CN101614503B - Multi-axis detection and correction device for 25 mm self-propelled anti-aircraft gun - Google Patents
Multi-axis detection and correction device for 25 mm self-propelled anti-aircraft gun Download PDFInfo
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- CN101614503B CN101614503B CN2009100172971A CN200910017297A CN101614503B CN 101614503 B CN101614503 B CN 101614503B CN 2009100172971 A CN2009100172971 A CN 2009100172971A CN 200910017297 A CN200910017297 A CN 200910017297A CN 101614503 B CN101614503 B CN 101614503B
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Abstract
The invention provides a multi-axis detection and correction device for a 25 mm self-propelled anti-aircraft gun, which comprises a measurement carrier provided with a guide rod, a display operation meter box connected with the measurement carrier, and a double-parallel light pipe connected with the display operation meter box and provided with a bracket, wherein the measurement carrier is internally provided with a dip angle sensor, the display operation meter box comprises a charger module, a storage cell and an intelligent display module, the charger module is connected with the storage cell, the storage cell is connected with the intelligent display module, the charger module is connected with the intelligent display module, the measurement carrier is connected with the intelligent display module, and the intelligent display module is also connected with the double-parallel light pipe. The correction device can rapidly adjust the parallelism of a gun pipe, correct the light axis and have simple operation.
Description
Technical field:
What the present invention relates to is a kind of detection means for correcting, and especially a kind of multiaxis line that is used for 25 millimeters Self propelled Antiaircraft Gun detects means for correcting.
Background technology:
In the prior art, technique known is that the gun tube to 25 millimeters Self propelled Antiaircraft Gun carries out timing, uses the school to take aim at target plate, and will detect the car body leveling through peephole, and complex operation is complicated, lose time, and error is big; To the correction of 25 millimeters Self propelled Antiaircraft Gun optical axis, selecting the infinity target for use is that benchmark is proofreaied and correct, and is subject to the restriction of environmental condition, does not reach desirable calibration result, and this is the existing in prior technology weak point.
Summary of the invention:
The object of the invention is exactly not enough to existing in prior technology; And provide a kind of multiaxis line that is used for 25 millimeters Self propelled Antiaircraft Gun to detect the technical scheme of means for correcting; The means for correcting of this scheme can be adjusted the depth of parallelism of gun tube fast, and optical axis is proofreaied and correct, and simple to operate.
This programme is realized through following technical measures: a kind of multiaxis line that is used for 25 millimeters Self propelled Antiaircraft Gun detects means for correcting; The characteristics of this programme are: comprise the measurement carrier that has guide rod; With the display operation instrument box that the measurement carrier is connected, the two parallel light tubes that have support that are connected with the display operation instrument box in addition; Be provided with obliquity sensor in the said measurement carrier; Described display operation instrument box comprises charger module, battery and intelligent display module; Said charger module is connected with battery, and battery is connected with intelligent display module, and described charger module is connected with intelligent display module; Described measurement carrier is connected with intelligent display module, and described intelligent display module also is connected with two parallel light tubes.Be provided with three measurement levels respectively, height and azimuthal obliquity sensor in the described measurement carrier.Be provided with visible light pipe parallel to each other and infrared light pipe in the described pair of parallel light tube, in visible light pipe and the infrared light pipe light-emitting device arranged all, described light-emitting device is supplied power by intelligent display module.The support of described pair of parallel light tube comprises stationary plane and supporting surface for L shaped, and the lapping plate that angle of site set screw is arranged on the stationary plane and fix with gun turret has the azimuth adjustment screw on the supporting surface, between stationary plane and supporting surface, be provided with oblique arm-tie.
The beneficial effect of this programme can be learnt according to the narration to such scheme; Because the measurement carrier that has guide rod is arranged in this scheme; Measure carrier and be connected, measure in the carrier and be provided with three measurement of dip angle sensors, measure level, height and the inclination angle, orientation of gun tube respectively with intelligent display module.
The intelligent display module of display operation instrument box shows horizontal angle, the angle of site and the azimuth of the gun tube of measuring the carrier measurement; Charger module can charge the battery, also can be directly to intelligent display module power supply, the use of convenient whole device; Battery can make whole device still can work under the situation of external power supply not having.
Be provided with the visible light pipe and the infrared light pipe that are parallel to each other in two parallel light tubes have, can be used as the external calibration standard of optical axis and TV axle, the handled easily personnel proofread and correct; In addition, intelligent display module is connected with two parallel light tubes, gives two parallel light tube power supplies.
