CN202350775U - Multifunctional laser aid of gyrotheodolite - Google Patents
Multifunctional laser aid of gyrotheodolite Download PDFInfo
- Publication number
- CN202350775U CN202350775U CN 201120514652 CN201120514652U CN202350775U CN 202350775 U CN202350775 U CN 202350775U CN 201120514652 CN201120514652 CN 201120514652 CN 201120514652 U CN201120514652 U CN 201120514652U CN 202350775 U CN202350775 U CN 202350775U
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- gyro
- theodolite
- holder
- laser
- assistor
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Abstract
The utility model relates to a multifunctional laser aid of a gyrotheodolite, which comprises a replaceable part and a fixed seat connected with the replaceable part. The other end of the fixed seat is provided with an adjustment support, and the front end of the adjustment support is provided with a laser source and a switch. One end of the replaceable part is provided with a clamping sleeve, the other end of the replaceable part is provided with a screw hole, and the replaceable part is connected with the fixed seat through the screw hole. The utility model has the technical effects that: 1, a simple and easy-to-remove auxiliary light source device is provided for alignment testing of self-alignment values of various gyrotheodolites via replaceable parts with different diameters, and a centering auxiliary light source can also be provided when the replaceable parts are arranged at the bottom of the gyrotheodolite; 2, the resistance to environmental interference is high, the size is small, the structure is simple, the operation is convenient and rapid, the stability is high, the efficiency of alignment can be greatly improved, the cost is low, the performance-price ratio is high, and the capacity of expansion is high; and 3, the multifunctional laser aid has high brightness, high detection accuracy, long service life and good stability and can be used conveniently, and the energy consumption is low.
Description
Technical field
The utility model belongs to boats and ships aim detecting applied technical field, and gyro-theodolite is used the multifunction laser assistor when being specifically related to a kind of boats and ships aim detecting.
Background technology
Aim detecting is the important content in the boats and ships development engineering, is the important step of setting up unified deck coordinate system.Shipbuilding is a complicated system engineering, and system's (equipment) in order to satisfy its user demand, must carry out aim detecting to its bearing accuracy after installation.
At present, the gyro-theodolite mensuration is one of main method of equipment bearing accuracy aim detecting in the marine system aim detecting.Come the equipment position angle is aimed at through gyro-theodolite autocollimatic value function during measurement; But because the restriction of gyro-theodolite itself; The general light that penetrates a little less than, in the measurement of reality, require a great deal of time and energy is sought the light beam that reflects, and instrumentation for a long time; Make eye fatigue easily, work efficiency is difficult to improve.
Gyro-theodolite centering is one of operation necessary before it uses, and moment gyroscope transit centering is mostly used the centering mode of hanging plummet, its complex operation, and inefficiency, and this method is affected by the external environment greatlyyer, causes the bigger error of centralization easily.
Therefore; Can search out flare intuitively if having a kind of simple utility appliance to be installed in to send intense light source on the gyro-theodolite lens barrel; Can will increase work efficiency greatly for gyro-theodolite provides laser alignment required light source again, save human resources; Thereby the generation high economic benefit, and have wide practical use.
Summary of the invention
The utility model technical matters to be solved is to overcome the deficiency of prior art, provides a kind of gyro-theodolite to use the multifunction laser assistor, and this assistor does not receive power limitations; Not disturbed by other light sources; It is little to have volume, simple in structure, easy to use; Working time is long, high reliability features.
The technical scheme that the utility model adopted is: include Replacement Part and the holder that links to each other with Replacement Part, the other end of holder is installed the adjustment bearing, and adjustment bearing front end is installed on lasing light emitter and deploy switch.
Press such scheme, described Replacement Part one end is a cutting ferrule, and the other end is provided with screw, links to each other with holder through screw.The cutting ferrule diameter of field-replaceable unit can be changed according to the gyro-theodolite of various lens barrel bores, also can be assembled to various gyro-theodolites bottom.
Press such scheme, said holder middle part offers cavity, and ball seat is offered at the cavity middle part, and described adjustment bearing is installed in bulb and the ball seat phase configuration that is provided with through the rear end in the cavity, and links to each other with holder through three adjustment screws.Come the calibration beam direction through adjustment adjustment screw.
Press such scheme, the pipe box that the setting of described adjustment bearing front end is extended is forward installed lasing light emitter in the pipe box.
Press such scheme, described lasing light emitter comprises laser tube and power supply, and said laser tube is the high-precision laser pipe.
The utility model method of application is following:
The first step; Auxiliary gyro-theodolite autocollimatic value is aimed at: earlier gyro-theodolite is set up, select to be connected with holder with the corresponding Replacement Part of gyro-theodolite lens barrel bore, the laser assistor is set on the gyro-theodolite lens barrel; Open light source switch, seek flare; Second step; Auxiliary gyro-theodolite centering: gyro-theodolite is set up, select to be connected with holder, the laser assistor is installed in the gyro-theodolite bottom with the corresponding Replacement Part of gyro-theodolite; Open light source switch, hot spot carries out centering to gyro-theodolite on the deck plane by being radiated at.
