JP2011180125A5 - - Google Patents

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JP2011180125A5
JP2011180125A5 JP2011002709A JP2011002709A JP2011180125A5 JP 2011180125 A5 JP2011180125 A5 JP 2011180125A5 JP 2011002709 A JP2011002709 A JP 2011002709A JP 2011002709 A JP2011002709 A JP 2011002709A JP 2011180125 A5 JP2011180125 A5 JP 2011180125A5
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Japan
Prior art keywords
positioning ring
box
positioning
column
opening
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Pending
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JP2011002709A
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Japanese (ja)
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JP2011180125A (en
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Priority claimed from TW99105946A external-priority patent/TW201131525A/en
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Publication of JP2011180125A publication Critical patent/JP2011180125A/en
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上縁に開口部が設けられる箱体と、
仰角目盛りが設けられた透明の半球カバーであり、底部辺縁が前記箱体上縁の開口部周縁を被覆する天幕カバーと、
中空であり、直径が前記箱体の開口部より若干小さく、両側に前記箱体と接続される枢着軸がそれぞれ設けられる第１の位置決めリングと、
扇形の中空であり、直径が前記第１の位置決めリングより若干小さく、前記第１の位置決めリングの枢着軸と垂直の両側には、前記第１の位置決めリングと接続される枢着軸がそれぞれ設けられ、周縁に凹溝が設けられ、中心に中心軸が設けられる第２の位置決めリングと、
一方の端部に中空柱体が設けられ、他方の端部に中実柱体が設けられ、前記中空柱体は、上縁に貫通孔が設けられ、下縁に基準中心が設けられ、前記中実柱体は、前記第２の位置決めリングの中心軸に枢着される位置決め柱と、を備え、
前記箱体の開口部には、前記第１の位置決めリングが収納され、前記第１の位置決めリングの中空部分には、前記第２の位置決めリングが収納され、前記第２の位置決めリングの扇形の中空部分には、前記位置決め柱が収納されることを特徴とする多軸式太陽軌跡追跡経緯儀。 A box with an opening at the upper edge;
A transparent hemispherical cover provided with an elevation graduation, and a awning cover whose bottom edge covers the periphery of the opening of the upper edge of the box;
A first positioning ring that is hollow, has a diameter slightly smaller than the opening of the box, and is provided with pivoting shafts connected to the box on both sides;
A fan-shaped hollow having a diameter slightly smaller than that of the first positioning ring, and a pivot shaft connected to the first positioning ring on each side perpendicular to the pivot shaft of the first positioning ring. A second positioning ring provided with a groove on the periphery and a central axis at the center;
A hollow column is provided at one end, a solid column is provided at the other end, the hollow column is provided with a through hole at the upper edge, a reference center is provided at the lower edge, The solid column body includes a positioning column pivotally attached to the central axis of the second positioning ring,
The first positioning ring is accommodated in the opening of the box, and the second positioning ring is accommodated in the hollow portion of the first positioning ring. A multi-axis solar trajectory tracking theodolite characterized in that the positioning column is accommodated in the hollow portion. 上縁に開口部が設けられる箱体と、
仰角目盛りが設けられた透明の半球カバーであり、底部辺縁が前記箱体上縁の開口部周縁を被覆する天幕カバーと、
中空であり、直径が前記箱体の開口部より若干小さく、両側に前記箱体と接続される枢着軸がそれぞれ設けられる第１の位置決めリングと、
中実であり、直径が前記第１の位置決めリングより若干小さく、前記第１の位置決めリングの枢着軸と垂直の両側には、前記第１の位置決めリングと接続される枢着軸がそれぞれ設けられ、周縁に貫通孔が設けられ、前記貫通孔は、基準中心が設けられた中心まで延伸する第２の位置決めリングと、を備え、
前記箱体の開口部には、前記第１の位置決めリングが収納され、前記第１の位置決めリングの中空部分には、前記第２の位置決めリングが収納されることを特徴とする多軸式太陽軌跡追跡経緯儀。 A box with an opening at the upper edge;
A transparent hemispherical cover provided with an elevation graduation, and a awning cover whose bottom edge covers the periphery of the opening of the upper edge of the box;
