CN206627455U - A kind of aircraft device applied to defects detection in pipeline - Google Patents
A kind of aircraft device applied to defects detection in pipeline Download PDFInfo
- Publication number
- CN206627455U CN206627455U CN201621276693.8U CN201621276693U CN206627455U CN 206627455 U CN206627455 U CN 206627455U CN 201621276693 U CN201621276693 U CN 201621276693U CN 206627455 U CN206627455 U CN 206627455U
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- China
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- aircraft
- interior
- fuselage
- propeller
- motor
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Abstract
The utility model discloses a kind of aircraft device applied to defects detection in pipeline.Including interior aircraft and outer aircraft, interior aircraft includes interior aircraft fuselage and the interior aircraft propeller with interior flying machine and interior aircraft motor, and outer aircraft includes outer aircraft fuselage and the outer aircraft propeller on outer aircraft fuselage and outer aircraft motor.Interior aircraft of the present utility model employs the arrangement of annular camera, can be directed to the different pipeline of diameter, adaptability is good, and can be used to detect complete inner-walls of duct simultaneously.
Description
Technical field
Detection field in pressure pipeline is the utility model is related to, especially a kind of device for being used for defects detection in pipeline,
For detecting pipeline internal flaw.
Background technology
Line clogging and corrosion are the common conditions during pressure pipeline use, have impact on the normal operation of pressure pipeline
And security.It is also more and more currently for the technology of pipe detection, including Magnetic Flux Leakage Inspecting, EDDY CURRENT, based on optical principle
Non-Destructive Testing, ultrasound detection, leak detection etc. based on detection ball.But the cost that they have is all too high, and
Detection speed is also very slow；The detector restricted application either having.
Utility model content
The purpose of this utility model is to overcome deficiency of the prior art, there is provided one kind is used for defects detection in pipeline
Device, can be applicable the detection of different inner diameters pipeline, riser tubing detection efficiency, exclude potential safety hazard.
In order to solve the above technical problems, technical scheme provided by the utility model is to include interior aircraft and outer aircraft：
Described interior aircraft includes interior aircraft fuselage and the interior aircraft propeller with interior flying machine
With interior aircraft motor；Four interior aircraft propellers are installed on interior aircraft fuselage, interior aircraft propeller respectively with respectively
From interior aircraft motor connection, by interior aircraft motor driven aircraft propeller rotate so that drive in aircraft it is aerial
Flight；The head end of interior aircraft fuselage is provided with for detecting objects in front with the interior flight ultrasonic sensor of avoidance, interior
Velocity sensor is installed inside aircraft fuselage, ring support is installed in the middle part of interior aircraft fuselage, ring support it is outer
Phase unit and annular light source are installed on side face.
Described outer aircraft includes outer aircraft fuselage and the outer vehicle spin on outer aircraft fuselage
Oar and outer aircraft motor；Four outer aircraft propellers are installed on outer aircraft fuselage, outer aircraft propeller respectively with
Respective outer aircraft motor connection, rotated by flight propeller outside outer aircraft motor driven and then drive outer aircraft aerial
Flight, the head end of outer aircraft fuselage is provided with outer aircraft ultrasonic sensor.
Described phase unit includes multiple cameras being mainly made up of video camera and light source, along ring support periphery on camera
The circle spacing in face uniformly installs；In each camera, video camera is radially installed outwardly, and the light source for illumination is arranged in
Video camera.
The camera insertion is arranged in ring support.
Compared with prior art, the beneficial effects of the utility model are：
Interior aircraft of the present utility model employs the arrangement of annular camera, can be directed to the different pipeline of diameter, no
Need have very strong adaptability, and can be used for same from the arrangement position and layout light source of new design camera under different internal diameters
When detect complete inner-walls of duct.
Brief description of the drawings
Fig. 1 is Flight Vehicle Structure schematic diagram in the utility model.
Fig. 2 is aircraft fuselage inner structure schematic diagram in the utility model.
