KR20010003534A - Aaaaa - Google Patents

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Publication number
KR20010003534A
KR20010003534A KR1019990023860A KR19990023860A KR20010003534A KR 20010003534 A KR20010003534 A KR 20010003534A KR 1019990023860 A KR1019990023860 A KR 1019990023860A KR 19990023860 A KR19990023860 A KR 19990023860A KR 20010003534 A KR20010003534 A KR 20010003534A
Authority
KR
South Korea
Prior art keywords
satellite antenna
shadow
antenna
generating device
satellite
Prior art date
Application number
KR1019990023860A
Other languages
Korean (ko)
Inventor
권태인
Original Assignee
권태인
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
Priority to US09/857,254 priority Critical patent/US6686889B1/en
Application filed by 권태인 filed Critical 권태인
Priority to KR1019990023860A priority patent/KR20010003534A/en
Priority to CA002349425A priority patent/CA2349425A1/en
Priority to IL14306199A priority patent/IL143061A0/en
Priority to AU16920/00A priority patent/AU1692000A/en
Priority to EP99959959A priority patent/EP1151497A4/en
Priority to JP2000587407A priority patent/JP2003522434A/en
Priority to KR1020017006846A priority patent/KR20010101111A/en
Priority to CN 99814177 priority patent/CN1329764A/en
Priority to PCT/KR1999/000741 priority patent/WO2000035049A1/en
Publication of KR20010003534A publication Critical patent/KR20010003534A/en

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q3/00Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
    • H01Q3/02Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole
    • H01Q3/08Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying two co-ordinates of the orientation
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q19/00Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic
    • H01Q19/10Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces
    • H01Q19/12Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces wherein the surfaces are concave
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/12Supports; Mounting means
    • H01Q1/1207Supports; Mounting means for fastening a rigid aerial element
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/12Supports; Mounting means
    • H01Q1/125Means for positioning
    • H01Q1/1257Means for positioning using the received signal strength

Abstract

PURPOSE: A satellite antenna installed using a shadow of the sun is provided to facilitate the conveyance and usage of the satellite antenna by simplifying the structure of the satellite antenna. CONSTITUTION: A satellite antenna(1) comprises a shadow creating device(4) which is installed from a rear portion(2) of the satellite antenna(1) to a front portion(3) of the satellite antenna(1). The shadow creating device(4) is fixed to the rear portion(2) of the satellite antenna(1) and is tapered in the direction of the front portion(3) of the satellite antenna(1). A bead(5) and a sight(6) are formed at an upper portion of the shadow creating device(4). The bead(5) and the sight(6) are oriented in the same direction with an angle of elevation and an azimuth of the satellite antenna(1). A perforation hole(7) is formed between the sight(6) and the rear portion(2) of the satellite antenna(1).

Description

태양의 그림자를 이용하여 설치하는 위성안테나{AAAAA}Satellite antenna installed using the sun's shadow {AAAAA}

[발명의 분야][Field of Invention]

본 발명은 위성안테나에 관한 것이다.The present invention relates to a satellite antenna.

더욱 구체적으로는 태양의 그림자에 의하여 설치하는 위성안테나에 관한 것이다.More specifically, it relates to a satellite antenna installed by the shadow of the sun.

[발명의 배경][Background of invention]

위성안테나를 설치할 때에는 각도조절이 대단히 복잡하였다.The angle adjustment was very complicated when installing the satellite antenna.

그래서 발명자는 태양의 그림자에 의하여 설치하는 안테나를 발명하여 특허출원 하였고, 그 후에도 이를 계량하여 특허출원하고 있는 중이다.Therefore, the inventor invented the patent by inventing the antenna installed by the shadow of the sun, and after that, it is still applying for the patent.

종전에 발명자가 출원한 것들은,Previously filed by the inventor,

주로 위성안테나의 휘드혼 상부(10)로부터 위성안테나 상부 중앙(11)을 직선으로 연결하는 그림자생성장치를 설치하고, 그 그림자에 의하여 안테나의 각도를 조절하는 방식이었다.Mainly, the shadow generating device was installed to connect the center of the upper part of the satellite antenna from the upper part of the top horn 10 of the satellite antenna and the angle of the antenna was adjusted by the shadow.

