CN204154518U - Artillery reconnaissance vehicle servo platform corner accuracy testing agency - Google Patents
Artillery reconnaissance vehicle servo platform corner accuracy testing agency Download PDFInfo
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- CN204154518U CN204154518U CN201420568237.5U CN201420568237U CN204154518U CN 204154518 U CN204154518 U CN 204154518U CN 201420568237 U CN201420568237 U CN 201420568237U CN 204154518 U CN204154518 U CN 204154518U
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Abstract
The utility model discloses a kind of artillery reconnaissance vehicle servo platform corner accuracy testing agency, and the base top surface in aiming group is fixed with the first sleeve, and the first sleeve upper end is connected with the second sleeve, is inserted with the 3rd sleeve in first and second sleeve; 3rd sleeve top is fixed with one block of supporting plate, and the erecting frame of autocollimator is supported on supporting plate, and the camera end banding of autocollimator has adapter sleeve, and there is web joint adapter sleeve lower end; In the U-lag of web joint right-hand member, card has a positioning stud, and the adjusting nut on this root positioning stud top is fixed with CCD camera; Reflection group is located at the aiming group left side, and holder is wherein fixed with stud, and on stud, cover has Triangulum reed, and on the stud of Triangulum reed upper and lower, each cover has set nut; Leveling board end face is provided with eight prisms, is installed with level at eight prism end faces by backing plate.The utility model can facilitate, detect accurately the corner accuracy of scout car servo platform, thus ensures that the high precision of servo platform is run well.
Description
Technical field
The utility model belongs to a kind of accuracy detection mechanism, specifically, particularly relates to a kind of artillery reconnaissance vehicle servo platform corner accuracy testing agency.
Background technology
Scout car is that my army's artillery reconnaissance means are more complete at present, the large complicated Reconnaissance Equipment of the one that integration degree is higher, it collects white light, infrared, radar, laser ranging, satnav, traffic guidance is in one, relate to optics, electronics, computing machine, multiple fields such as machinery and traffic guidance, and primarily of chassis, information handling system, reconnaissance system (ccd video camera on car, thermal infrared imager, socut and adjust radar, range finder using laser and laser eyepiece indicating module), positioning and orientation system, servo-drive system, communication system, reconnaissance system round the clock under car, defence system, power control system and subsystem 10 subsystem compositions.Utilize this equipment, all-weather reconnaissance operation can be completed.
At present, the scout car being representative with XXX series artillery reconnaissance vehicle equips army successively in a large number.But, research and development for the maintenance support equipment of novel scout car also relatively lag behind, fault detect, the maintenance support of equipment also need more to rely on equipment contractor, particularly under army's condition, shortage scout car CAN communication system and servo-drive system carry out accurate detection means, have a strong impact on the performance of scout car fighting efficiency, do not meet demand under battle conditions, be badly in need of the corresponding maintenance conditions equipment of exploitation, with the Support Resource construction of satisfied equipment, improve army's maintenance ability of this equipment.
Servo-drive system is as one of the key components of novel scout car, it is as the carrying platform of multiple photoelectronic reconnaissance equipment, its control accuracy is directly connected to the scouting precision of reconnaissance equipment, therefore must detect timely servo-drive system and calibrate, guarantee the precision of servo-drive system, demand under battle conditions could be met.But at present under army's condition, particularly difficult to the detection of servo-drive system corner accuracy, this is mainly because servo system structure is complicated, and control accuracy requires high, and calibration difficulty is large.
Utility model content
Technical problem to be solved in the utility model is the artillery reconnaissance vehicle servo platform corner accuracy testing agency providing a kind of precision high, easy to use.
