CN102434763A - Composite shaft structure of detector - Google Patents

Composite shaft structure of detector Download PDF

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Publication number
CN102434763A
CN102434763A CN2011102967078A CN201110296707A CN102434763A CN 102434763 A CN102434763 A CN 102434763A CN 2011102967078 A CN2011102967078 A CN 2011102967078A CN 201110296707 A CN201110296707 A CN 201110296707A CN 102434763 A CN102434763 A CN 102434763A
Authority
CN
China
Prior art keywords
pitching
azimuth
motor
housing
inside casing
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
CN2011102967078A
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Chinese (zh)
Inventor
张冰
王端
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.)
Sichuan Jiuzhou Electric Group Co Ltd
Original Assignee
Sichuan Jiuzhou Electric Group Co Ltd
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 Sichuan Jiuzhou Electric Group Co Ltd filed Critical Sichuan Jiuzhou Electric Group Co Ltd
Priority to CN2011102967078A priority Critical patent/CN102434763A/en
Publication of CN102434763A publication Critical patent/CN102434763A/en
Pending legal-status Critical Current

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Abstract

The invention discloses a composite shaft structure of a detector, which comprises a base, an outer frame, an inner frame, an azimuth motor, a pitching motor, an azimuth photoelectric coded disc and a pitching photoelectric coded disc; the outer frame and the inner frame are both in annular shapes; the outer frame is sleeved on the external of the inner frame; the azimuth motor and the azimuth photoelectric coded disc are fixed on the base; the azimuth motor is connected with the outer frame by a transmission shaft and a cylindrical gear mechanism for driving the outer frame to rotate along the direction of the azimuth; the pitching motor and the pitching photoelectric coded disc are installed on the outer frame; and the pitching motor is connected with the inner frame for driving the inner frame to rotate along the pitching direction. The composite shaft structure of the detector has the advantages of simple structure, easy manufacture, low cost, light weight, small size, high stabilizing precision and capabilities of accurately controlling the position angle and the pitching angle of the detector and conveniently and effectively observing the position of the observed articles.

Description

Prober composite shaft mechanism
Technical field
The present invention relates to a kind of rotating mechanism, particularly relate to a kind of prober composite shaft mechanism.
Background technique
In the engineering practical application, use prober observation measured article, usually run into and need the measured article on the moving platform be rotated a certain angle in the present position, thereby make an experiment test in each orientation.The test of this test needs a plurality of engineering staffs' cooperation usually, realizes the test data of different amount with the method for dial, commands all the other operator's adjustment while observe position of detector.Be not easy to observe but need confirm measured article whether in the situation of desired location if run into, then operator's observation difficulty will increase, and accuracy of observation might reduce.How to address the above problem the direction that becomes those skilled in the art's thinking and make great efforts.
Summary of the invention
The object of the invention is exactly the deficiency to above-mentioned existing technology, and a kind of prober composite shaft mechanism is provided, and can accurately control the azimythal angle and the pitching angle of prober.
The object of the invention is realized through following technical proposals:
A kind of prober composite shaft mechanism comprises base, housing, inside casing, azimuth-drive motor, pitching motor, orientation photoelectric code disk, pitching photoelectric code disk; Said housing and inside casing are ring, and housing is placed in outside the inside casing; Azimuth-drive motor and orientation photoelectric code disk are fixed on the base, and azimuth-drive motor is connected with housing with cylindrical gear mechanism through transmission shaft, drive housing and do the azimuth direction rotation; Pitching motor and pitching photoelectric code disk are installed on the housing, and pitching motor is connected with inside casing, drive inside casing and do the pitch orientation rotation.
Further, said housing can be done the rotation of azimuth direction ± 45 °.
Further, said inside casing can be done the rotation of pitch orientation ± 45 °.
Further, the velocity ratio of said cylindrical gear mechanism is 1:1.
Beneficial effect of the present invention is: simple in structure, easy processing, with low cost, in light weight, volume is little, lasting accuracy is high, can accurately control the azimythal angle and the pitching angle of prober, observing by the residing position of observation thing easily and effectively.
Description of drawings
Fig. 1 is a structural representation of the present invention;
Fig. 2 is a side view of the present invention.
Embodiment
Below in conjunction with specific embodiment and accompanying drawing the present invention is further described.
As depicted in figs. 1 and 2, a kind of prober composite shaft mechanism comprises base 1, housing 2, inside casing 3, azimuth-drive motor 4, pitching motor 6, orientation photoelectric code disk 5, pitching photoelectric code disk 7; Said housing 2 is a ring with inside casing 3, and housing 2 is placed in outside the inside casing 3; Azimuth-drive motor 4 is fixed on the base 1 with orientation photoelectric code disk 5, and azimuth-drive motor 4 is connected with housing 2 with cylindrical gear mechanism 8 through transmission shaft, drives housing 2 and does the azimuth direction rotation; Pitching motor 6 is installed on the housing 2 with pitching photoelectric code disk 7, and pitching motor 6 is connected with inside casing 3, drives inside casing 3 and does the pitch orientation rotation.
Said housing 2 can be done the rotation of azimuth direction ± 45 °, and inside casing 3 can be done the rotation of pitch orientation ± 45 °.The velocity ratio of said cylindrical gear mechanism 8 is 1:1.
In use, radar antenna and Infrared detector are rigidly connected through flange plate and are one, and are fixed on the inside casing 3.Housing 2 and inside casing 3 are through the rotation of closed loop servo system control azimuth motor 4, pitching motor 6 and orientation photoelectric code disk 5, pitching photoelectric code disk 7 completion azimythal angles and pitching angle ± 45 °, and accurate control target travelling speed.
The above is merely preferred embodiment of the present invention, not in order to restriction the present invention, all any modifications of within spirit of the present invention and principle, being done, is equal to and replaces and improvement etc., all should be included within protection scope of the present invention.