Fig. 3 is the outer middle Flight Vehicle Structure schematic diagram of the utility model.
Fig. 4 is the outer aircraft fuselage inner structure schematic diagram of the utility model.
Fig. 5 is the utility model camera cross section structure schematic diagram.
In figure：1：Interior aircraft fuselage, 2/3/4/5：Interior aircraft propeller, 6/7/8/9：Interior flight motor, 10：It is interior
Aircraft ultrasonic sensor, 11：Video camera, 12：Light source, 15：Velocity sensor, 18：Ring support；19：Outer aircraft machine
Body, 20/21/22/23：Outer aircraft propeller, 24/25/26/27：Outer aircraft motor, 28：Outer aircraft battery, 32：Outside
Aircraft ultrasonic sensor, 35：Ring support outer wall, 36：Inner-walls of duct to be detected.
Embodiment
Further illustrated below in conjunction with embodiment shown in the drawings.
The utility model includes interior aircraft and outer aircraft：Interior aircraft is acquired to the pipeline of different inner diameters, is adopted
View data is sent to outer aircraft after collection, then high in the clouds is sent to through outer aircraft.
As depicted in figs. 1 and 2, interior aircraft include interior aircraft fuselage 1 and on interior aircraft fuselage 1 in
Aircraft propeller 2,3,4,5 and interior aircraft motor 6,7,8,9；Four interior aircraft spiral shells are installed on interior aircraft fuselage 1
Oar 2,3,4,5 is revolved, interior aircraft propeller 2,3,4,5 is connected with respective interior aircraft motor 6,7,8,9 respectively, by interior flight
In device motor driven flight propeller rotate so that drive in aircraft airflight；The head end installation of interior aircraft fuselage 1
Have for detecting objects in front with the interior aircraft ultrasonic sensor 10 of avoidance, speed is installed inside interior aircraft fuselage 1
Sensor 15, the middle part of interior aircraft fuselage 1 are provided with ring support 18, are provided with the outer peripheral face of ring support 18 for clapping
Take the photograph the phase unit of inner-walls of duct image.
As shown in Figure 3 and Figure 4, outer aircraft includes outer aircraft fuselage 19 and on outer aircraft fuselage 19
Outer aircraft propeller 20,21,22,23, outer aircraft motor 24,25,26,27 and outer flight battery 28；Outer aircraft fuselage
Four outer aircraft propellers 20,21,22,23 are installed on 19, outer aircraft propeller 20,21,22,23 respectively with it is respective
Outer aircraft motor 24,25,26,27 connects, and is rotated by aircraft propeller outside outer aircraft motor driven and then drives outer fly
Row device airflight；The head end of outer aircraft fuselage 19 is provided with for detecting objects in front with the outer aircraft ultrasound of avoidance
Wave sensor 32.
As shown in figure 5, phase unit includes multiple cameras being mainly made up of video camera 11 and light source 12, along annular on camera
The circle spacing of the outer peripheral face of support 18 uniformly installs；In each camera, video camera 11 is radially installed outwardly, for illuminating
Light source 12 be arranged in video camera 11, camera insertion is arranged in ring support 18.
Embodiment and its implementation process of the present utility model are as follows：
After inside and outside aircraft is opened, interior aircraft is put into pipeline to be detected, while the annular camera of interior aircraft
Group and light source group are all opened completely, and the phase unit enclosed by being arranged in ring support one is shot, and gathers the figure of pipe wall
Picture.The image of shooting is sent to outer aircraft by wireless radio-frequency, and outer aircraft uploads to the view data of reception outer
The high in the clouds in portion, high in the clouds the image received are further processed the result for obtaining defects detection.
In being flown using interior aircraft in pipeline and gathering image process, enable minimum camera and meet 360 without dead angle
Pipeline shooting.Specific implementation can be with external diameter 200mm pipeline, and camera perspective is π degree, ring support diameter 150mm, camera
Between radian be 30 degree, camera each second 30, pictures were shot.