A first positioning ring that is hollow, has a diameter slightly smaller than the opening of the box, and is provided with pivoting shafts connected to the box on both sides;
It is solid and has a diameter slightly smaller than that of the first positioning ring, and a pivot shaft connected to the first positioning ring is provided on both sides perpendicular to the pivot shaft of the first positioning ring. A through hole is provided at the periphery, and the through hole includes a second positioning ring extending to the center at which the reference center is provided,
The multi-axis sun, wherein the first positioning ring is accommodated in the opening of the box, and the second positioning ring is accommodated in a hollow portion of the first positioning ring. Trajectory tracking theodolite. 上縁に開口部が設けられる箱体と、
仰角目盛りが設けられた透明の半球カバーであり、底部辺縁が前記箱体上縁の開口部周縁を被覆する天幕カバーと、
中空であり、直径が前記箱体の開口部より若干小さく、両側に前記箱体と接続される枢着軸がそれぞれ設けられる第１の位置決めリングと、
扇形の中空であり、直径が前記第１の位置決めリングより若干小さく、前記第１の位置決めリングの枢着軸と垂直の両側には、前記第１の位置決めリングと接続される枢着軸がそれぞれ設けられ、周縁に凹溝が設けられ、中心に中心軸が設けられる第２の位置決めリングと、
一方の端部に中空柱体が設けられ、他方の端部に中実柱体が設けられ、前記中空柱体内には、磁石が収納され、前記中実柱体は、前記第２の位置決めリングの中心軸に枢着される位置決め柱と、
内部に磁石が配置され、単独構造であり、前記天幕カバーの外表面に配置される位置決め部材と、を備え、
前記箱体の開口部には、前記第１の位置決めリングが収納され、前記第１の位置決めリングの中空部分には、前記第２の位置決めリングが収納され、前記第２の位置決めリングの扇形の中空部分には、前記位置決め柱が収納され、前記位置決め部材の底部は、前記天幕カバーの外表面上に配置され、
前記位置決め部材を前記天幕カバーの表面上において移動させたとき、前記位置決め柱は、前記位置決め柱の磁石が前記位置決め部材の磁石に吸着されることによって連動し、これにより、前記第１の位置決めリング及び前記第２の位置決めリングが移動することを特徴とする多軸式太陽軌跡追跡経緯儀。 A box with an opening at the upper edge;
A transparent hemispherical cover provided with an elevation graduation, and a awning cover whose bottom edge covers the periphery of the opening of the upper edge of the box;
A first positioning ring that is hollow, has a diameter slightly smaller than the opening of the box, and is provided with pivoting shafts connected to the box on both sides;
A fan-shaped hollow having a diameter slightly smaller than that of the first positioning ring, and a pivot shaft connected to the first positioning ring on each side perpendicular to the pivot shaft of the first positioning ring. A second positioning ring provided with a groove on the periphery and a central axis at the center;
A hollow column is provided at one end, a solid column is provided at the other end, a magnet is accommodated in the hollow column, and the solid column includes the second positioning ring. A positioning column pivotally attached to the central axis of
A magnet is disposed inside, has a single structure, and a positioning member disposed on the outer surface of the awning cover,
The first positioning ring is accommodated in the opening of the box, and the second positioning ring is accommodated in the hollow portion of the first positioning ring. In the hollow portion, the positioning column is housed, and the bottom of the positioning member is disposed on the outer surface of the awning cover,
When the positioning member is moved on the surface of the awning cover, the positioning column is interlocked by the magnet of the positioning column being attracted to the magnet of the positioning member, whereby the first positioning ring And a multi-axis solar trajectory tracking theodolite, wherein the second positioning ring moves. 前記箱体の開口部周縁には、前記天幕カバーが収容される環状溝が設けられ、前記箱体の前記天幕カバーが接続される内外周囲には、方位角目盛りが設けられ、 前記箱体外部の前記第１の位置決めリングの枢着軸が接続される両側には、緯度目盛りが設けられることを特徴とする請求項１、２又は３に記載の多軸式太陽軌跡追跡経緯儀。 