CN108267091A - A kind of fixed exploratory heading depth measurement aircraft - Google Patents
A kind of fixed exploratory heading depth measurement aircraft Download PDFInfo
- Publication number
- CN108267091A CN108267091A CN201611261115.1A CN201611261115A CN108267091A CN 108267091 A CN108267091 A CN 108267091A CN 201611261115 A CN201611261115 A CN 201611261115A CN 108267091 A CN108267091 A CN 108267091A
- Authority
- CN
- China
- Prior art keywords
- aircraft
- fixed
- exploratory heading
- depth measurement
- controller
- 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.)
- Pending
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B11/00—Measuring arrangements characterised by the use of optical techniques
- G01B11/22—Measuring arrangements characterised by the use of optical techniques for measuring depth
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B15/00—Measuring arrangements characterised by the use of electromagnetic waves or particle radiation, e.g. by the use of microwaves, X-rays, gamma rays or electrons
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B17/00—Measuring arrangements characterised by the use of infrasonic, sonic or ultrasonic vibrations
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Length Measuring Devices With Unspecified Measuring Means (AREA)
Abstract
The present invention relates to a kind of fixed exploratory heading depth measurement aircraft, including fixed exploratory heading sounding gear, aircraft, controller of aircraft, operation hole；The fixed exploratory heading sounding gear cooperation fixed setting is on board the aircraft；The controller of aircraft cooperation is fixedly mounted on board the aircraft；The operation hole is located on aircraft, the cooperation fixed exploratory heading sounding gear setting；The depth that the fixed exploratory heading sounding gear passes through the operation hole measurement exploratory heading；The sounding gear is non-contact type distance measuring apparatus；The depth measurement controller is computer control.The depth of exploratory heading can be measured, movement is quickly, conveniently.
Description
Technical field
The present invention relates to electronics and machinery equipment field, especially a kind of fixed exploratory heading depth measurement aircraft.
Background technology
In some constructions, many exploratory headings are made, but exploratory heading backfill does not often backfill not in time, even；Existing management because
Element, economic factor also have certain relationship with lacking exploratory heading backfill equipment.
When carrying out exploratory heading backfill, after obtaining the diameter of exploratory heading, depth, can be calculated according to the diameter of exploratory heading, depth
The volume of exploratory heading can further calculate the volume of material that exploratory heading backfill needs.During construction, the depth of different exploratory headings has
Difference in order to obtain preferable backfill effect, calculates the volume of material that backfill uses, it is necessary to measure the depth of exploratory heading.
When carrying out exploratory heading depth measurement work, if there is a kind of exploratory heading depth measurement aircraft, it will be able to rapidly measure exploratory heading
Depth, movement quickly, conveniently, reduce road and occupy.
Invention content
Technical problem：
In view of the defects existing in the prior art, the present invention proposes a kind of fixed exploratory heading depth measurement aircraft, can measure
The depth of exploratory heading, movement is quickly, conveniently.
Technical solution：
To achieve the above object, the present invention proposes a kind of fixed exploratory heading depth measurement aircraft,
Including fixed exploratory heading sounding gear, aircraft, controller of aircraft, operation hole；
The fixed exploratory heading sounding gear cooperation fixed setting is on board the aircraft；
The controller of aircraft cooperation is fixedly mounted on board the aircraft；
The operation hole is located on aircraft, the cooperation fixed exploratory heading sounding gear setting；The fixed exploratory heading
The depth that sounding gear passes through the operation hole measurement exploratory heading；
The controller of aircraft is fixedly connected formula exploratory heading sounding gear；
The fixed exploratory heading sounding gear is used to measure the depth of exploratory heading；
The controller of aircraft is computer control；
The fixed exploratory heading sounding gear is used for after aircraft is stayed in above exploratory heading, measures exploratory heading；
The fixed exploratory heading sounding gear includes depth measurement stent, detection hole, sounding gear, depth measurement controller；
The depth measurement stent includes bottom surface；
In the bottom surface of the depth measurement stent, the position of the corresponding sounding gear detection direction is equipped with the detection
Hole enables the sounding gear to detect the exploratory heading below the depth measurement stent by the detection hole；
The sounding gear cooperation is fixed on the depth measurement stent；
The depth measurement controller is fixed with the depth measurement support assorted；
The depth measurement controller is computer control；
The depth measurement controller is connected with the controller of aircraft；
The depth measurement controller is connected with peripheral control unit and/or power supply；
The depth measurement controller is connected with the sounding gear；
The sounding gear is non-contact type distance measuring apparatus.
Further, the fixed exploratory heading depth measurement aircraft further includes positioning device；
The positioning device cooperation fixed setting is on board the aircraft；
The controller of aircraft mating connection positioning device.
Further, the positioning device is the combination of satellite positioning device, inertial positioning device, base station location device.
Further, the sounding gear is rangefinder.
Further, the rangefinder is ultrasonic range finder or laser range finder or infrared range-measurement system or electromagnetic distance measurement
Instrument.
Further, the sounding gear by communication line or analog signal or pulse signal to external transmission measurement knot
Fruit.
Further, the depth measurement controller shares a controller with the controller of aircraft.
Further, the fixed exploratory heading depth measurement aircraft, further includes monitor camera；The fixed exploratory heading is surveyed
The monitor camera of cooperation installation monitoring search coverage on deep aircraft；The monitor camera mating connection monitor；It is described
Monitor is included positioned at the monitor of driver's cabin and/or the monitor positioned at vehicle-mounted manipulation position and/or remote controler and/or long-range prison
Visual organ and/or mobile phone.