Two parallel light tubes also have a L bracket, are convenient on car body, install two parallel light tubes; This shows that the present invention compared with prior art has outstanding substantive distinguishing features and obvious improvement, the beneficial effect of its enforcement also is conspicuous.
Description of drawings:
Fig. 1 is the structural representation of the specific embodiment of the invention.
Fig. 2 is two parallel light tubes and supporting structure sketch map.
Among the figure, 1 is charger module, and 2 is two parallel light tubes, and 3 is guide rod, and 4 for measuring carrier; 5 is intelligent display module, and 6 is battery, and 7 is visible light pipe, and 8 is supporting surface, and 9 is oblique arm-tie; 10 is the azimuth adjustment screw, and 11 are angle of site set screw, and 12 is stationary plane, and 13 is gun turret; 14 is lapping plate, and 15 is infrared light pipe, and 16 is two parallel light tube supports, and 17 is the display operation instrument box.
The specific embodiment:
For clearly demonstrating the technical characterstic of this programme,, and, this programme is set forth in conjunction with its accompanying drawing below by a specific embodiment.
Can find out through accompanying drawing; The multiaxis line that is used for 25 millimeters Self propelled Antiaircraft Gun of this programme detects means for correcting; The characteristics of this programme are: comprise the measurement carrier 4 that has guide rod 3; With the display operation instrument box 17 that measurement carrier 4 is connected, the two parallel light tubes 2 that have support 16 that are connected with display operation instrument box 17 in addition; Be provided with obliquity sensor in the said measurement carrier 4; Described display operation instrument box 17 comprises charger module 1, battery 6 and intelligent display module 5; Said charger module 1 is connected with battery 6, and battery 6 is connected with intelligent display module 5, and described charger module 1 is connected with intelligent display module 5; Described measurement carrier 4 is connected with intelligent display module 5, and described intelligent display module 5 also is connected with two parallel light tubes 2.Be provided with three measurement levels respectively, height and azimuthal obliquity sensor in the described measurement carrier 4.Be provided with visible light pipe parallel to each other 7 and infrared light pipe 15 in the described pair of parallel light tube 2, in visible light pipe 7 and the infrared light pipe 15 light-emitting device arranged all, described light-emitting device is by intelligent display module 5 power supplies.The support 16 of described pair of parallel light tube 2 is for L shaped; Comprise stationary plane 12 and supporting surface 8; The lapping plate 14 that angle of site set screw 11 is arranged on the stationary plane 12 and fix with gun turret 13 has azimuth adjustment screw 10 on the supporting surface 8, between stationary plane 12 and supporting surface 8, be provided with oblique arm-tie 9.
During use; The measurement carrier 4 that has guide rod 3 is inserted in the benchmark gun tube, then on intelligent display module 5, will demonstrate corresponding angle, after angle zero setting; To measure carrier 4 again and put into other gun tubes; Then intelligent display module 5 will demonstrate the misalignment angle of other gun tube with prover pipe, through other parts of adjustment gun tube, make the gun tube of transferring consistent with the base piece tube's axis.
To three light microscopics, infrared optical axis and the adjustment of TV cross hairs the time; The support 16 of two parallel light tubes 2 is fixed on the gun turret 13; Then two parallel light tubes 2 are fixed on the supporting surface 8 of support 16; This moment, two parallel light tubes 2 just became the external calibration benchmark of three light microscopics, infrared optical axis and TV cross hairs; The light-emitting device of two parallel light tubes 2 is a bulb, and intelligent display module 5 just can be observed visible light pipe 7 and produce an infinity visible light target cross hairs for bulb provides electric energy in the aiming eyepiece; 15 of infrared light pipes produce an infinity infrared light target cross hairs, and the adjustment personnel just can be by these two cross hairs adjustment, need not be by external object, for adjustment brings convenience.
The present invention is not limited in the above-mentioned specific embodiment, and the variation that those of ordinary skills make in essential scope of the present invention, remodeling, interpolation or replacement also should belong to protection scope of the present invention.
