KR20000059633A - Aaaaa - Google Patents

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Publication number
KR20000059633A
KR20000059633A KR1019990007383A KR19990007383A KR20000059633A KR 20000059633 A KR20000059633 A KR 20000059633A KR 1019990007383 A KR1019990007383 A KR 1019990007383A KR 19990007383 A KR19990007383 A KR 19990007383A KR 20000059633 A KR20000059633 A KR 20000059633A
Authority
KR
South Korea
Prior art keywords
elevation
angle
satellite antenna
holes
thin film
Prior art date
Application number
KR1019990007383A
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
Application filed by 권태인 filed Critical 권태인
Priority to KR1019990007383A priority Critical patent/KR20000059633A/en
Priority to US09/857,254 priority patent/US6686889B1/en
Priority to IL14306199A priority patent/IL143061A0/en
Priority to AU16920/00A priority patent/AU1692000A/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
Priority to EP99959959A priority patent/EP1151497A4/en
Priority to CA002349425A priority patent/CA2349425A1/en
Priority to DE1999161822 priority patent/DE19961822C2/en
Priority to JP11367141A priority patent/JP2000318639A/en
Publication of KR20000059633A publication Critical patent/KR20000059633A/en

Links

Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q3/00—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
    • H01Q3/02—Arrangements 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
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00—Details of, or arrangements associated with, antennas
    • H01Q1/12—Supports; Mounting means
    • H01Q1/125—Means for positioning

Landscapes

  • Body Structure For Vehicles (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Details Of Aerials (AREA)

Abstract

PURPOSE: An angle meter for measuring an angle of elevation of a satellite antenna is provided to simplify the structure of the angle meter to carry conveniently. CONSTITUTION: In an angle meter for measuring an angle of elevation of a satellite antenna, a portable thin film(1) having a straight side(2) is punched with a plurality of through holes(3) to be respectively inserted with axes formed of wire, fiber and hair having a smaller diameter than the through holes. The through holes are disposed in such a manner that the straight side of the thin film forms different angles of elevation by the gravity, when the axes are sequentially inserted in the through holes. Around the through holes the numbers(4) of the angles of elevation are recorded. The straight side formed with a desired angle of elevation is approached the satellite antenna and the angle of elevation of the straight side is accorded with the angle of elevation of the satellite antenna.

Description

위성안테나 앙각측정용 각도계{AAAAA}Goniometer for satellite antenna elevation measurement {AAAAA}

이 발명은 위성안테나를 설치할 때 사용하는 앙각측정용 각도계에 관한 것이다.The present invention relates to an elevation angle goniometer used when installing a satellite antenna.

위성안테나를 설치하기 위하여 사용하던 종래의 앙각측정용 각도계는 중력에 의하여 수직을 형성하는 지침, 그 지침이 지향하는 수치판으로 구성되어 있어 정확성이 높은 반면 구조가 복잡하고 휴대가 편리하지 못하였다.Conventional elevation measurement goniometer used to install a satellite antenna is composed of a guideline to form a vertical by gravity, a numerical plate to which the guide is directed, high accuracy, but complicated structure and was not convenient to carry.

그러나, 위성안테나의 앙각을 측정하는 각도계는 고도의 정밀성을 요구하지 않는다.However, a goniometer measuring the elevation angle of the satellite antenna does not require high precision.

즉, 위성안테나를 설치할 경우에 앙각과 방위각이 근사치에 이르러 전계강도측정장치가 반응을 나타내기까지의 첫 번째 단계까지는 각도계를 사용하지만, 미세조정을 하는 두 번째 단계에서는 전계강도측정장치에 의존하고 있기 때문이다.In other words, when the satellite antenna is installed, the elevation angle and the azimuth angle are approximated, and the first step until the field strength measuring device responds is used. However, in the second step of fine tuning, the field strength measuring device relies on the field strength measuring device. Because there is.

특히 각도계의 사용빈도가 적은 경우에는 정밀성이 높은 각도계 보다는 구조가 간단하고 휴대가 간편한 간이한 각도계 혹은 1회용으로 사용할 수 있는 각도계가 더욱 필요하였다.Particularly, when the frequency of use of the goniometer is small, a simple goniometer which is simple in structure and easy to carry or a goniometer that can be used for one-time use is needed more than a high precision goniometer.

그래서 일부 위성안테나는 간편성을 기하기 위하여 스텐드와 연동하여 스텐드의 수직이 확보 되었을 때에 사용가능한 구조의 각도계를 부설시키고 있으나, 이 역시 스텐드의 수직을 확보하는 수단이 불편 하였다.Therefore, some satellite antennas are laid with a goniometer of the structure that can be used when the stand is secured in conjunction with the stand for the sake of simplicity, but it is also inconvenient to secure the stand vertical.

그래서 이 발명의 목적은 매우 간편하고 휴대하기 편리한 위성안테나 앙각측정용 각도계를 창조하려는 것이다.The object of this invention is therefore to create a very simple and easy to carry satellite angle goniometer.

본 발명은 휴대가 용이하며 직선의 변(2)을 가진 박막(1)에 별도의 축을 삽입할 수 있는 다수의 천공(3)을 하되, 별도의 축을 각 천공(3)에 순차적으로 삽입하였을 때, 중력에 의하여 박막(1)이 가진 직선의 변(2)이 일정한 간격으로 각기 다른 앙각을 형성하도록 천공(3)의 위치를 배열하고, 각 천공(3) 주위에는 각 천공(3)이 위와같이 형성시키는 앙각의 수치(4)를 기재 한다.The present invention is easy to carry and when a plurality of perforations (3) to insert a separate axis in the thin film (1) having a straight side (2), when a separate axis is sequentially inserted into each perforation (3) , By arranging the positions of the perforations 3 so that the sides of the straight line 2 of the thin film 1 form different elevation angles at regular intervals, and each perforation 3 is above and around each perforation 3. The numerical value (4) of the elevation angle to form together is described.