Claims (4)

1. a prober composite shaft mechanism is characterized in that: comprise base, housing, inside casing, azimuth-drive motor, pitching motor, orientation photoelectric code disk, pitching photoelectric code disk;
Said housing and inside casing are ring, and housing is placed in outside the inside casing;
Azimuth-drive motor and orientation photoelectric code disk are fixed on the base, and azimuth-drive motor is connected with housing with cylindrical gear mechanism through transmission shaft, drive housing and do the azimuth direction rotation;
Pitching motor and pitching photoelectric code disk are installed on the housing, and pitching motor is connected with inside casing, drive inside casing and do the pitch orientation rotation.
2. prober composite shaft according to claim 1 mechanism is characterized in that: said housing can be done the rotation of azimuth direction ± 45 °.
3. prober composite shaft according to claim 1 mechanism is characterized in that: said inside casing can be done the rotation of pitch orientation ± 45 °.
4. prober composite shaft according to claim 1 mechanism, it is characterized in that: the velocity ratio of said cylindrical gear mechanism is 1:1.
CN2011102967078A 2011-09-30 2011-09-30 Composite shaft structure of detector Pending CN102434763A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2011102967078A CN102434763A (en) 2011-09-30 2011-09-30 Composite shaft structure of detector

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2011102967078A CN102434763A (en) 2011-09-30 2011-09-30 Composite shaft structure of detector

Publications (1)

Publication Number Publication Date
CN102434763A true CN102434763A (en) 2012-05-02

Family

ID=45982997

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2011102967078A Pending CN102434763A (en) 2011-09-30 2011-09-30 Composite shaft structure of detector

Country Status (1)

Country Link
CN (1) CN102434763A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103674842A (en) * 2013-12-20 2014-03-26 河北汉光重工有限责任公司 Telemetering rotary table

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1276675A (en) * 2000-06-27 2000-12-13 浙江南望图像信息产业有限公司 Intelligent spherical camera with automatic ominibearing search of target
CN101035202A (en) * 2006-03-10 2007-09-12 上海乐金广电电子有限公司 Pitching device for monitor
CN101089657A (en) * 2007-07-13 2007-12-19 中国人民解放军理工大学气象学院 Three servo device of optical nephoscope
US20080246847A1 (en) * 2007-04-06 2008-10-09 Canon Kabushiki Kaisha Imaging apparatus and pan/tilt head control method
CN101619971A (en) * 2009-07-31 2010-01-06 北京航空航天大学 Aerophotography gyrostabilized platform with three freedom degrees and large load
CN202252673U (en) * 2011-09-30 2012-05-30 四川九洲电器集团有限责任公司 Compound axis structure of detector

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1276675A (en) * 2000-06-27 2000-12-13 浙江南望图像信息产业有限公司 Intelligent spherical camera with automatic ominibearing search of target
CN101035202A (en) * 2006-03-10 2007-09-12 上海乐金广电电子有限公司 Pitching device for monitor
US20080246847A1 (en) * 2007-04-06 2008-10-09 Canon Kabushiki Kaisha Imaging apparatus and pan/tilt head control method
CN101089657A (en) * 2007-07-13 2007-12-19 中国人民解放军理工大学气象学院 Three servo device of optical nephoscope
CN101619971A (en) * 2009-07-31 2010-01-06 北京航空航天大学 Aerophotography gyrostabilized platform with three freedom degrees and large load
CN202252673U (en) * 2011-09-30 2012-05-30 四川九洲电器集团有限责任公司 Compound axis structure of detector

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103674842A (en) * 2013-12-20 2014-03-26 河北汉光重工有限责任公司 Telemetering rotary table

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Application publication date: 20120502