Finally it should be noted that listed above is only a specific embodiment of the present utility model, not to this reality
Any formal limitation is done with new.Obviously, the utility model is not limited to above example, can also there is many variations.This
All deformations that the technical staff in field directly can export or associate from the utility model disclosure, are considered as
The scope of protection of the utility model.
Claims (3)
1. a kind of aircraft device applied to defects detection in pipeline, it is characterised in that including interior aircraft and outer aircraft：
Described interior aircraft includes interior aircraft fuselage (1) and the interior vehicle spin on interior flight fuselage (1)
Oar (2,3,4,5) and interior aircraft motor (6,7,8,9)；Four interior aircraft propellers are installed on interior aircraft fuselage (1)
(2,3,4,5), interior aircraft propeller (2,3,4,5) are connected with respective interior aircraft motor (6,7,8,9) respectively, are flown by interior
In row device motor driven aircraft propeller rotate so that drive in aircraft airflight；The head of interior aircraft fuselage (1)
End is provided with for detecting objects in front with the interior flight ultrasonic sensor (10) of avoidance, and interior aircraft fuselage (1) is internal to pacify
Equipped with velocity sensor (15), ring support (18), the periphery of ring support (18) are installed in the middle part of interior aircraft fuselage (1)
Phase unit and annular light source are installed on face；
Described outer aircraft includes outer aircraft fuselage (19) and the outer aircraft on outer aircraft fuselage (19)
Propeller (20,21,22,23) and outer aircraft motor (24,25,26,27)；It is provided with outer aircraft fuselage (19) outside four
Aircraft propeller (20,21,22,23), outer aircraft propeller (20,21,22,23) respectively with respective outer aircraft motor
(24,25,26,27) connect, rotated by flight propeller outside outer aircraft motor driven and then drive outer aircraft airflight,
The head end of outer aircraft fuselage (19) is provided with outer aircraft ultrasonic sensor (32)；
Inside and outside aircraft is equipped with wireless radio transmission equipment, outer aircraft built with less radio-frequency receiving device, interior aircraft and
Wireless radio frequency mode communicates between outer aircraft.
A kind of 2. aircraft device applied to defects detection in pipeline according to claim 1, it is characterised in that：It is described
Phase unit include multiple cameras being mainly made up of video camera (11) and light source (12), along ring support (18) periphery on camera
The circle spacing in face uniformly installs；In each camera, video camera (11) is radially installed outwardly, the light source for illumination
(12) it is arranged in video camera (11).
A kind of 3. aircraft device applied to defects detection in pipeline according to claim 2, it is characterised in that：It is described
Camera insertion is arranged in ring support (18).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621276693.8U CN206627455U (en) | 2016-11-23 | 2016-11-23 | A kind of aircraft device applied to defects detection in pipeline |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621276693.8U CN206627455U (en) | 2016-11-23 | 2016-11-23 | A kind of aircraft device applied to defects detection in pipeline |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206627455U true CN206627455U (en) | 2017-11-10 |
Family
ID=60212840
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621276693.8U Expired - Fee Related CN206627455U (en) | 2016-11-23 | 2016-11-23 | A kind of aircraft device applied to defects detection in pipeline |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206627455U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106442570A (en) * | 2016-11-23 | 2017-02-22 | 中国计量大学 | Internal pipeline defect detecting device, detecting method and start setting method of cameras |
-
2016
- 2016-11-23 CN CN201621276693.8U patent/CN206627455U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106442570A (en) * | 2016-11-23 | 2017-02-22 | 中国计量大学 | Internal pipeline defect detecting device, detecting method and start setting method of cameras |
| CN106442570B (en) * | 2016-11-23 | 2023-08-22 | 中国计量大学 | Device and method for detecting defects in pipeline and method for opening and setting camera |
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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 |
Granted publication date: 20171110 Termination date: 20211123 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |