CN205002735U - Engineering detects aircraft with panorama shooting and measurement function - Google Patents
Engineering detects aircraft with panorama shooting and measurement function Download PDFInfo
- Publication number
- CN205002735U CN205002735U CN201520728148.7U CN201520728148U CN205002735U CN 205002735 U CN205002735 U CN 205002735U CN 201520728148 U CN201520728148 U CN 201520728148U CN 205002735 U CN205002735 U CN 205002735U
- Authority
- CN
- China
- Prior art keywords
- aircraft
- camera
- measurement function
- shot
- pan
- 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.)
- Expired - Fee Related
Links
Landscapes
- Arrangements For Transmission Of Measured Signals (AREA)
Abstract
The utility model discloses an engineering detects aircraft with panorama shooting and measurement function, include aircraft, wireless remote control ware and install shooting system, measurement system, data acquisition and analytic system, the data wireless transmission system on the aircraft, shooting system, measurement system all are connected with data acquisition and analytic system, data acquisition and analytic system and data wireless transmission system are connected, data wireless transmission system and wireless remote control ware wireless connection. The utility model discloses a characteristics are: simple structure, with low costs, the detection is convenient, work efficiency is high, have can 360 degrees shootings of no dead angle, engineering survey and posture adjustment the function, solved engineering detection achievement in special position be difficult to survey and the measuring problem.
Description
Technical field
The utility model relates to engineering detecting field, is specifically related to a kind of engineering detecting aircraft with pan-shot and measurement function.
Background technology
At present, the many use specialties of engineering detecting industry detect vehicle, set up framing scaffold or lifting operation to detect bridge, the presentation quality of the building such as tall and slender structure and large-span steel and dimensional measurement, said method is time-consuming, both slow job schedule had been dragged, produce again larger economic cost, at the bottom of large-scale wide cut bridge, the special constructions such as large-span steel truss then cannot adopt above-mentioned traditional method to detect, and some privileged sites is difficult to observation and measures in engineering detecting work, therefore need now a kind ofly can break through traditional checkout equipment to solve the problem.
Utility model content
The purpose of this utility model is to overcome above-mentioned not enough problem, provides a kind of engineering detecting aircraft with pan-shot and measurement function.
The technical scheme that the utility model is adopted for achieving the above object is: a kind of engineering detecting aircraft with pan-shot and measurement function, comprise aircraft, Digiplex and be arranged on carry-on camera system, measuring system, data collection and transmission, data radio transmission system, described camera system, measuring system are all connected with data collection and transmission, described data collection and transmission is connected with data radio transmission system, described data radio transmission system and Digiplex wireless connections.
Described camera system comprises camera, 360 degree of runing rests, described camera is connected with aircraft by 360 degree of runing rests, described measuring system comprises attitude sensor, laser range finder, angel measuring instrument, described attitude sensor is installed on board the aircraft, and described laser range finder and angel measuring instrument are installed in surface of camera head place.
Described aircraft comprises aircraft body, flight-control computer, support, rotor, motor, described flight-control computer to be arranged in aircraft body and with Digiplex wireless connections, described support one end is connected with aircraft body, the other end installs rotor, described rotor is connected with motor, described motor is connected with flight-control computer, described 360 degree of runing rests are arranged on aircraft body sidepiece, and described attitude sensor, data collection and transmission, data radio transmission system are installed in aircraft body.
Described aircraft body circumferentially evenly installs four described supports, four described supports are decussation, and each described support is all provided with rotor, and four rotors are positioned at sustained height plane, four described rotors are connected with motor, and the sense of rotation of adjacent rotor is contrary.
Described camera adopts integrated form camera.
Described camera system also comprises the illumination be arranged on camera.
Feature of the present utility model is: structure is simple, cost is low, it is convenient to detect, work efficiency is high, by arranging 360 degree of runing rests, camera is made to have the camera angle of vertical 180 degree, change the limitation that aircraft in the past can only be taken downwards, therefore can at the bottom of bridge, the position that facade body of wall etc. was difficult to observe in the past checks, and the measurement function had target object, can measure by concrete yardstick to target object from graphical analysis and laser measurement two angles, therefore the concrete size of fracture situation and target object Measurement accuracy can be carried out, attitude sensor is set up in aircraft, by the compensation to self attitude angle, external influence can be overcome to a certain extent, obtain measurement data more accurately.
Accompanying drawing explanation
Fig. 1 is planimetric map of the present utility model.
Fig. 2 is elevation drawing of the present utility model.