그리고 이를 실용함에 있어서는, 먼저 박막(1)상 기재된 앙각의 수치(4)중 필요한 각도 혹은 가장 유사한 각도가 표시된 천공(3)을 선택한 다음 여기에 별도의 축을 삽입하되, 그 축은 천공의 직경보다 작은 크기의 철사, 섬유, 두발 등을 이용한다. 그리고 중력을 이용하여 박막의 변(2)에 필요한 앙각을 형성시켜, 그 변(2)을 위성안테나에 접근시킨 후, 안테나의 앙각을 박막(1)의 앙각과 일치시킨다.And in practical use, first select the perforation (3) of the required angle or the most similar angle among the numerical values (4) described on the thin film (1), and then insert a separate axis here, the axis is smaller than the diameter of the perforation Use wires, fibers and hairs of the same size. Then, by using gravity, an elevation angle necessary for the side 2 of the thin film is formed, and the side 2 is approached to the satellite antenna, and then the elevation angle of the antenna coincides with the elevation angle of the thin film 1.

이와 같이 본 발명을 실용하게 되면,Thus, if the present invention is practical,

본 발명이 가지는 탁월한 간편성 때문에 널리 보급 사용될 것이기 때문에, 가전제품화 되고 있는 소형위성안테나를 일반인이 직접 설치하는데 크게 공헌하게 될 것이다.Since the present invention will be widely used due to the excellent simplicity of the present invention, it will greatly contribute to the general public to install a small satellite antenna which is becoming a home appliance.

발명이 이루고자 하는 기술적 과제 누락Missing technical challenges for invention

제1도는 본 발명 위성안테나 앙각측정용 각도계로서, 휴대하기 용이하며 직선의 변(2)을 가진 박막(1)에, 별도의 축을 삽입할 수 있는 다수의 천공(3)을 하며, 각 천공(3) 주위에는 축을 삽입하였을 때 형성되는 앙각의 수치(4)를 기재한다.1 is a satellite angle measuring angle measuring device of the present invention, which is easy to carry and has a plurality of perforations 3 into which a separate axis can be inserted into a thin film 1 having a straight side 2, each perforation ( 3) The value (4) of the elevation angle formed when the shaft is inserted is described.

발명의 구성 및 작용 누락Missing configuration and action of the invention

발명의 효과 누락Missing Effect of Invention

Claims (1)

휴대하기 용이하며 직선의 변을 가진 박막에 별도의 축을 삽입할 수 있는 다수의 천공을 하되, 별도의 축을 각 천공에 순차적으로 삽입하였을 때, 중력에 의하여 박막이 가진 직선의 변이 일정한 간격으로 각기 다른 앙각을 형성하도록 천공의 위치를 배열하고, 각 천공 주위에는 각 천공이 위와같이 형성시키는 앙각의 수치를 기재한 것을 특징으로 한 위성안테나 앙각측정용 각도계.It is easy to carry and has a plurality of perforations to insert a separate axis in the thin film having a straight side, when the separate axes are inserted in each perforation sequentially, the sides of the straight line of the thin film due to gravity are different at regular intervals A satellite antenna elevation measurement goniometer, wherein the positions of the perforations are arranged to form the elevation angles, and the perimeter values of each perforation are described around each perforation.
KR1019990007383A 1998-12-08 1999-05-03 Aaaaa KR20000059633A (en)

Priority Applications (12)

Application Number Priority Date Filing Date Title
KR1019990007383A KR20000059633A (en) 1999-05-03 1999-05-03 Aaaaa
US09/857,254 US6686889B1 (en) 1998-12-08 1999-06-12 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
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
EP99959959A EP1151497A4 (en) 1998-12-08 1999-12-06 Method and apparatus for antenna orientation and antenna with the same
CA002349425A CA2349425A1 (en) 1998-12-08 1999-12-06 Method and apparatus for antenna orientation and antenna with the same
DE1999161822 DE19961822C2 (en) 1999-05-03 1999-12-21 Motor vehicle frame with a reinforcement structure
JP11367141A JP2000318639A (en) 1999-05-03 1999-12-24 Reinforcing structure of motor vehicle body

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
KR1019990007383A KR20000059633A (en) 1999-05-03 1999-05-03 Aaaaa

Publications (1)

Publication Number Publication Date
KR20000059633A true KR20000059633A (en) 2000-10-05

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ID=19575713

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1019990007383A KR20000059633A (en) 1998-12-08 1999-05-03 Aaaaa

Country Status (3)

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JP (1) JP2000318639A (en)
KR (1) KR20000059633A (en)
DE (1) DE19961822C2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4010817B2 (en) * 2002-01-30 2007-11-21 本田技研工業株式会社 Vehicle body frame structure
CN106533352B (en) * 2016-09-08 2018-05-01 上海卫星工程研究所 Satellite vapour image shade and application method

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS58128970A (en) * 1982-01-27 1983-08-01 Mazda Motor Corp Construction of car body
JP3137881B2 (en) * 1995-09-01 2001-02-26 本田技研工業株式会社 Car body structure
DE19622675C2 (en) * 1996-06-05 2001-03-22 Daimler Chrysler Ag Sidewall assembly with an outer, half-shell profiled sidewall part

Also Published As

Publication number Publication date
JP2000318639A (en) 2000-11-21
DE19961822A1 (en) 2000-11-16
DE19961822C2 (en) 2002-08-14

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