The technical solution of the utility model is as follows: a kind of artillery reconnaissance vehicle servo platform corner accuracy testing agency, it is characterized in that: be made up of aiming group (M) and reflection group (F), wherein aiming group (M) comprises base (1) and autocollimator (8), wherein: described base (1) end face is vertically fixed with the first sleeve (2), this the first sleeve upper end coaxial threaded is connected with the second sleeve (3), is inserted with the 3rd sleeve (4) in first and second sleeve; Described 3rd sleeve (4) lower end is connected with sleeve nut (5), this sleeve nut can by the center pit axial limiting of the second sleeve (3), and the root of the 3rd sleeve (4) outer wall and two set levers (6) is adjacent to, these two set levers are connected with the threaded hole on described second sleeve (3); Described 3rd sleeve (4) upper horizontal is fixed with one piece of supporting plate (7), the erecting frame that described autocollimator (8) carries is supported on this supporting plate top surface, have an adapter sleeve (9) at the camera end banding of autocollimator, this adapter sleeve lower end level is fixed with one piece of web joint (10); Described web joint (10) right-hand member has the U-lag of a up/down perforation, in this U-lag, card has a positioning stud (11), this root positioning stud top is connected with an adjusting nut (12), and this adjusting nut end face level is fixed with a CCD camera (13);
Described reflection group (F) is located at aiming group (M) left side, and comprise holder (14) and coupling shaft (22), wherein holder (14) end face is vertically fixed with a stud (15), on this stud, cover has a Triangulum reed (16), and the stud (15) of Triangulum reed upper and lower is respectively set with a set nut; Three angles of described Triangulum reed (16) are vertically provided with a supporting studs (17) respectively, this supporting studs and Triangulum reed (16) are rotatably assorted, and the lower end of supporting studs (17) is supported on described holder (14) end face, and every root supporting studs (17) upper end is set with a nut, these three nuts are fixed on same leveling board (18) bottom surface; Described leveling board (18) end face is provided with eight prism (19), and on eight prism end faces, level is provided with one piece of backing plate (20), and the upper face of this backing plate is installed with the level (21) of two bar shapeds; After the center pit of leveling board (18) and eight prisms (19) is passed in described coupling shaft (22) lower end, be threaded with described holder (14), the threaded upper ends of this coupling shaft is connected with a handle.
Before detection, the holder (14) of reflection group (F) is fixed on the center at reconnaissance platforms top, and the base (1) of aiming group (M) is placed on roof parallel light tube bracing frame, and adjust height and the horizontal level of autocollimator, and controlling servo rotation, the reflection image of the autocollimator division line that CCD thecamera head is arrived to notebook computer display image viewing overlaps with autocollimator division line images themselves.During detection, rotate reconnaissance platforms division line reflection image and division line images themselves overlapping positions extremely for the first time, the difference reading servo turning angle and 45 degree in display window is the running accuracy that servo rotates 45 degree, the like namely obtain the running accuracy that servo rotates 90 degree, 135 degree, 180 degree, 225 degree, 270 degree, 315 degree, 360 degree.
Adopt above technical scheme, the utility model can facilitate, detect accurately the corner accuracy of scout car servo platform, thus ensures that the high precision of servo platform is run well, and the structure of this testing agency is simple, easy to implement, has good practicality.
In order to improve calibration accuracy, two described levels (21) are mutually vertical.
Beneficial effect: the utility model can facilitate, detect accurately the corner accuracy of scout car servo platform, thus ensure that the high precision of servo platform is run well, and the structure of this testing agency is simple, easy to implement, there is good practicality.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model;
Fig. 2 is the structural representation of aiming group in Fig. 1;
Fig. 3 is the structural representation of reflection group in Fig. 1;
Fig. 4 is the vertical view of Fig. 3.
Embodiment
Below in conjunction with drawings and Examples, the utility model is described in further detail:
As shown in Fig. 1,2,3 and 4, a kind of artillery reconnaissance vehicle servo platform corner accuracy testing agency, this testing agency is formed by aiming at group M and reflection group F.Wherein, described aiming group M is formed primarily of base 1, first sleeve 2, second sleeve 3, the 3rd sleeve 4, sleeve nut 5, set lever 6, supporting plate 7, autocollimator 8, adapter sleeve 9, web joint 10, positioning stud 11, adjusting nut 12 and CCD camera 13.Wherein, described base 1 end face is vertically fixed with the first sleeve 2, and the upper end coaxial threaded of this first sleeve 2 is connected with the second sleeve 3, in the first sleeve 2 and the second sleeve 3, be inserted with the 3rd sleeve 4.The lower end of described 3rd sleeve 4 is connected with sleeve nut 5, this sleeve nut 5 can by the center pit axial limiting of the second sleeve 3, and the root of the 3rd sleeve 4 outer wall and two set levers 6 is adjacent to, these two set levers 6 are connected with the threaded hole on the second sleeve 3, so just can adjust the height of the 3rd sleeve 4.