Wherein: 1, aircraft body 2, flight-control computer 3, attitude sensor 4, data collection and transmission 5, data radio transmission system 6, camera 7, illumination 8, laser range finder 9, angel measuring instrument 10,360 degree of runing rests 11, motor 12, rotor 13, support 14, Digiplexs.
Embodiment
As Fig. 1, shown in 2, the utility model is a kind of engineering detecting aircraft with pan-shot and measurement function, comprise aircraft, Digiplex 14, and be arranged on carry-on camera system, measuring system, data collection and transmission 4, data radio transmission system 5, described aircraft comprises aircraft body 1, flight-control computer 2, support 13, rotor 12, motor 11, described flight-control computer 2 to be arranged in aircraft body 1 and with Digiplex 14 wireless connections, described support 13 one end is connected with aircraft body 1, the other end installs rotor 12, described rotor 12 is connected with motor 11, described motor 11 is connected with flight-control computer 2, preferably, described aircraft body 1 circumferentially evenly installs four described supports 13, four described supports 13 are in decussation, each described support 13 is all provided with rotor 12, four rotors 12 are positioned at sustained height plane, four described rotors 12 connect respective motor 11, the sense of rotation of adjacent motor 11 is contrary, namely the sense of rotation of rotor 12 is contrary, to ensure stabilized flight, described camera system comprises camera 6, 360 degree of runing rests 10, described camera 6 is arranged on aircraft body 1 sidepiece by 360 degree of runing rests 10, described camera 6 adopts integrated form camera, when described camera 6 installs illumination 7 for insufficient light, described measuring system comprises attitude sensor 3, laser range finder 8, angel measuring instrument 9, described attitude sensor 3 is arranged in aircraft body 1, described laser range finder 8 and angel measuring instrument 9 are installed in camera 6 surface, described camera system, measuring system is all connected with data collection and transmission 4, described data collection and transmission 4 is connected with data radio transmission system 5, described data radio transmission system 5 and Digiplex 14 wireless connections, described data collection and transmission 4, data radio transmission system 5 is installed in aircraft body 1.
During work, first by Digiplex 14, aircraft is adjusted near detected face, adjust 360 degree of runing rests 10, make camera 6 and laser range finder 8, the surface of angel measuring instrument 9 is substantially parallel with tested surface, be fixed near institute's location puts by adjustment angel measuring instrument 9 laser spots that makes laser range finder discharge, during as measured crack, should ensure that laser spots is all arranged in both sides, crack, then the focal length of camera 6 is adjusted, take after imaging clearly, illumination 7 is opened when insufficient light, and the attitude sensor 3 simultaneously recorded now, the data information of laser range finder 8 and angel measuring instrument 9, obtain the distance in images between laser spots as calculated, and then obtain fracture width and region area.
The above; be only the utility model preferably embodiment; but protection domain of the present utility model is not limited thereto; anyly be familiar with those skilled in the art in the technical scope that the present invention discloses; be equal to according to the technical solution of the utility model and inventive concept thereof and replace or change, all should be encompassed within protection domain of the present utility model.
Claims (7)
1. one kind has the engineering detecting aircraft of pan-shot and measurement function, it is characterized in that: comprise aircraft, Digiplex (14) and be arranged on carry-on camera system, measuring system, data collection and transmission (4), data radio transmission system (5), described camera system, measuring system are all connected with data collection and transmission (4), described data collection and transmission (4) is connected with data radio transmission system (5), described data radio transmission system (5) and Digiplex (14) wireless connections.
2. there is the engineering detecting aircraft of pan-shot and measurement function as claimed in claim 1, it is characterized in that: described camera system comprises camera (6), 360 degree of runing rests (10), described camera (6) is connected with aircraft by 360 degree of runing rests (10), described measuring system comprises attitude sensor (3), laser range finder (8), angel measuring instrument (9), described attitude sensor (3) is installed on board the aircraft, and described laser range finder (8) and angel measuring instrument (9) are installed in camera (6) surface.
3. there is the engineering detecting aircraft of pan-shot and measurement function as claimed in claim 2, it is characterized in that: described aircraft comprises aircraft body (1), flight-control computer (2), support (13), rotor (12), motor (11), described flight-control computer (2) be arranged on aircraft body (1) upper and with Digiplex (14) wireless connections, described support (13) one end is connected with aircraft body (1), the other end installs rotor (12), described rotor (12) is connected with motor (11), described motor (11) is connected with flight-control computer (2), described 360 degree of runing rests (10) are arranged on aircraft body (1) sidepiece, described attitude sensor (3), data collection and transmission (4), data radio transmission system (5) is installed in aircraft body (1).