이 방식은 전세계 모든 지역에서 사용할 수 있는 방식이기는 하지만, 안테나 앙각이 비교적 낮은 지역에서는 다소 불편하였다.Although this method can be used in all regions of the world, it is somewhat inconvenient in areas where the antenna elevation is relatively low.

다시 말하자면, 앙각이 약 30도 미만인 지역에서 옵셋형 안테나를 사용할 때에는, 그 안테나가 거의 수직에 가까운 각도를 이루기 때문에 그림자생성장치를 그렇게 길게 늘어뜨리지 않아도 된다.In other words, when using an offset antenna in an area where the elevation angle is less than about 30 degrees, the shadow generator does not have to be stretched so long as the antenna is almost perpendicular.

그 이유는 안테나가 수직에 가깝게 바로 서게되면 안테나 상부에서 전방을 향하여 물체를 작게 돌출 시켜도 그림자는 안테나 하부까지 길게 드리워지기 때문이다.The reason is that if the antenna is standing upright close to the vertical, the shadow will be extended to the lower part of the antenna even if the object is protruded small from the top of the antenna toward the front.

따라서 낮은 앙각을 사용하는 지역을 위하여서는 좀더 간단한 그림자생성장치가 필요하였다.Therefore, a simpler shadow-generating device was needed for low elevation areas.

또한 종전 발명은 그림자생성장치와 장애물확인장치가 따로 분리되어 있어서 제조가 다소 불편하였다.In addition, the prior invention was somewhat uncomfortable manufacturing because the shadow generating device and the obstacle identification device is separated separately.

그래서 발명자는 위에서 추가적으로 언급된 문제조차도 해결된 위성안테나를 제공하려 한다.The inventors therefore seek to provide a satellite antenna that solves even the problems mentioned above.

본 발명의 목적은,The object of the present invention,

태양의 그림자에 의하여 설치하는 옵셋형 위성안테나를, 앙각이 낮은 지역에서 사용할 때 적합한 그림자생성장치를 제공하려는 것이다.The purpose is to provide a shadow generating device suitable for use in an area with low elevation angles using offset satellite antennas installed by the sun's shadow.

본 발명의 다른 목적은, 위성안테나 전방의 장애물을 확인하는 장애물확인장치를 그림자생성장치와 통합시켜 더욱 단순화된, 태양의 그림자에 의하여 설치하는 위성안테나를 제공하려는 것이다.Another object of the present invention is to provide a satellite antenna installed by the shadow of the sun, which is further simplified by integrating an obstacle checking device for identifying an obstacle in front of the satellite antenna with a shadow generating device.

위와 같은 목적들은 모두 다음에 설명되는 본 발명에 의하여 달성될 수 있다.All of the above objects can be achieved by the present invention described below.

제1도는 본 발명 위성안테나의 측면도이다.1 is a side view of the satellite antenna of the present invention.

[도면의 주요 부호에 대한 간단한 설명]BRIEF DESCRIPTION OF THE MAIN SIGNS IN THE FIGURE

(1)위성안테나 (2)위성안테나 후방 (3)위성안테나 전방 (4)그림자생성장치(1) satellite antennas (2) rear satellites (3) front satellites (4) shadow generators

(5)가늠쇠 (6)가늠자 (7)천공 (8)그림자생성장치 지지대 (9)브라켓(5) Scales (6) Scales (7) Perforation (8) Shadow Supporters (9) Bracket

본 발명의 태양의 그림자에 의하여 설치하는 위성안테나는,Satellite antenna installed by the shadow of the sun of the present invention,

위성안테나(1) 후방(2)으로부터 전방(3)을 향하여 위성안테나(1)를 관통하여 돌출하는 그림자생성장치(4)를 설치하되,Install a shadow generating device (4) protruding through the satellite antenna (1) toward the front (3) from the rear (2) of the satellite antenna (1),