Claims (2)
1. a multiaxis line that is used for 25 millimeters Self propelled Antiaircraft Gun detects means for correcting; It is characterized in that: comprise the measurement carrier [4] that has guide rod [3]; With the display operation instrument box [17] that measurement carrier [4] is connected, the two parallel light tubes [2] that have support [16] that are connected with display operation instrument box [17] in addition; Be provided with three measurement levels respectively, height and azimuthal obliquity sensor in the said measurement carrier [4]; Described display operation instrument box [17] comprises charger module [1], battery [6] and intelligent display module [5]; Said charger module [1] is connected with battery [6]; Battery [6] is connected with intelligent display module [5], and described charger module [1] is connected with intelligent display module [5], and described measurement carrier [4] is connected with intelligent display module [5]; Described intelligent display module [5] also is connected with two parallel light tubes [2]; Be provided with visible light pipe [7] parallel to each other and infrared light pipe [15] in the described pair of parallel light tube [2], in visible light pipe [7] and the infrared light pipe [15] light-emitting device arranged all, described light-emitting device is supplied power by intelligent display module [5].
2. the multiaxis line that is used for 25 millimeters Self propelled Antiaircraft Gun according to claim 1 detects means for correcting; It is characterized in that: the support [16] of described pair of parallel light tube [2] is for L shaped; Comprise stationary plane [12] and supporting surface [8]; The lapping plate [14] that angle of site set screw [11] is arranged on the stationary plane [12] and fix with gun turret [13] has azimuth adjustment screw [10] on the supporting surface [8], between stationary plane [12] and supporting surface [8], be provided with oblique arm-tie [9].
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009100172971A CN101614503B (en) | 2009-08-07 | 2009-08-07 | Multi-axis detection and correction device for 25 mm self-propelled anti-aircraft gun |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009100172971A CN101614503B (en) | 2009-08-07 | 2009-08-07 | Multi-axis detection and correction device for 25 mm self-propelled anti-aircraft gun |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN101614503A CN101614503A (en) | 2009-12-30 |
| CN101614503B true CN101614503B (en) | 2012-06-27 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN2009100172971A Expired - Fee Related CN101614503B (en) | 2009-08-07 | 2009-08-07 | Multi-axis detection and correction device for 25 mm self-propelled anti-aircraft gun |
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Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102162708B (en) * | 2010-12-17 | 2013-09-25 | 中国人民解放军军械工程学院 | Cannon barrel axial line positioner |
| CN102519421A (en) * | 2011-12-06 | 2012-06-27 | 沈阳第三三○一工厂 | Synchronicity detector of mirror gun |
| CN108507501B (en) * | 2017-02-28 | 2020-01-24 | 北京卓力新航科技有限责任公司 | Portable artillery multi-barrel axis parallelism detector |
| CN106949782B (en) * | 2017-04-27 | 2018-11-27 | 中国人民解放军防空兵学院 | A kind of axis means for correcting and method |
| CN108645334A (en) * | 2018-05-04 | 2018-10-12 | 中国船舶重工集团公司第七0七研究所 | A kind of barrel axis measuring device and method |
| CN114111447B (en) * | 2021-11-15 | 2023-04-28 | 中国人民解放军32286部队50分队 | Multi-path aiming axis parallelism adjusting device for rotary arm type platform |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4870290A (en) * | 1988-09-26 | 1989-09-26 | Honeywell Inc. | Object motion sensing and measuring apparatus using position sensing detectors |
| CN2174679Y (en) * | 1993-09-25 | 1994-08-17 | 中国科学院沈阳自动化研究所 | Automatic defect checking device for inner bore of cannon |
| CN1727864A (en) * | 2005-01-13 | 2006-02-01 | 中国科学院长春光学精密机械与物理研究所 | A kind of static angular pick-up unit of portable optical observation sighting instrument |
| CN2823968Y (en) * | 2005-10-31 | 2006-10-04 | 兰州北方机械厂 | Laser target corrector |
| CN201034471Y (en) * | 2007-04-24 | 2008-03-12 | 南京北方光电装备技术有限公司 | All-weather gun calibration instrument |
-
2009
- 2009-08-07 CN CN2009100172971A patent/CN101614503B/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4870290A (en) * | 1988-09-26 | 1989-09-26 | Honeywell Inc. | Object motion sensing and measuring apparatus using position sensing detectors |
| CN2174679Y (en) * | 1993-09-25 | 1994-08-17 | 中国科学院沈阳自动化研究所 | Automatic defect checking device for inner bore of cannon |
| CN1727864A (en) * | 2005-01-13 | 2006-02-01 | 中国科学院长春光学精密机械与物理研究所 | A kind of static angular pick-up unit of portable optical observation sighting instrument |
| CN2823968Y (en) * | 2005-10-31 | 2006-10-04 | 兰州北方机械厂 | Laser target corrector |
| CN201034471Y (en) * | 2007-04-24 | 2008-03-12 | 南京北方光电装备技术有限公司 | All-weather gun calibration instrument |
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| CN101614503A (en) | 2009-12-30 |
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