4. there is the engineering detecting aircraft of pan-shot and measurement function as claimed in claim 3, it is characterized in that: described aircraft body (1) circumferentially evenly installs four described supports (13), four described supports (13) are in decussation, each described support (13) is all provided with rotor (12), four rotors (12) are positioned at sustained height plane, four described rotors (12) are connected with motor (11), and the sense of rotation of adjacent rotor (12) is contrary.
5. the engineering detecting aircraft with pan-shot and measurement function as described in claim as arbitrary in claim 2-4, is characterized in that: described camera (6) adopts integrated form camera.
6. there is the engineering detecting aircraft of pan-shot and measurement function as claimed in claim 2 or claim 3, it is characterized in that: described camera system also comprises the illumination (7) be arranged on camera (6).
7. there is the engineering detecting aircraft of pan-shot and measurement function as claimed in claim 5, it is characterized in that: described camera system also comprises the illumination (7) be arranged on camera (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520728148.7U CN205002735U (en) | 2015-09-21 | 2015-09-21 | Engineering detects aircraft with panorama shooting and measurement function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520728148.7U CN205002735U (en) | 2015-09-21 | 2015-09-21 | Engineering detects aircraft with panorama shooting and measurement function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205002735U true CN205002735U (en) | 2016-01-27 |
Family
ID=55159620
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520728148.7U Expired - Fee Related CN205002735U (en) | 2015-09-21 | 2015-09-21 | Engineering detects aircraft with panorama shooting and measurement function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205002735U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109631769A (en) * | 2018-12-20 | 2019-04-16 | 重庆迈高电梯有限公司 | A kind of elevator investigation method |
| CN113758451A (en) * | 2020-06-04 | 2021-12-07 | 拓荆科技股份有限公司 | Device and method for detecting relative position and parallel state in parallel plate reactor |
-
2015
- 2015-09-21 CN CN201520728148.7U patent/CN205002735U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109631769A (en) * | 2018-12-20 | 2019-04-16 | 重庆迈高电梯有限公司 | A kind of elevator investigation method |
| CN113758451A (en) * | 2020-06-04 | 2021-12-07 | 拓荆科技股份有限公司 | Device and method for detecting relative position and parallel state in parallel plate reactor |
| CN113758451B (en) * | 2020-06-04 | 2023-09-22 | 拓荆科技股份有限公司 | Device and method for detecting relative position and parallel state in parallel plate reactor |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN108106801B (en) | Bridge and tunnel disease non-contact detection system and detection method | |
| CN105698776B (en) | A kind of two dimension reference vehicular transfer device and its measurement method | |
| CN201757642U (en) | Remote deformation monitoring system based on digital photographing technology | |
| CN106197292B (en) | A kind of building displacement monitoring method | |
| CN102589523A (en) | Method and equipments for remotely monitoring displacement of building | |
| CN105865349B (en) | A kind of building displacement monitoring method | |
| US11774318B2 (en) | Force and inclination monitoring system with self-position recognition | |
| CN210486775U (en) | Portable deformation detection device | |
| CN105606129A (en) | Measurement and calibration method for assisting in mounting of airplane inertial navigation finished product assembly | |
| CN203824548U (en) | Bridge structure concrete surface observation area measuring instrument | |
| CN205002735U (en) | Engineering detects aircraft with panorama shooting and measurement function | |
| CN109387329A (en) | Small drone weight center of gravity measuring device and measuring method | |
| CN114993263A (en) | High accuracy building unmanned aerial vehicle survey and drawing system based on leveling point location | |
| CN205301201U (en) | Detection apparatus for beyond region of objective existence surface texture defect is built in construction | |
| CN205449052U (en) | Device for measuring building inclination angle by laser | |
| CN204999519U (en) | Two dimension tower crane squareness measurement device | |
| CN109000601A (en) | A kind of pylon offset dynamic observation system | |
| CN205858356U (en) | Attitude of shield machine controls the mounting structure of total powerstation support hanging basket | |
| CN202041184U (en) | Multi-parameter detection device for crane structure safety | |
| CN208721070U (en) | A kind of horizontal vertical measuring device of high level armored concrete wall | |
| CN208238780U (en) | A kind of detection device for high pier verticality | |
| CN205209423U (en) | Device of monitoring building vertical deformation seam deflection | |
| CN105606016A (en) | Space strain measurement apparatus based on triaxial inclination angle positioning and method thereof | |
| CN102620660A (en) | Ultra-remote detection method for cracks of buildings and structures | |
| CN205664834U (en) | Novel measuring prism |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| 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: 20160127 Termination date: 20170921 |