그림자생성장치(4)는 안테나 후방(2)에서 고정되고, 돌출을 시작하는 부위로부터 점차 굵기가 작아져 끝 부분이 뾰쪽한 모양으로 구성되며,The shadow generating device 4 is fixed at the rear of the antenna (2), the thickness is gradually reduced from the starting portion of the protrusion is composed of a pointed shape,

그림자생성장치(4)의 상부에는,On top of the shadow generating device 4,

안테나가 지향하는 방위각 및 앙각과 같은 방향의 전방을 지향하는 가늠쇠(5)와 가늠자(6)로, 가늠쇠(5)와 안테나 후방(2) 사이에는 천공(7)으로 각 구성된 장애물확인장치(5,6,7)가 설치된 것을 특징으로 한다.Obstacle checking device each composed of a scale (5) and scale (6) to the front in the same direction, such as the azimuth and elevation angle directed by the antenna, and a perforation (7) between the scale (5) and the rear of the antenna (5) , 6,7) is installed.

이하 첨부된 도면에 의하여 본 발명의 내용을 상세히 설명한다.Hereinafter, the contents of the present invention will be described in detail with reference to the accompanying drawings.

제1도는 본 발명을 개략적으로 도시한 측면도로서,1 is a side view schematically showing the present invention,

위성안테나(1) 후방(2)에 있는 브라켓(9)을 위로 연장하여 그림자생성장치(4)를 지지할 수 있는 지지대(8)를 만들고, 이 지지대(8)는 안테나(1)을 관통하여 전방(3)으로 돌출하는 그림자생성장치(4)를 지지한다.Extending the bracket (9) at the rear (2) of the satellite antenna (1) upwards to create a support (8) capable of supporting the shadow generating device (4), which is passed through the antenna (1) Supports the shadow generating device (4) protruding forward (3).

그림자생성장치(4)는 돌출을 시작하는 부위로부터 점차 굵기가 작아져 끝 부분이 뾰쪽한 모양으로 구성되어, 그 끝 부분이 안테나(1) 전면에 설치되는 각도표 위에 태양의 그림자를 생성시키게 한다.The shadow generating device 4 gradually becomes smaller in thickness from the starting point of the protruding portion so that the end portion has a pointed shape, so that the end portion generates the shadow of the sun on the angle table installed in front of the antenna 1. .

그림자생성장치(4)의 상부에는 장애물확인장치(5,6,7)를 설치하되,Obstacle check devices (5, 6, 7) is installed on the upper portion of the shadow generating device (4),

안테나가 지향하는 방위각 및 앙각과 같은 방향의 전방을 지향하는 가늠쇠(5)와 가늠자(6)를 돌출시키고, 가늠쇠(5)와 안테나 후방(2) 사이에는 천공(7)을 하여 위성안테나를 설치할 때 그 공(7)과 가늠쇠(5) 가늠자(6)을 순차로 통하여 전방을 주시할 수 있게 한다.Protrudes the scale (5) and the scale (6) to the front in the same direction, such as the azimuth and elevation angle, and the perforation (7) between the bracket (5) and the rear of the antenna (2) to install a satellite antenna When the ball (7) and the scale (5) scale (6) in order to be able to look forward.

이와 같이 구성된 태양의 그림자에 의하여 설치하는 위성안테나는 다음과 같이 실용된다.The satellite antenna installed by the shadow of the sun thus constructed is practically used as follows.

계절과 날자, 시각, 지구상좌표, 위성의 위치에 따라 태양의 그림자가 도달하여야 할 위치를 확정한 다음, 그 위치에 그림자생성장치(4) 끝의 뾰쪽한 부분의 그림자를 도달시키는 방법으로 각도를 조절하여 설치한다.Determine the location where the sun's shadow should reach according to the season, date, time, earth coordinates, and the position of the satellite, and then adjust the angle by reaching the shadow of the pointed part of the end of the shadow generator (4). Adjust and install.

그리고, 공(7)과 가늠쇠(5), 가늠자(6)을 순차로 통하여 전방을 주시하여 장애물이 안테나를 가로막고 있는지 확인하고 조치하게 된다.Then, the front of the ball (7), the scale (5), the scale (6) by looking at the front to check whether the obstacle is blocking the antenna and take action.

따라서 본 발명은,Therefore, the present invention,

태양의 그림자를 이용하여 위성안테나를 더욱 단순화시켜 제조와 운송, 사용이 편리하게 되었다.The shadow of the sun further simplifies the satellite antenna, making it easier to manufacture, transport and use.

특히 그림자생성장치와 장애물확인장치를 통합하여 위성안테나를 단순화시킨 것이다.In particular, the satellite antenna is simplified by integrating the shadow generation device and the obstacle identification device.

본 발명은 단순한 변형이나 변경은 이 분야의 통상의 지식을 가진 자에 의하여 용이하게 실시될 수 있다.Simple modifications and variations of the present invention can be readily made by one of ordinary skill in the art.

이러한 변형이나 변경은 모두 본 발명의 영역에 속하는 것이다.Such modifications and variations are all within the scope of the present invention.

Claims (1)

위성안테나(1) 후방(2)으로부터 전방(3)을 향하여 위성안테나(1)를 관통하여 돌출하는 그림자생성장치(4)를 설치하되,Install a shadow generating device (4) protruding through the satellite antenna (1) toward the front (3) from the rear (2) of the satellite antenna (1), 그림자생성장치(4)는 안테나 후방(2)에서 고정되고, 돌출을 시작하는 부위로부터 점차 굵기가 작아져 끝 부분이 뾰쪽한 모양으로 구성되며,The shadow generating device 4 is fixed at the rear of the antenna (2), the thickness is gradually reduced from the starting portion of the protrusion is composed of a pointed shape, 그림자생성장치(4)의 상부에는,On top of the shadow generating device 4, 안테나가 지향하는 방위각 및 앙각과 같은 방향의 전방을 지향하는 가늠쇠(5)와 가늠자(6)로, 가늠쇠(5)와 안테나 후방(2) 사이에는 천공(7)으로 각 구성된 장애물확인장치(5,6,7)가 설치된 것을 특징으로 하는 위성안테나(1).Obstacle checking device each composed of a scale (5) and the scale (6) to the front in the same direction, such as the azimuth and elevation angle that the antenna is directed, and a perforation (7) between the scale (5) and the rear of the antenna (5) Satellite antenna (1), characterized in that installed, 6,7.
KR1019990023860A 1998-12-08 1999-06-23 Aaaaa KR20010003534A (en)

Priority Applications (10)

Application Number Priority Date Filing Date Title
US09/857,254 US6686889B1 (en) 1998-12-08 1999-06-12 Method and apparatus for antenna orientation and antenna with the same
KR1019990023860A KR20010003534A (en) 1999-06-23 1999-06-23 Aaaaa
CA002349425A CA2349425A1 (en) 1998-12-08 1999-12-06 Method and apparatus for antenna orientation and antenna with the same
IL14306199A IL143061A0 (en) 1998-12-08 1999-12-06 Method and apparatus for antenna orientation and antenna with the same
AU16920/00A AU1692000A (en) 1998-12-08 1999-12-06 Method and apparatus for antenna orientation and antenna with the same
EP99959959A EP1151497A4 (en) 1998-12-08 1999-12-06 Method and apparatus for antenna orientation and antenna with the same
JP2000587407A JP2003522434A (en) 1998-12-08 1999-12-06 Apparatus and method for directing antenna to transmitter, and antenna using the same
KR1020017006846A KR20010101111A (en) 1998-12-08 1999-12-06 Method and apparatus for antenna orientation and antenna with the same
CN 99814177 CN1329764A (en) 1998-12-08 1999-12-06 Method and device for antenna direction, and antenna thereof
PCT/KR1999/000741 WO2000035049A1 (en) 1998-12-08 1999-12-06 Method and apparatus for antenna orientation and antenna with the same

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
KR1019990023860A KR20010003534A (en) 1999-06-23 1999-06-23 Aaaaa

Publications (1)

Publication Number Publication Date
KR20010003534A true KR20010003534A (en) 2001-01-15

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Application Number Title Priority Date Filing Date
KR1019990023860A KR20010003534A (en) 1998-12-08 1999-06-23 Aaaaa

Country Status (1)

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KR (1) KR20010003534A (en)

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