知られ
ており、図9に示すように空中線1が支柱2の先端に指
向制御自在に取付けられる。この支柱2の基端には、複
数の脚2aが船舶に設けられる取付基台3に対応して形
成され、この基端側が球面軸受4を介して取付基台に自
在状に結合される(図10参照)。そして、この支柱2
は、図11に示すように球面軸受4を介して取付基台3
に自在状に結合された状態で、弾性支持部材5を用いて
取付基台3に対して直立状に弾性支持される。この弾性
支持部材5は、その固有振動数ωが図12に示すよう
に、中央復帰ばね力を支柱に与え、そのばね定数をk、
支柱2の脚の長さをr、空中線の質量をm、重力加速度
をg、支柱の長さをl、慣性モーメントをIとすると、 ω=((kr2 −mgl)/I)1/2 の式で表される。これは、弾性支持部材5のばね定数k
を小さく設定すると、固有振動数ωが低下されて、取付
基台3の傾きが大きくなると、ばねが押し潰されて振動
系として役を果たさなくなり、他方、ばね定数kを大き
く設定すると、その固有振動数ωが高くなり、防振機能
がなくなることにより、これらを考慮したばね定数kに
設定される。
2. Description of the Related Art Conventionally, an antenna device mounted on a ship is required to have directional characteristics with respect to the whole sky, so that there is a so-called inverted pendulum type mounting structure which is directionally controllably mounted on a tip of a column. To be taken. As such a mounting structure, USP, No. 4582291 or the like is known, and as shown in FIG. 9, the antenna 1 is mounted on the tip of the support column 2 so that the orientation can be controlled. A plurality of legs 2a are formed at the base end of the support column 2 so as to correspond to a mounting base 3 provided on the ship, and the base end side is freely connected to the mounting base via a spherical bearing 4 ( (See FIG. 10). And this prop 2
Is mounted through the spherical bearing 4 as shown in FIG.
Is elastically supported in an upright state with respect to the mounting base 3 by using the elastic support member 5 in a state of being freely connected. As shown in FIG. 12, the elastic support member 5 applies a central return spring force to the support column so that its natural frequency ω is k,
Assuming that the leg length of the column 2 is r, the mass of the antenna is m, the gravitational acceleration is g, the column length is l, and the moment of inertia is I, then ω = ((kr 2 −mgl) / I) 1/2 It is expressed by the formula. This is the spring constant k of the elastic support member 5.
If is set to a small value, the natural frequency ω is decreased, and if the inclination of the mounting base 3 is increased, the spring is crushed and does not serve as a vibration system. On the other hand, if the spring constant k is set to a large value, Since the frequency ω becomes high and the vibration damping function is lost, the spring constant k is set in consideration of these.

【0003】また、支柱2の脚の先端部には、リミッタ
6が設けられ、このリミッタ6を介して支柱が一定以上
傾斜しないように位置規制される。上記構成において、
支柱2、球面軸受4及び弾性支持部材5は、取付基台3
が水平で、しかも振動の振幅の小さな状態において、協
働して振動系を形成し、取付基台からの振動を防振して
支柱上の空中線1への振動の伝達を防止する。
A limiter 6 is provided at the tip of the leg of the column 2, and the position of the column is regulated by the limiter 6 so that the column does not tilt more than a certain amount. In the above configuration,
The pillar 2, the spherical bearing 4, and the elastic support member 5 are mounted on the mounting base 3.
Is horizontal and has a small vibration amplitude, they cooperate to form a vibration system to prevent vibration from the mounting base and prevent transmission of the vibration to the antenna 1 on the column.

【0004】しかしながら、上記空中線装置では、その
防振構造上、比較的動揺が小さく、しかも取付構造の固
有振動数を高くすることが可能な大型船舶に搭載するこ
とにより、効果的な防振を行うことが可能であるが、比
較的動揺が大きく、しかも取付構造の固有振動数を高く
することが困難な小型船舶に搭載すると、その振動系の
構造上、効果的な防振が困難で、適用範囲に制約を有す
るという問題を有する。即ち、小型船舶にあっては、船
舶の積載重量等の関係上、取付基台への取付構造を十分
に強固に形成して、取付構造の固有振動数を高く設定す
るのが困難であるうえ、その動揺が大型船舶に比して大
きいために、振動系としての固有振動数をさらに下げな
ければ効果的な防振ができないが、前述したばね定数k
の設定上の制約により、対応が困難なものである。
However, due to the vibration isolation structure of the antenna device, it is possible to provide effective vibration isolation by mounting it on a large ship that is relatively stable and has a high natural frequency of the mounting structure. Although it is possible to do it, when it is mounted on a small ship that is relatively swaying and it is difficult to increase the natural frequency of the mounting structure, effective vibration isolation is difficult due to the structure of its vibration system, There is a problem in that the application range is limited. That is, in the case of a small boat, it is difficult to set the natural frequency of the mounting structure to a high value by forming the mounting structure to the mounting base sufficiently strong because of the loading weight of the ship. However, since the vibration is larger than that of a large ship, effective vibration isolation cannot be achieved unless the natural frequency of the vibration system is further reduced.
It is difficult to deal with due to the setting restrictions of.

【0005】この移動体搭載型空中線装置における防振
の問題は、空中線1の指向性の関係上、その取付構造
が、いわゆる倒立振子型等のトップヘビー構造となるた
めに、その耐防振・耐衝撃性能がアンテナ特性に直接的
に影響を及ぼすことで、重大な課題となっている。
The problem of anti-vibration in this mobile-mounted antenna device is that, due to the directivity of the antenna 1, the mounting structure is a so-called inverted pendulum-type top heavy structure, so that the anti-vibration The impact resistance directly affects the antenna characteristics, which is a serious problem.

【0006】[0006]

【発明が解決しようとする課題】以上述べたように、従
来の空中線装置では、振動系の構造上、動揺が大きな船
舶に搭載すると、満足の行く防振特性を得るのが困難
で、アンテナ特性の低下を招くという問題を有する。
As described above, in the conventional antenna device, it is difficult to obtain a satisfactory vibration damping characteristic when the antenna is mounted on a ship with great vibration due to the structure of the vibration system. However, there is a problem in that

【0007】この発明は上記の事情に鑑みてなされたも
ので、高性能な防振特性を確保したうえで、防振特性の
多様化を図り得るようにして、高精度なアンテナ特性を
実現した空中線装置を提供することを目的とする。
The present invention has been made in view of the above circumstances, and achieves highly accurate antenna characteristics by ensuring high-performance vibration-damping characteristics and diversifying the vibration-damping characteristics. It is an object to provide an antenna device.

【0008】[0008]

【課題を解決するための手段】この発明は、先端部に空
中線が指向制御自在に取付けられ、基端に複数の取付脚
が取付基台に対応して放射状に設けられる支柱と、この
支柱の前記取付脚側の一端を前記取付基台に自在状に結
合する自在継手手段と、前記支柱を取付基台に対して略
直立状に弾性支持する弾性支持手段と、前記取付基台に
取付けられ、前記支柱の取付脚に対して非線形弾性力を
与える弾性体部及び振動減衰力を与える摩擦体部を有し
たダンパー手段とを備えて空中線装置を構成したもので
ある。
SUMMARY OF THE INVENTION According to the present invention, an antenna is attached to a tip end portion of the antenna in a directionally controllable manner, and a plurality of mounting legs are radially provided at a base end corresponding to a mounting base. Universal joint means for freely connecting one end of the mounting leg side to the mounting base, elastic supporting means for elastically supporting the support column in a substantially upright state with respect to the mounting base, and mounted on the mounting base. The antenna device is configured by including an elastic body portion that gives a non-linear elastic force to the mounting leg of the support column and a damper means having a friction body portion that gives a vibration damping force.

【0009】[0009]

【作用】上記構成によれば、支柱は、弾性支持手段によ
り、中央復帰力が付与されると共に、ダンパー手段によ
り、非線形弾性力と振動減衰力が付与されることによ
り、弾性支持手段で小さい振動が防振され、ダンパー手
段で大きい振動の防振と振動の減衰を実行する。これに
より、取付構造の固有振動数に影響されることなく、取
付基台の小さい動揺、あるいは大きな動揺に伴う振動を
効果的に防振及び減衰することが可能となる。
According to the above construction, the elastic support means imparts a central restoring force to the support column, and the damper means imparts a non-linear elastic force and a vibration damping force. The anti-vibration is performed, and the damper means executes the anti-vibration of the large vibration and the damping of the vibration. As a result, it is possible to effectively prevent and damp the vibration associated with the small shaking or the large shaking of the mounting base without being affected by the natural frequency of the mounting structure.

【0010】[0010]

【実施例】以下、この発明の実施例について、図面を参
照して詳細に説明する。図1はこの発明の一実施例に係
る空中線装置を示すもので、取付用支柱10の先端に
は、空中線11が指向制御自在に取付けられる。支柱1
0の基端には、放射状に複数の取付脚12が船舶に設け
られる取付基台13に対向して設けられ、この取付脚1
2には、図2に示すように先端に凹状の係止部12aが
それぞれ設けられる。そして、取付脚12の係止部12
aには、ダンパー14が取付けられる。
Embodiments of the present invention will be described below in detail with reference to the drawings. FIG. 1 shows an antenna apparatus according to an embodiment of the present invention. An antenna 11 is attached to the tip of a mounting column 10 so that the pointing of the antenna 11 can be controlled. Prop 1
At the base end of 0, a plurality of mounting legs 12 are provided radially opposite to a mounting base 13 provided on the ship.
As shown in FIG. 2, each of the 2 is provided with a recessed locking portion 12a at the tip thereof. Then, the locking portion 12 of the mounting leg 12
The damper 14 is attached to a.

【0011】ダンパー14は、例えば図3に示すよう
に、第1及び第2の筒体14a,14bが取付体14c
に対して軸方向に移動自在に組合わされ、これら第1及
び第2の筒体14a,14b間には、図4に示すばね特
性を持つ非線形ばね14dと摩擦部材14eが介在され
る。このうち第1の筒体14aには、係止溝14fが上
記取付脚12の係止部12aに対応して形成され、この
係止溝14fには、取付脚12の係止部12aが挿着さ
れる。そして、取付体14cは、ボルト14gを介して
上記取付基台133に取付けられる。
In the damper 14, for example, as shown in FIG. 3, first and second cylindrical bodies 14a and 14b are attached to a mounting body 14c.
And a non-linear spring 14d having a spring characteristic shown in FIG. 4 and a friction member 14e are interposed between the first and second cylindrical bodies 14a and 14b. Of these, a locking groove 14f is formed in the first cylindrical body 14a so as to correspond to the locking portion 12a of the mounting leg 12, and the locking portion 12a of the mounting leg 12 is inserted in the locking groove 14f. Be worn. Then, the mounting body 14c is mounted on the mounting base 133 via the bolt 14g.

【0012】また、上記支柱10は、その基端側が前述
したよう球面軸受4(図10参照)を介して取付基台1
3に自在状に結合されると共に、弾性支持部材5(図1
0参照)を用いて取付基台13に対して直立状に弾性支
持され、空中線11を、いわゆる倒立振子型に設置す
る。
The base 10 of the column 10 is mounted on the mounting base 1 via the spherical bearing 4 (see FIG. 10) as described above.
3 and the elastic support member 5 (see FIG. 1).
(Refer to 0), the antenna 11 is elastically supported in an upright state with respect to the mounting base 13, and the antenna 11 is installed in a so-called inverted pendulum type.

【0013】なお、上記支柱10の取付脚12として
は、空中線10の指向方向に応じて、2箇所以上形成さ
れる。上記構成において、取付基台13に振動が加わる
と、弾性支持部材5、ダンパー14が作用して、振動の
防振と共に、減衰を行い支柱10を介して空中線11に
伝播されるのを防止する。即ち、ダンパー14は、図5
に示す防振構造を取り、取付基台13に振動が加わる
と、比較的小さい振動が弾性支持部材5により防振さ
れ、比較的大きな振動がダンパー14の非線形ばね14
dにより防振される。同時に、ダンパー14は、図6に
示すように摩擦材14eの減衰力で振動を減衰する。こ
れにより、支柱10の先端部の空中線11は、取付基台
13に加わる振動や衝撃に影響されることなく、高精度
な指向制御が可能となる。
The mounting legs 12 of the support column 10 are formed in two or more places depending on the direction of the antenna 10. In the above configuration, when vibration is applied to the mounting base 13, the elastic support member 5 and the damper 14 act to dampen the vibration and prevent it from propagating to the antenna 11 via the column 10. . That is, the damper 14 is shown in FIG.
When a vibration is applied to the mounting base 13 by taking the vibration damping structure shown in FIG. 2, a relatively small vibration is damped by the elastic support member 5, and a relatively large vibration is damped by the nonlinear spring 14 of the damper 14.
Anti-vibration due to d. At the same time, the damper 14 damps the vibration by the damping force of the friction material 14e as shown in FIG. As a result, the antenna 11 at the tip of the column 10 can be controlled with high accuracy without being affected by the vibration or shock applied to the mounting base 13.

【0014】なお、この発明による防振構造を用いて振
動試験を行った結果、図7に示すように効果的な防振特
性が得られ、図8に示す従来の形式による防振特性に比
して効果的に向上されることが確認される。
As a result of a vibration test using the vibration-proof structure according to the present invention, effective vibration-proof characteristics are obtained as shown in FIG. 7, which is in comparison with the conventional type vibration-proof characteristics shown in FIG. It is confirmed that it is effectively improved.

【0015】このように、上記空中線装置は、空中線1
1が指向制御自在に取付けられる支柱10を取付基台1
3に球面軸受4を介して自在状に結合すると共に、弾性
支持部材5を介して直立状に弾性支持し、さらに、支柱
10に取付脚12を設けて、この取付脚12を非線形ば
ね14d及び摩擦材14eを組合わせたダンパー14を
介在して取付基台13に設置するように構成した。
As described above, the antenna device is used in the antenna 1
1 is a support base 1 on which a directional control can be freely mounted
3 is freely connected to the shaft 3 via a spherical bearing 4, and is elastically supported in an upright state via an elastic support member 5. Further, a mounting leg 12 is provided on the support column 10, and the mounting leg 12 is connected to the nonlinear spring 14d and It was configured to be installed on the mounting base 13 with a damper 14 that is a combination of friction materials 14e interposed.

【0016】これによれば、取付基台13に振動が加わ
ると、弾性支持部材5により与えられる中央復帰力によ
り小さい振動を防振し、ダンパー14の非線形ばね14
dの弾性力で大きな振動を防振し、その摩擦材14eの
振動減衰振動減衰力で振動を減衰することにより、取付
基台13の小さい動揺、あるいは大きな動揺に伴う振動
を効果的に防振及び減衰する。従って、大型の船舶や、
小型の船舶に搭載する場合、特別に取付構造を強固にし
たりすることなく、効果的な防振機能を得ることがで
き、振動や衝撃とは、無関係に空中線11の指向制御が
可能となり、高精度なアンテナ特性が得られる。
According to this, when vibration is applied to the mounting base 13, a smaller vibration is suppressed by the central restoring force given by the elastic support member 5, and the nonlinear spring 14 of the damper 14 is prevented.
Large vibrations are damped by the elastic force of d, and vibrations are damped by the vibration damping vibration damping force of the friction material 14e, so that vibrations associated with small or large shaking of the mounting base 13 are effectively damped. And decay. Therefore, large vessels,
When mounted on a small vessel, an effective anti-vibration function can be obtained without specially strengthening the mounting structure, and the pointing control of the antenna 11 can be performed regardless of vibration and shock, and high Accurate antenna characteristics can be obtained.

【0017】また、これによれば、そのダンパー構造
上、ダンパー14を最小限まで、薄形化することが可能
となるという効用を有する。なお、上記実施例では、ダ
ンパー14として、非線形ばね14d及び振動減衰用の
摩擦材14eを一体的に組合わせたものを用いて構成し
たが、これに限ることなく、例えば非線形ばね14d及
び摩擦材14eを分離して、これら非線形ばね14d、
あるいは摩擦材14eの一方を支柱の取付脚毎に単独に
配設するように構成しても良い。
Further, according to this, there is an advantage that the damper 14 can be thinned to the minimum due to its damper structure. In the above embodiment, the damper 14 is configured by integrally combining the non-linear spring 14d and the vibration damping friction material 14e, but the damper 14 is not limited to this. 14e is separated and these nonlinear springs 14d,
Alternatively, one of the friction members 14e may be separately provided for each mounting leg of the support column.

【0018】また、上記ダンパー14と支柱10の取付
脚12との取付手段としては、上記実施例のように取付
脚12に係止部12aを設け、ダンパー14の第1の筒
体14aに係止溝14fを設けて相互を取付けるように
構成したが、これに限ることなく、フランジを用いて取
付けたり、各種の取付手段で構成することが可能であ
る。
As a means for attaching the damper 14 to the mounting leg 12 of the column 10, a locking portion 12a is provided on the mounting leg 12 as in the above embodiment, and is engaged with the first cylindrical body 14a of the damper 14. Although the groove 14f is provided so as to be attached to each other, the present invention is not limited to this, and it is possible to use a flange or various attachment means.

【0019】さらに、上記実施例では、船舶に搭載する
ように構成した場合を代表して説明したが、これに限る
ことなく、自動車等の移動体に搭載するように構成する
ことも可能である。よって、この発明は、上記実施例に
限ることなく、その他、この発明の要旨を逸脱しない範
囲で種々の変形を実施し得ることは勿論である。
Furthermore, in the above-mentioned embodiment, the case of being configured to be mounted on a ship was described as a representative, but the present invention is not limited to this, and it may be configured to be mounted on a moving body such as an automobile. . Therefore, the present invention is not limited to the above-described embodiments, and it is needless to say that various modifications can be made without departing from the gist of the present invention.

【0020】[0020]

【発明の効果】以上詳述したように、この発明によれ
ば、高性能な防振特性を確保したうえで、防振特性の多
様化を図り得るようにして、高精度なアンテナ特性を実
現した空中線装置を提供することができる。
As described in detail above, according to the present invention, it is possible to achieve high-precision antenna characteristics by ensuring high-performance anti-vibration characteristics and diversifying anti-vibration characteristics. The antenna device can be provided.

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

【図1】この発明の一実施例に係る空中線装置を示した
図。
FIG. 1 is a diagram showing an antenna device according to an embodiment of the present invention.

【図2】図1の取付脚の詳細を示した図。FIG. 2 is a diagram showing details of a mounting leg of FIG.

【図3】図1のダンパーを取出して示した図。FIG. 3 is a diagram showing the damper of FIG. 1 taken out.

【図4】図1のダンパーの非線形ばねのばね特性を示し
た図。
FIG. 4 is a diagram showing spring characteristics of a nonlinear spring of the damper shown in FIG.

【図5】図1の防振構造の概念を示した図。FIG. 5 is a diagram showing the concept of the vibration isolation structure of FIG. 1.

【図6】図1のダンパーのダンパー特性を示した図。FIG. 6 is a diagram showing damper characteristics of the damper shown in FIG.

【図7】図1の防振特性を示した図。FIG. 7 is a diagram showing the image stabilization characteristics of FIG.

