CN207113890U - A kind of Surveying Engineering high accuracy gyroscope instrument - Google Patents
A kind of Surveying Engineering high accuracy gyroscope instrument Download PDFInfo
- Publication number
- CN207113890U CN207113890U CN201721195480.7U CN201721195480U CN207113890U CN 207113890 U CN207113890 U CN 207113890U CN 201721195480 U CN201721195480 U CN 201721195480U CN 207113890 U CN207113890 U CN 207113890U
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- gyroscope
- high accuracy
- rotary body
- electro
- engineering high
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Abstract
The utility model discloses a kind of Surveying Engineering high accuracy gyroscope instrument, including base, electro-magnetic shielding cover and gyroscope rotary body, the base bottom is provided with aircraft, the chassis interior is provided with controller, control module is provided with the controller, locating module and communication module, the front of chassis is provided with infrared camera, the submounts are provided with rotating seat, the gyroscope rotary body is provided with above the rotating seat, and the gyroscope rotary body is connected as a single entity with the rotating seat, rotary inductor is installed in the rotating shaft of the gyroscope rotary body, distance measurement instrument is installed at the top of the rotating shaft, the electro-magnetic shielding cover is provided with the outside of the gyroscope rotary body.Beneficial effect is：The electro-magnetic shielding cover can isolate to the electromagnetic signal of surrounding, improve the degree of accuracy of DATA REASONING, while the data of measurement and position can be sent to Remote end in real time, the unapproachable tunnel of alternative manual measurement human body and grotto.
Description
Technical field
It the utility model is related to building engineering survey apparatus field, and in particular to a kind of Surveying Engineering high accuracy gyroscope
Instrument.
Background technology
Gyroscope is around being orthogonal to one of the axis of rotation with the moment of momentum sensitivity housing relative inertness space of high-speed rotator
Or the angular movement detection means of two axles.Gyroscope can not only coordinate with the camera on mobile phone, and image when making shooting is more
Clearly, also game operation effect can be realized, it may also be used for engineering survey as the sensor of various types of games.Application No.：
201610783734.0 Chinese patent, particular content is：A kind of spheroid rotor three-axis gyroscope is disclosed, belongs to gyroscope skill
Art field.Its spheroid rotor, pedestal, gimbal and gyroscope frame for including some sensors and arranging successively from inside to outside
Frame, the spheroid rotor and the pedestal of its periphery are rotatablely connected, and the pedestal is rotatablely connected with gimbal, gimbal and gyroscope
Frame member connects, and the spheroid rotor, pedestal, the center of rotation of gimbal and gyroscopes frame both pass through spheroid rotor
The centre of sphere, gyroscopes frame bottom connecting bracket seat.Though the gyroscope in above-mentioned patent provides self stability, can not realize
The remote transmission of measurement data, and spheroid rotor is easily disturbed by electromagnetic signal around when rotated, measurement data is produced mistake
Difference, it is therefore desirable to which a kind of Surveying Engineering is solved the above problems with high accuracy gyroscope instrument.
Utility model content
The purpose of this utility model is that to solve the above problems and provides a kind of Surveying Engineering high accuracy gyroscope
Instrument.
The utility model is achieved through the following technical solutions above-mentioned purpose：A kind of Surveying Engineering high accuracy gyroscope instrument,
Including base, electro-magnetic shielding cover and gyroscope rotary body, the base bottom is provided with aircraft, and the chassis interior is provided with
Controller, control module, locating module and communication module is provided with the controller, the front of chassis is provided with infrared take the photograph
As head, the submounts are provided with rotating seat, the gyroscope rotary body, and the gyro are provided with above the rotating seat
Instrument rotary body is connected as a single entity with the rotating seat, is provided with rotary inductor in the rotating shaft of the gyroscope rotary body, described turn
Distance measurement instrument is installed at the top of axle, the electro-magnetic shielding cover is provided with the outside of the gyroscope rotary body.