The upper horizontal of described 3rd sleeve 4 is fixed with one block of supporting plate 7, and the autocollimator 8 of outsourcing carries erecting frame, and this erecting frame is supported on the end face of this supporting plate 7.Have an adapter sleeve 9 at the camera end banding of autocollimator 8, the lower end level of this adapter sleeve 9 is fixed with one piece of web joint 10.Described web joint 10 right-hand member has the U-lag of a up/down perforation, in this U-lag, card has a positioning stud 11, the top of this root positioning stud 11 is connected with an adjusting nut 12, and the end face level of this adjusting nut 12 is fixed with the CCD camera 13 of an outsourcing.
As shown in Fig. 1,2,3 and 4, described reflection group F is located at the aiming group M left side, and forms primarily of holder 14, stud 15, Triangulum reed 16, supporting studs 17, leveling board 18, eight prism 19, backing plate 20, level 21 and coupling shaft 22.Wherein, the end face of holder 14 is vertically fixed with a stud 15, on this stud 15, cover has a Triangulum reed 16, and the stud 15 of Triangulum reed 16 upper and lower is respectively set with a set nut.Three angles of described Triangulum reed 16 are vertically provided with a supporting studs 17 respectively, this supporting studs 17 is rotatably assorted with Triangulum reed 16, and the lower end of supporting studs 17 is supported on the end face of holder 14, and every root supporting studs 17 upper end is set with a nut, these three nuts are fixed on same leveling board 18 bottom surface.
The end face of described leveling board 18 is provided with eight prisms 19 of an outsourcing, on the end face of eight prisms 19, level is provided with one piece of backing plate 20, the upper face of this backing plate 20 is installed with the level 21 of two bar shapeds, and this level 21 is outsourcing piece, and two levels 21 are mutually vertical.After the center pit of leveling board 18 and eight prisms 19 is passed in described coupling shaft 22 lower end, be threaded with described holder 14, the threaded upper ends of this coupling shaft 22 is connected with a handle.
The foregoing is only preferred embodiment of the present utility model; it is not restriction with the utility model; all do within spirit of the present utility model and principle any amendment, equivalent to replace and improvement etc., all should be included within protection domain of the present utility model.
Claims (2)
1. an artillery reconnaissance vehicle servo platform corner accuracy testing agency, it is characterized in that: be made up of aiming group (M) and reflection group (F), wherein aiming group (M) comprises base (1) and autocollimator (8), wherein: described base (1) end face is vertically fixed with the first sleeve (2), this the first sleeve upper end coaxial threaded is connected with the second sleeve (3), is inserted with the 3rd sleeve (4) in first and second sleeve; Described 3rd sleeve (4) lower end is connected with sleeve nut (5), this sleeve nut can by the center pit axial limiting of the second sleeve (3), and the root of the 3rd sleeve (4) outer wall and two set levers (6) is adjacent to, these two set levers are connected with the threaded hole on described second sleeve (3); Described 3rd sleeve (4) upper horizontal is fixed with one piece of supporting plate (7), the erecting frame that described autocollimator (8) carries is supported on this supporting plate top surface, have an adapter sleeve (9) at the camera end banding of autocollimator, this adapter sleeve lower end level is fixed with one piece of web joint (10); Described web joint (10) right-hand member has the U-lag of a up/down perforation, in this U-lag, card has a positioning stud (11), this root positioning stud top is connected with an adjusting nut (12), and this adjusting nut end face level is fixed with a CCD camera (13);
Described reflection group (F) is located at aiming group (M) left side, and comprise holder (14) and coupling shaft (22), wherein holder (14) end face is vertically fixed with a stud (15), on this stud, cover has a Triangulum reed (16), and the stud (15) of Triangulum reed upper and lower is respectively set with a set nut; Three angles of described Triangulum reed (16) are vertically provided with a supporting studs (17) respectively, this supporting studs and Triangulum reed (16) are rotatably assorted, and the lower end of supporting studs (17) is supported on described holder (14) end face, and every root supporting studs (17) upper end is set with a nut, these three nuts are fixed on same leveling board (18) bottom surface; Described leveling board (18) end face is provided with eight prism (19), and on eight prism end faces, level is provided with one piece of backing plate (20), and the upper face of this backing plate is installed with the level (21) of two bar shapeds; After the center pit of leveling board (18) and eight prisms (19) is passed in described coupling shaft (22) lower end, be threaded with described holder (14), the threaded upper ends of this coupling shaft is connected with a handle.
2. artillery reconnaissance vehicle servo platform corner accuracy testing agency according to claim 1, is characterized in that: two described levels (21) are mutually vertical.
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CN201420568237.5U CN204154518U (en) | 2014-09-29 | 2014-09-29 | Artillery reconnaissance vehicle servo platform corner accuracy testing agency |
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CN201420568237.5U CN204154518U (en) | 2014-09-29 | 2014-09-29 | Artillery reconnaissance vehicle servo platform corner accuracy testing agency |
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Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
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CN106556359A (en) * | 2016-11-25 | 2017-04-05 | 中车戚墅堰机车有限公司 | The method that body axiality is detected using body coaxality measuring mechanism |
CN107478575A (en) * | 2017-09-29 | 2017-12-15 | 无锡创想分析仪器有限公司 | One kind rotates adjustable type spectroanalysis instrument |
CN107765279A (en) * | 2017-10-17 | 2018-03-06 | 北京航天发射技术研究所 | A kind of fusion inertia, the vehicle positioning directional sighting system and method for sight of satellite |
CN109297508A (en) * | 2018-08-11 | 2019-02-01 | 西安应用光学研究所 | A kind of vehicular photoelectric system sport car accuracy test device and method |
CN112325114A (en) * | 2020-10-30 | 2021-02-05 | 中国船舶重工集团公司第七0七研究所 | Portable adjusting support for erecting autocollimator and adjusting method |
CN114234855A (en) * | 2021-11-22 | 2022-03-25 | 北京航天控制仪器研究所 | Small-angle corner calibration device and method for galvanometer motor |
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2014
- 2014-09-29 CN CN201420568237.5U patent/CN204154518U/en not_active Expired - Fee Related
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106556359A (en) * | 2016-11-25 | 2017-04-05 | 中车戚墅堰机车有限公司 | The method that body axiality is detected using body coaxality measuring mechanism |
CN107478575A (en) * | 2017-09-29 | 2017-12-15 | 无锡创想分析仪器有限公司 | One kind rotates adjustable type spectroanalysis instrument |
CN107765279A (en) * | 2017-10-17 | 2018-03-06 | 北京航天发射技术研究所 | A kind of fusion inertia, the vehicle positioning directional sighting system and method for sight of satellite |
CN107765279B (en) * | 2017-10-17 | 2020-08-07 | 北京航天发射技术研究所 | Vehicle-mounted positioning and directional aiming system and method integrating inertia and satellite |
CN109297508A (en) * | 2018-08-11 | 2019-02-01 | 西安应用光学研究所 | A kind of vehicular photoelectric system sport car accuracy test device and method |
CN109297508B (en) * | 2018-08-11 | 2022-08-09 | 西安应用光学研究所 | Vehicle-mounted photoelectric system running precision inspection device and method |
CN112325114A (en) * | 2020-10-30 | 2021-02-05 | 中国船舶重工集团公司第七0七研究所 | Portable adjusting support for erecting autocollimator and adjusting method |
CN114234855A (en) * | 2021-11-22 | 2022-03-25 | 北京航天控制仪器研究所 | Small-angle corner calibration device and method for galvanometer motor |
CN114234855B (en) * | 2021-11-22 | 2024-04-09 | 北京航天控制仪器研究所 | Small-angle rotation angle calibration device and method for vibrating mirror motor |
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C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150211 Termination date: 20150929 |
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EXPY | Termination of patent right or utility model |