【図8】従来の空中線装置の防振特性を示した図。FIG. 8 is a diagram showing a vibration isolation characteristic of a conventional antenna device.

【図9】従来の空中線装置を示した図。FIG. 9 is a diagram showing a conventional antenna device.

【図10】図9の一部詳細を示した図。FIG. 10 is a diagram showing a part of the details of FIG. 9;

【図11】図9の一部詳細を示した図。FIG. 11 is a diagram showing a part of details of FIG. 9;

【図12】図9の防振構造の概念を示した図。FIG. 12 is a view showing the concept of the image stabilization structure of FIG.

【符号の説明】[Explanation of symbols]

4…球面軸受。 5…弾性支持部材。 10…支柱。 11…空中線。 12…取付脚。 13…取付基台。 14…ダンパー。 14a…第1の筒体。 14b…第2の筒体。 14c…取付体。 14d…非線形ばね。 14e…摩擦材。 14f…係止溝。 14g…ボルト。 4 ... Spherical bearing. 5 ... Elastic support member. 10 ... Posts. 11 ... Antenna. 12 ... Mounting legs. 13 ... Mounting base. 14 ... Damper. 14a ... 1st cylinder. 14b ... 2nd cylinder. 14c ... Mounting body. 14d ... Non-linear spring. 14e ... Friction material. 14f ... Locking groove. 14g ... bolt.

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】 先端部に空中線が指向制御自在に取付け
られ、基端に複数の取付脚が取付基台に対応して放射状
に設けられる支柱と、 この支柱の前記取付脚側の一端を前記取付基台に自在状
に結合する自在継手手段と、 前記支柱を取付基台に対して略直立状に弾性支持する弾
性支持手段と、 前記取付基台に取付けられ、前記支柱の取付脚に対して
非線形弾性力を与える弾性体部及び振動減衰力を与える
摩擦体部を有したダンパー手段とを具備した空中線装
置。
1. A column having an antenna attached to the tip end portion thereof so as to be capable of directivity control, and a plurality of mounting legs radially provided at the base end corresponding to the mounting base, and one end of the column on the side of the mounting leg. Universal joint means for freely connecting to the mounting base, elastic supporting means for elastically supporting the support column in a substantially upright state with respect to the mounting base, and mounting means for mounting the support base to the mounting legs of the support column. Antenna device including an elastic body portion that applies a nonlinear elastic force and a damper means that has a friction body portion that applies a vibration damping force.
【請求項2】 前記ダンパー手段は、前記弾性体部及び
摩擦体部が、前記支柱の取付脚毎に分離して配置されて
なることを特徴とする請求項1記載の空中線装置。
2. The antenna device according to claim 1, wherein the damper means is configured such that the elastic body portion and the friction body portion are separately arranged for each mounting leg of the support column.
JP14641693A 1993-06-17 1993-06-17 Antenna system Pending JPH077310A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP14641693A JPH077310A (en) 1993-06-17 1993-06-17 Antenna system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP14641693A JPH077310A (en) 1993-06-17 1993-06-17 Antenna system

Publications (1)

Publication Number Publication Date
JPH077310A true JPH077310A (en) 1995-01-10

Family

ID=15407201

Family Applications (1)

Application Number Title Priority Date Filing Date
JP14641693A Pending JPH077310A (en) 1993-06-17 1993-06-17 Antenna system

Country Status (1)

Country Link
JP (1) JPH077310A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0961510A (en) * 1995-08-22 1997-03-07 Hitachi Zosen Corp Position detection device by GPS
JP2008228045A (en) * 2007-03-14 2008-09-25 Mitsubishi Electric Corp Satellite tracking antenna device

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0961510A (en) * 1995-08-22 1997-03-07 Hitachi Zosen Corp Position detection device by GPS
JP2008228045A (en) * 2007-03-14 2008-09-25 Mitsubishi Electric Corp Satellite tracking antenna device

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