In said structure, Remote end can connect the controller, the detection to gyroscope by the communication module
Data are collected, and control gyroscope to move, and the aircraft can drive gyroscope in the unapproachable tunnel of human body or rock
DATA REASONING is carried out in hole, the gyroscope rotary body drives the distance measurement instrument to rotate together with, makes the distance when rotating
Survey meter carries out continual measurement, and measured position is passed through into institute in real time to the cross section of tunnel or grotto diverse location
State communication module and be together sent to Remote end, while Remote end can check tunnel or rock by the infrared camera
Situation in hole.
In order to further improve the use function of high accuracy gyroscope instrument, the aircraft is propeller, with the controller
Electrical connection.
In order to further improve the use function of high accuracy gyroscope instrument, the locating module is d GPS locating module or the Big Dipper
Locating module.
In order to further improve the use function of high accuracy gyroscope instrument, the communication module be WiFi wireless signals module or
Bluetooth module.
In order to further improve the use function of high accuracy gyroscope instrument, the infrared camera is arranged on by link tilt
The front of chassis, and the infrared camera electrically connects with the controller.
In order to further improve the use function of high accuracy gyroscope instrument, the rotating seat is connected with the base by bearing
Connect.
In order to further improve the use function of high accuracy gyroscope instrument, the distance measurement instrument is infrared detector or laser
Detector, and the electro-magnetic shielding cover is stretched out on the head of the distance measurement instrument, and electrically connected with the controller.
In order to further improve the use function of high accuracy gyroscope instrument, the electro-magnetic shielding cover is spherical metal cap.
Beneficial effect is：The electro-magnetic shielding cover can isolate to the electromagnetic signal of surrounding, improve DATA REASONING
The degree of accuracy, while the data of measurement and position can be sent to Remote end in real time, alternative manual measurement human body without
The tunnel and grotto that method enters.
Brief description of the drawings
Fig. 1 is a kind of space diagram of Surveying Engineering high accuracy gyroscope instrument described in the utility model.
Fig. 2 is a kind of controller architecture block diagram of Surveying Engineering high accuracy gyroscope instrument described in the utility model.
Description of reference numerals is as follows：
1st, aircraft；2nd, base；3rd, rotating seat；4th, electro-magnetic shielding cover；5th, distance measurement instrument；6th, gyroscope rotary body；7、
Rotating shaft；8th, rotary inductor；9th, infrared camera；10th, locating module；11st, control module；12nd, communication module；13rd, controller.
Embodiment
The utility model is described in further detail below in conjunction with the accompanying drawings：As Figure 1-Figure 2, a kind of Surveying Engineering is with high-precision
Spend gyroscope, including base 2, electro-magnetic shielding cover 4 and gyroscope rotary body 6, the bottom of base 2 is provided with aircraft 1, in base 2
Portion is provided with controller 13, and controller 13 is used to control gyroscope to run, and control module 11, positioning mould are provided with controller 13
Block 10 and communication module 12, locating module 10 are used to position gyroscope, are easy to Remote end to check gyroscope position,
Base 2 is above provided with infrared camera 9, and base 2 is installed above rotating seat 3, and rotating seat 3 is used to drive electro-magnetic shielding cover 4
Rotate together with, rotating seat 3 is provided with gyroscope rotary body 6 above, and gyroscope rotary body 6 is connected as a single entity with rotating seat 3, gyro
Rotary inductor 8 is installed, rotary inductor 8 is used for the rotary speed for detecting gyroscope, rotating shaft 7 in the rotating shaft 7 of instrument rotary body 6
Top is provided with distance measurement instrument 5, and the outside of gyroscope rotary body 6 is provided with electro-magnetic shielding cover 4, electro-magnetic shielding cover 4 be used for every
From the electromagnetic signal of surrounding, prevent from influenceing the rotation of gyroscope rotary body 6.
In said structure, Remote end can connect controller 13, the detection data to gyroscope by communication module 12
It is collected, and controls gyroscope to move, aircraft 1 can drives gyroscope to be carried out in the unapproachable tunnel of human body or grotto
DATA REASONING, drive distance measurement instrument 5 to rotate together with when gyroscope rotary body 6 rotates, make distance measurement instrument 5 to tunnel or grotto
The cross section of diverse location carries out continual measurement, and measured position is together sent to by communication module 12 in real time
Remote end, while the situation that Remote end can be checked in tunnel or grotto by infrared camera 9.