The opening portion of the box body, the annular groove tent cover is accommodated is provided on the inner and outer periphery of the awning cover of the box body are coupled, the azimuth angle graduations provided et al is, the box body 4. The multi-axis solar trajectory tracking theodolite according to claim 1, 2 or 3 , wherein latitude scales are provided on both sides to which the pivoting shaft of the external first positioning ring is connected . 前記第１の位置決めリングの枢着軸には、観測点の緯度に基づいて角度を調整するために用いられる調整指針が設けられることを特徴とする請求項１、２又は３に記載の多軸式太陽軌跡追跡経緯儀。   4. The multi-axis according to claim 1, wherein the pivot shaft of the first positioning ring is provided with an adjustment pointer used for adjusting an angle based on a latitude of an observation point. Ceremony for tracking the sun trajectory. 前記第１の位置決めリングの外径周縁の前記第２の位置決めリングの枢着軸が接続される両側には、時刻目盛りが設けられることを特徴とする請求項１、２又は３に記載の多軸式太陽軌跡追跡経緯儀。 The time scale is provided on both sides of the outer peripheral edge of the first positioning ring to which the pivot shaft of the second positioning ring is connected. Axis solar trajectory tracking theodolite. 前記第２の位置決めリングの枢着軸には、観測時刻を設定するために用いられる調整指針が設けられることを特徴とする請求項１、２又は３に記載の多軸式太陽軌跡追跡経緯儀。 4. The multi-axis solar trajectory tracking theodolite according to claim 1, wherein an adjustment indicator used for setting an observation time is provided on a pivot axis of the second positioning ring. 5. . 前記第２の位置決めリングの凹溝周囲には、前記位置決め柱が観測月を設定するために用いられる月目盛りが設けられることを特徴とする請求項１又は３に記載の多軸式太陽軌跡追跡経緯儀。   4. The multi-axis solar trajectory tracking according to claim 1, wherein a moon scale used by the positioning column to set an observation month is provided around the groove of the second positioning ring. 5. Theodolite. 前記貫通孔内又は基準中心面上には、レーザーペンが装着されることを特徴とする請求項１又は２に記載の多軸式太陽軌跡追跡経緯儀。   The multi-axis solar trajectory tracking theodolite according to claim 1 or 2, wherein a laser pen is mounted in the through hole or on the reference center plane. 前記中空柱体には、嵌合管が設けられ、前記嵌合管の前端には、磁石が配置されることを特徴とする請求項３に記載の多軸式太陽軌跡追跡経緯儀。 The multi-axis solar trajectory tracking theodolite according to claim 3, wherein the hollow column body is provided with a fitting tube, and a magnet is disposed at a front end of the fitting tube.
JP2011002709A 2010-03-02 2011-01-11 Quasi-uniaxial solar trajectory tracking transit system Pending JP2011180125A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
TW099105946 2010-03-02
TW99105946A TW201131525A (en) 2010-03-02 2010-03-02 Quasi-uniaxial solar trajectory tracking theodolite

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JP2011180125A JP2011180125A (en) 2011-09-15
JP2011180125A5 true JP2011180125A5 (en) 2011-11-04

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KR101512657B1 (en) 2013-08-12 2015-04-17 류희욱 survey apparatus of the ecliptic for institution of solar panel
TWI506603B (en) * 2014-08-01 2015-11-01 Nat Taipei University Of Education Three - dimensional stereoscopic motion of the moon
CN106952564B (en) * 2017-03-29 2024-04-16 安徽宜飞思工业设计有限公司 Sun vision movement locus instrument
KR102638085B1 (en) * 2021-08-20 2024-02-21 소서현 An Hemispherical sundial nephometer

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US4136397A (en) * 1977-10-03 1979-01-23 Pierce Darrel J Astronomical timepiece
JPH0419780A (en) * 1990-05-07 1992-01-23 Fu-Wang Chien Quadrant
JPH04155210A (en) * 1990-10-18 1992-05-28 N K B:Kk Observing apparatus for position of sun
US5344325A (en) * 1993-05-17 1994-09-06 Wang Zn Hu Automatic tracking astronomical globe
US6343938B1 (en) * 2000-08-30 2002-02-05 David R. Moreland Moon phase demonstration system
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