The technique effect of the utility model is: a simple and easy detachable secondary light source equipment is provided when 1, the Replacement Part through different bores is various gyro-theodolite autocollimatic value aim detecting, also can be installed in the gyro-theodolite bottom through field-replaceable unit and does centering and use secondary light source; 2, it is strong to have an anti-environmental disturbances ability, and volume is little, and is simple in structure, simple operation, and the characteristics that stability is high can improve the efficient of alignment work greatly, and with low costly have very high cost performance and a very strong expansion capability; 3, not only brightness is big, and accuracy of detection is high, and is easy to use, and long service life, and energy consumption is low, good stability.
Description of drawings
Fig. 1 is the front elevation of an embodiment of the utility model.
Fig. 2 is the positive view of an embodiment of the utility model.
Fig. 3 is the user mode figure of the utility model.
Embodiment
Below in conjunction with accompanying drawing the utility model is described further.
Include Replacement Part 1; Described Replacement Part one end is a cutting ferrule, and the other end is provided with screw, links to each other with holder through screw; The cutting ferrule diameter of Replacement Part can be changed according to the gyro-theodolite 8 of various lens barrel bores, also can be assembled to various gyro-theodolites bottom.Holder 2 one ends are provided with bolt; Link to each other with part more through bolt, holder other end middle part offers cavity, and ball seat is offered at the cavity middle part; Adjustment bearing 4 is installed in bulb and the ball seat phase configuration that is provided with through the rear end in the cavity, and links to each other with holder through three adjustment screws 3; The pipe box that the setting of adjustment bearing front end is extended is forward installed lasing light emitter and deploy switch 5 in the pipe box, described lasing light emitter comprises laser tube 6 and power supply 7, and said laser tube is the high-precision laser pipe.The all available aluminium of described Replacement Part, holder and adjustment bearing is processed.The utility model comes the calibration laser beam direction through adjustment adjustment screw.
Claims (5)
1. a gyro-theodolite is used the multifunction laser assistor, it is characterized in that including Replacement Part and the holder that links to each other with Replacement Part, and the other end of holder is installed the adjustment bearing, and adjustment bearing front end is installed on lasing light emitter and deploy switch.
2. gyro-theodolite as claimed in claim 1 is used the multifunction laser assistor, it is characterized in that described Replacement Part one end is a cutting ferrule, and the other end is provided with screw, links to each other with holder through screw.
3. according to claim 1 or claim 2 gyro-theodolite is used the multifunction laser assistor; It is characterized in that said holder middle part offers cavity; Ball seat is offered at the cavity middle part; Described adjustment bearing is installed in bulb and the ball seat phase configuration that is provided with through the rear end in the cavity, and links to each other with holder through three adjustment screws.
4. according to claim 1 or claim 2 gyro-theodolite is used the multifunction laser assistor, it is characterized in that the pipe box that the setting of described adjustment bearing front end is extended forward, installs lasing light emitter in the pipe box.
5. gyro-theodolite as claimed in claim 4 is used the multifunction laser assistor, it is characterized in that described lasing light emitter comprises laser tube and power supply, and said laser tube is the high-precision laser pipe.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201120514652 CN202350775U (en) | 2011-12-12 | 2011-12-12 | Multifunctional laser aid of gyrotheodolite |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201120514652 CN202350775U (en) | 2011-12-12 | 2011-12-12 | Multifunctional laser aid of gyrotheodolite |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202350775U true CN202350775U (en) | 2012-07-25 |
Family
ID=46539774
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201120514652 Expired - Lifetime CN202350775U (en) | 2011-12-12 | 2011-12-12 | Multifunctional laser aid of gyrotheodolite |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202350775U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103913597A (en) * | 2014-03-27 | 2014-07-09 | 北京航天控制仪器研究所 | Centering monitoring system for spinning top accelerometer floater |
| CN111238453A (en) * | 2018-11-28 | 2020-06-05 | 赫克斯冈技术中心 | Intelligent positioning module |
| CN114935327A (en) * | 2022-04-26 | 2022-08-23 | 中国舰船研究设计中心 | Improvement method of deck theodolite |
-
2011
- 2011-12-12 CN CN 201120514652 patent/CN202350775U/en not_active Expired - Lifetime
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103913597A (en) * | 2014-03-27 | 2014-07-09 | 北京航天控制仪器研究所 | Centering monitoring system for spinning top accelerometer floater |
| CN111238453A (en) * | 2018-11-28 | 2020-06-05 | 赫克斯冈技术中心 | Intelligent positioning module |
| US11486704B2 (en) | 2018-11-28 | 2022-11-01 | Hexagon Technology Center Gmbh | Intelligent positioning module |
| CN111238453B (en) * | 2018-11-28 | 2023-09-05 | 赫克斯冈技术中心 | Intelligent positioning module |
| CN114935327A (en) * | 2022-04-26 | 2022-08-23 | 中国舰船研究设计中心 | Improvement method of deck theodolite |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term |
Granted publication date: 20120725 |
|
| CX01 | Expiry of patent term |