In order to further improve the use function of high accuracy gyroscope instrument, aircraft 1 is propeller, is electrically connected with controller 13
Connect, locating module 10 is d GPS locating module or Big Dipper locating module, and communication module 12 is WiFi wireless signals module or bluetooth mould
Block, infrared camera 9 is arranged on before base 2 by link tilt, and infrared camera 9 electrically connects with controller 13, rotation
Seat 3 is connected with base 2 by bearing, and distance measurement instrument 5 is infrared detector or laser detector, and the head of distance measurement instrument 5
Electro-magnetic shielding cover 4 is stretched out in portion, and is electrically connected with controller 13, and electro-magnetic shielding cover 4 is spherical metal cap.
General principle, principal character and advantage of the present utility model has been shown and described above.The technical staff of the industry
It should be appreciated that the utility model is not restricted to the described embodiments, the simply explanation described in above-described embodiment and specification is originally
The principle of utility model, on the premise of the spirit and scope of the utility model is not departed from, the utility model also has various change
And improvement, these changes and improvements are both fallen within claimed the scope of the utility model.The utility model requires protection scope
Defined by appended claims and its effect thing.
Claims (8)
- A kind of 1. Surveying Engineering high accuracy gyroscope instrument, it is characterised in that：Rotated including base, electro-magnetic shielding cover and gyroscope Body, the base bottom are provided with aircraft, and the chassis interior is provided with controller, control mould is provided with the controller Block, locating module and communication module, the front of chassis are provided with infrared camera, and the submounts are provided with rotating seat, The gyroscope rotary body is provided with above the rotating seat, and the gyroscope rotary body is connected as a single entity with the rotating seat, Rotary inductor is installed in the rotating shaft of the gyroscope rotary body, distance measurement instrument, the top are installed at the top of the rotating shaft The electro-magnetic shielding cover is provided with the outside of spiral shell instrument rotary body.
- A kind of 2. Surveying Engineering high accuracy gyroscope instrument according to claim 1, it is characterised in that：The aircraft is spiral shell Oar is revolved, is electrically connected with the controller.
- A kind of 3. Surveying Engineering high accuracy gyroscope instrument according to claim 1, it is characterised in that：The locating module is D GPS locating module or Big Dipper locating module.
- A kind of 4. Surveying Engineering high accuracy gyroscope instrument according to claim 1, it is characterised in that：The communication module is WiFi wireless signals module or bluetooth module.
- A kind of 5. Surveying Engineering high accuracy gyroscope instrument according to claim 1, it is characterised in that：The infrared camera The front of chassis is arranged on by link tilt, and the infrared camera electrically connects with the controller.
- A kind of 6. Surveying Engineering high accuracy gyroscope instrument according to claim 1, it is characterised in that：The rotating seat and institute Base is stated to connect by bearing.
- A kind of 7. Surveying Engineering high accuracy gyroscope instrument according to claim 1, it is characterised in that：The distance measurement instrument For infrared detector or laser detector, and the electro-magnetic shielding cover is stretched out on the head of the distance measurement instrument, and with the control Device electrical connection processed.
- A kind of 8. Surveying Engineering high accuracy gyroscope instrument according to claim 1, it is characterised in that：The electro-magnetic shielding cover For spherical metal cap.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721195480.7U CN207113890U (en) | 2017-09-19 | 2017-09-19 | A kind of Surveying Engineering high accuracy gyroscope instrument |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721195480.7U CN207113890U (en) | 2017-09-19 | 2017-09-19 | A kind of Surveying Engineering high accuracy gyroscope instrument |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207113890U true CN207113890U (en) | 2018-03-16 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721195480.7U Expired - Fee Related CN207113890U (en) | 2017-09-19 | 2017-09-19 | A kind of Surveying Engineering high accuracy gyroscope instrument |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207113890U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110440117A (en) * | 2019-08-24 | 2019-11-12 | 高平 | A kind of construction engineering cost field surveys device based on BIM technology |
-
2017
- 2017-09-19 CN CN201721195480.7U patent/CN207113890U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110440117A (en) * | 2019-08-24 | 2019-11-12 | 高平 | A kind of construction engineering cost field surveys device based on BIM technology |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180316 Termination date: 20210919 |