JPH052426U - Helical antenna - Google Patents
Helical antennaInfo
- Publication number
- JPH052426U JPH052426U JP359991U JP359991U JPH052426U JP H052426 U JPH052426 U JP H052426U JP 359991 U JP359991 U JP 359991U JP 359991 U JP359991 U JP 359991U JP H052426 U JPH052426 U JP H052426U
- Authority
- JP
- Japan
- Prior art keywords
- cylinder
- helical antenna
- conductor
- camphor
- satellite
- 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
Links
Landscapes
- Details Of Aerials (AREA)
Abstract
(57)【要約】
【目的】 衛星搭載用ヘリカルアンテナにおいて、従来
はその構成品の一部であった誘電体円筒の存在のために
電磁波の伝送損失が大きく、電気特性が良くないという
課題があり、これを改善する必要があった。
【構成】 従来の誘電体円筒の代わりに樟脳円筒5を具
備させた。
【効果】 宇宙空間における運用時においては、樟脳円
筒5が昇華、消失してしまうため電気損失の小さく電気
特性の良好なヘリカルアンテナが得られる効果がある。
(57) [Summary] [Purpose] In the helical antenna mounted on a satellite, the transmission loss of electromagnetic waves is large due to the presence of a dielectric cylinder, which has been a part of the conventional components, and the electrical characteristics are not good. Yes, there was a need to improve this. [Structure] A camphor cylinder 5 is provided in place of the conventional dielectric cylinder. [Effect] During operation in outer space, the camphor cylinder 5 sublimates and disappears, so that there is an effect that a helical antenna with small electric loss and good electric characteristics can be obtained.
Description
【0001】[0001]
この考案は、宇宙空間などの高真空中で運用され、人工衛星等に搭載される通 信用のアンテナに関するものである。 The present invention relates to a trusted antenna that is operated in a high vacuum such as outer space and is mounted on an artificial satellite or the like.
【0002】[0002]
第3図は、例えば、電子情報通信学会編、アンテナ工学ハンドブック(オーム 社発行)のP73に示された技術を応用し設計された従来のヘリカルアンテナを 示す図であり、図において、1は誘電体の円筒、2は誘電体円筒1にらせん状に 巻き付けられた導体、3は導体2のらせん軸に垂直な面に設けられた反射板、4 はケーブルである。 FIG. 3 is a diagram showing a conventional helical antenna designed by applying the technology shown in P73 of Antenna Engineering Handbook (published by Ohmsha, Inc.) edited by The Institute of Electronics, Information and Communication Engineers, where 1 is a dielectric. The body cylinder, 2 is a conductor spirally wound around the dielectric cylinder 1, 3 is a reflector provided on a surface perpendicular to the spiral axis of the conductor 2, and 4 is a cable.
【0003】 このように構成されたヘリカルアンテナは、衛星内の送信部からケーブル4を 介し、導体2に給電され、導体2のらせん軸の方向に円偏波を放射する。また、 導体2は、地上においてはその自重のため、それ自身での寸法、形状の維持が難 しく、衛星打ち上げの際には、打ち上げの振動荷重に耐えられないという欠陥が あるため、誘電体円筒1に巻き付けられ保持されている。The helical antenna thus configured is fed to the conductor 2 from the transmitting section in the satellite via the cable 4 and radiates circularly polarized wave in the direction of the spiral axis of the conductor 2. In addition, the conductor 2 has a defect that it is difficult to maintain its own size and shape on the ground due to its own weight on the ground, and it cannot withstand the vibration load of the launch at the time of satellite launch. It is wound around and held on the cylinder 1.
【0004】[0004]
従来のヘリカルアンテナは、以上のように、導体2に誘電体円筒1が近接する 構成となっているため、アンテナの運用時、導体2を伝播する電磁波の伝送損失 が大きく電気特性が良くないという欠点があった。また、将来、より高性能な衛 星通信用アンテナが要求される状況下にあっては、本装置を適用できないという 課題があった。 As described above, the conventional helical antenna has the structure in which the dielectric cylinder 1 is in close proximity to the conductor 2, so that when the antenna is in operation, the transmission loss of electromagnetic waves propagating through the conductor 2 is large and the electrical characteristics are not good. There was a flaw. In addition, there is a problem that this device cannot be applied in the situation where a higher performance satellite communication antenna is required in the future.
【0005】 この考案は、上記のような課題を解消するためになされたもので、衛星打ち上 げ時の振動荷重に耐え、運用時には伝送損失が少さく、電気特性の良好なヘリカ ルアンテナを得ることを目的とする。The present invention has been made in order to solve the above problems, and obtains a helical antenna which withstands the vibration load at the time of launching a satellite, has little transmission loss during operation, and has good electric characteristics. The purpose is to
【0006】[0006]
この考案に係わるヘリカルアンテナは、従来の構成品である誘電体円筒の代わ りに、昇華性の物質である例えば樟脳によって形成された円筒を適用したもので ある。 The helical antenna according to the present invention employs a cylinder formed by a sublimable substance such as camphor instead of the conventional dielectric cylinder.
【0007】[0007]
この考案は、導体を保持する円筒を樟脳によって形成したことにより、導体を 、衛星打ち上げ時の振動荷重から保護するとともに、衛星が宇宙環境に投入され た後は、周囲気圧が著しく低下するため、樟脳円筒は急速に昇華し、宇宙空間に 拡散することとなり、宇宙空間での運用時におけるアンテナの構成は、導体と反 射板とケーブルだけのものとなる。 This invention protects the conductor from the vibration load at the time of launching the satellite by forming the cylinder holding the conductor by camphor, and the ambient atmospheric pressure drops significantly after the satellite is put into the space environment. The camphor cylinder rapidly sublimes and diffuses into outer space, and the antenna configuration during operation in outer space consists only of conductors, reflection plates, and cables.
【0008】[0008]
実施例1 以下この考案の一実施例について説明する。第1図は、この考案の収納時にお けるヘリカルアンテナを示す図、第2図は、この考案の運用時におけるヘリカル アンテナを示す図である。第1図及び第2図において、2はらせん状に成形され た導体、3は導体2のらせん軸にある垂直な面に設けられた反射板、4はケーブ ル、5は導体2を保持している樟脳円筒である。 上記のように構成されたヘリカルアンテナにおいて、樟脳円筒の5の大きさ、 形状は、大気中での昇華量を考慮したものでなければならない。 Embodiment 1 An embodiment of the present invention will be described below. FIG. 1 is a diagram showing the helical antenna when the device is stored, and FIG. 2 is a diagram showing the helical antenna when the device is operated. In FIGS. 1 and 2, 2 is a spirally-shaped conductor, 3 is a reflector provided on a plane perpendicular to the spiral axis of the conductor 2, 4 is a cable, and 5 is a conductor. It is a camphor cylinder. In the helical antenna configured as described above, the size and shape of the camphor cylinder 5 should be set in consideration of the amount of sublimation in the atmosphere.
【0009】 この考案によるヘリカルアンテナ、樟脳円筒5が、導体2を保持することによ り、地上においては、導体2の自重による変形を防止し、衛星打ち上げの際には 、打ち上げ振動荷重による導体2の損傷を防止することができる。また、衛星が 宇宙空間に投入された後は、周囲気圧の低下により、樟脳円筒5が急速に昇華、 拡散するため、第2図に示されるような状態となり、本装置の構成は、導体2と 反射板3とケーブル4だけのものとなる。なお、衛星の軌道上では、重力やその 他の本装置に影響を及ぼすような荷重は加わらないため、導体2を保持する必要 はない。The helical antenna and the camphor cylinder 5 according to the present invention hold the conductor 2 to prevent the conductor 2 from being deformed on the ground due to its own weight, and at the time of launching the satellite, the conductor due to the launching vibration load. The damage of 2 can be prevented. Also, after the satellite is put into outer space, the camphor cylinder 5 rapidly sublimes and diffuses due to the decrease in ambient pressure, and the state shown in FIG. 2 is reached. Only the reflector 3 and the cable 4 will be used. In the orbit of the satellite, it is not necessary to hold the conductor 2 because gravity and other loads that affect the device are not applied.
【0010】 なお、上記実施例では、右回りのらせん状導体の場合について示したが、左回 りのらせん状導体や、両回りのらせん状導体の構造、更には、多線巻ヘリカルア ンテナ等の装置に応用しても同様の効果を奏する。 また、上記実施例では、円筒材料に樟脳を適用した例を示したが、樟脳以外に もナフタリンやヨウ素などの昇華性物質であれば、同様の作用が期待できる。In the above embodiment, the case of the clockwise spiral conductor was shown, but the structure of the counterclockwise spiral conductor, the spiral conductors of both rotations, and further the multi-winding helical antenna, etc. The same effect can be obtained even when applied to the device. Further, in the above-mentioned examples, an example in which camphor is applied to the cylindrical material has been shown, but similar effects can be expected if a sublimable substance such as naphthalene or iodine is used in addition to camphor.
【0011】[0011]
以上のように、この考案によれば、ヘリカルアンテナのらせん状導体を樟脳円 筒により保持する構成としたので、衛星打ち上げの振動荷重に耐えることができ 、宇宙空間における運用時においては伝送損失の小さく電気特性の良好なものが 得られる効果がある。 As described above, according to the present invention, since the helical conductor of the helical antenna is held by the camphor cylinder, it is possible to withstand the vibration load of the satellite launch and to reduce the transmission loss during operation in outer space. The effect is that a small product with good electrical characteristics can be obtained.
【0012】[0012]
【図1】この考案の一実施例によるヘリカルアンテナの
収納時を示す図である。FIG. 1 is a diagram showing a helical antenna according to an embodiment of the present invention when it is stored.
【図2】この考案の一実施例によるヘリカルアンテナの
運用時を示す図である。FIG. 2 is a diagram showing the operation of the helical antenna according to the embodiment of the present invention.
【図3】従来のヘリカルアンテナを示す図である。FIG. 3 is a diagram showing a conventional helical antenna.
1 誘電体円筒 2 導体 3 反射板 4 ケーブル 5 樟脳円筒 1 Dielectric cylinder 2 Conductor 3 Reflector 4 Cable 5 Camphor cylinder
Claims (1)
と、前記円筒の外周に成形されたらせん状の導体、及び
前記導体のらせん軸に垂直な面に設けられた反射板とに
よって構成されたことを特徴とするヘリカルアンテナ。[Claims for utility model registration] [Claim 1] A cylinder made of camphor, which is a sublimable substance, a spiral conductor formed on the outer periphery of the cylinder, and a conductor perpendicular to the spiral axis of the conductor. A helical antenna, characterized in that it is composed of a reflector.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP359991U JPH052426U (en) | 1991-02-04 | 1991-02-04 | Helical antenna |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP359991U JPH052426U (en) | 1991-02-04 | 1991-02-04 | Helical antenna |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH052426U true JPH052426U (en) | 1993-01-14 |
Family
ID=11561951
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP359991U Pending JPH052426U (en) | 1991-02-04 | 1991-02-04 | Helical antenna |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH052426U (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR101715176B1 (en) * | 2016-03-25 | 2017-03-14 | (주)인텔리안테크놀로지스 | Satellite communication antenna apparatus |
WO2022050039A1 (en) * | 2020-09-02 | 2022-03-10 | ソニーグループ株式会社 | Antenna, and electronic device |
-
1991
- 1991-02-04 JP JP359991U patent/JPH052426U/en active Pending
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR101715176B1 (en) * | 2016-03-25 | 2017-03-14 | (주)인텔리안테크놀로지스 | Satellite communication antenna apparatus |
WO2017164454A1 (en) * | 2016-03-25 | 2017-09-28 | (주)인텔리안테크놀로지스 | Antenna apparatus for satellite communication |
WO2022050039A1 (en) * | 2020-09-02 | 2022-03-10 | ソニーグループ株式会社 | Antenna, and electronic device |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CA1322046C (en) | Monopole/l-shaped parasitic elements for circularly/elliptically polarized wave transceiving | |
US5255005A (en) | Dual layer resonant quadrifilar helix antenna | |
US4816836A (en) | Conformal antenna and method | |
US2863145A (en) | Spiral slot antenna | |
Warren et al. | Large, deployable S-band antenna for a 6U CubeSat | |
US20070188397A1 (en) | Broadband polarized antenna including magnetodielectric material, isoimpedance loading, and associated methods | |
EP0612120A1 (en) | Dielectric rod antenna | |
GB814310A (en) | Improvements in or relating to highly active wide-band absorbers for short radio waves | |
US3823404A (en) | Thin sandwich telemetry antenna | |
GB930382A (en) | ||
JPH052426U (en) | Helical antenna | |
US8605001B2 (en) | Radome equipment | |
Yu et al. | Wideband conical-beam circularly polarized microstrip antenna for large ground plane | |
US2478313A (en) | Antenna construction | |
US3852756A (en) | Electrically small resonant antenna with capacitively coupled load | |
AU2016202486B2 (en) | Artificial satellite with integrated antenna | |
US3172112A (en) | Dumbbell-loaded folded slot antenna | |
CN106249206A (en) | For receiving the antenna equipment of electromagnetic wave and for the method running the antenna equipment for receiving electromagnetic wave | |
US7113146B2 (en) | Broadband monopole | |
US6791033B2 (en) | High-voltage insulation system | |
US4443804A (en) | Modified difference mode coaxial antenna with flared aperture | |
US7158088B2 (en) | Magnetic source oscillators universal passive antenna | |
Kumar | A Dual-Band Microstrip Patch Antenna for Wireless Applications | |
Lier et al. | Demonstration of 3D printed hexagonal high gain short backfire antenna with hard EM walls | |
JPH0234483B2 (en) |