Technique effect：
Fixed exploratory heading depth measurement aircraft proposed by the present invention provides a kind of fixed exploratory heading depth measurement aircraft, can
The depth of exploratory heading is measured, movement is quickly, conveniently.
Description of the drawings
Fig. 1 is a kind of structure diagram of embodiment of the fixed exploratory heading sounding gear of the present invention：
151. depth measurement stents, 152. detection holes, 153. rangefinders, 154. depth measurement controllers, 155. connecting lines.
Fig. 2 is a kind of structure diagram of embodiment of the fixed exploratory heading depth measurement aircraft of the present invention：
31. aircraft, 32. fixed exploratory heading sounding gears, 34. connecting lines, 35. controller of aircraft, 36. operation holes.
Fig. 3 is the structure diagram of another embodiment of the fixed exploratory heading depth measurement aircraft of the present invention：
31. aircraft, 32. fixed exploratory heading sounding gears, 33. positioning devices, 34. connecting lines, 35. flying vehicles controls
Device, 36. operation holes.
Specific embodiment
In order to make the purpose , technical scheme and advantage of the present invention be clearer, with reference to the accompanying drawings and embodiments, it is right
The present invention is described in further detail.It should be appreciated that the specific embodiments described herein are merely illustrative of the present invention,
It is not intended to limit the present invention.
Implement use-case one
As shown in Figure 1, being a kind of a kind of structure diagram of embodiment of fixed exploratory heading sounding gear of the present invention, wrap
Include depth measurement stent 151, detection hole 152, rangefinder 153, depth measurement controller 154, connecting line 155.
The depth measurement stent 151 includes bottom surface, for fixing the other component of the movable exploratory heading sounding gear；
In the bottom surface of the depth measurement stent 151, the position of the corresponding sounding gear detection direction is equipped with the inspection
Gaging hole 152 enables the rangefinder 153 to detect the exploratory heading of 151 lower section of depth measurement stent by the detection hole 152；
The edge of the detection hole 152 be it is closed or open, it is preferably closed；
The cooperation of rangefinder 153 is fixed on the depth measurement stent 151；
On the fixed depth measurement stent 151 of the cooperation of depth measurement controller 154；
The depth measurement controller 154 is computer control, is the prior art；
The connecting line 155 is the total of the circuit of each component and external equipment inside the movable exploratory heading sounding gear of connection
With；
The depth measurement controller 154 is connected by connecting line 155 and peripheral control unit and/or power supply；
The depth measurement controller 154 is connected by the connecting line 155 and the rangefinder 153.
The sounding gear includes rangefinder 153；The rangefinder 153 includes ultrasonic range finder 153 or laser ranging
Instrument 153 or one of infrared range-measurement system 153 or electromagnetic distance measuring instrument 153, preferably laser range finder 153.
The rangefinder 153 is by communication line or analog signal to external transmission measurement as a result, preferably through simulation
Signal is to external transmission measurement result；
Depth measurement controller 154 receives the measurement result that rangefinder 153 transmits.
Depth measurement controller 154 is by communication line or analog signal to external transmission measurement result.
The means of power that all electrical equipments are connected by depth measurement controller 154；The supply unit is generator
And/or storage battery power supply system and/or generator combine electric power system with accumulator；Preferably storage battery power supply system.
In use, laser range finder 153 measures distance, subtracts laser range finder 153 apart from ground perpendicular to exploratory heading direction
The distance in face obtains the depth of exploratory heading.
Implement use-case two
As shown in Fig. 2, be a kind of a kind of structure diagram of embodiment of fixed exploratory heading depth measurement aircraft of the present invention,
Including aircraft 31, fixed exploratory heading sounding gear 32, connecting line 34, controller of aircraft 35, operation hole 36.
The fixed exploratory heading sounding gear 32 is fixed exploratory heading sounding gear 32 of the present invention or other spies
Hole depth measurement measuring device 32；Preferably implement the fixed exploratory heading sounding gear 32 described in use-case one；
The fixed exploratory heading sounding gear 32 is used to measure the depth of exploratory heading.
The fixed cooperation of exploratory heading sounding gear 32 is fixed on aircraft 31；
The cooperation of controller of aircraft 35 is fixedly mounted on aircraft 31；
The depth measurement controller 154 passes through the connecting line 34 and/or the connecting line with the controller of aircraft 35
109 are connected；
The cooperation of connecting line 34 is fixedly mounted on aircraft 31；
The operation hole 36 is located on aircraft 31, and the fixed exploratory heading sounding gear 32 is coordinated to set；The fixation
Formula exploratory heading sounding gear 32 measures exploratory heading by the operation hole 36；
The controller of aircraft 35 is fixedly connected formula exploratory heading sounding gear 32 by connecting line 34；
The fixed exploratory heading sounding gear 32 is used for after aircraft 31 is stayed in above exploratory heading, measures exploratory heading；
The controller of aircraft 35 is computer control；
The connecting line 34 is the computer control system connecting line being used cooperatively with controller of aircraft 35；
Optionally, the depth measurement controller 154 shares a controller with the controller of aircraft, it is preferred that described
Mersure Controler shares a controller with the controller of aircraft.
Optionally, the monitor camera for monitoring search coverage is installed in cooperation on the fixed exploratory heading depth measurement aircraft；Institute
State monitor camera mating connection monitor；The monitor is included positioned at the monitor of driver's cabin and/or positioned at vehicle-mounted manipulation
The monitor and/or remote controler and/or remote monitor and/or mobile phone of position.Preferably, monitor camera, the monitoring are installed
Device is the monitor positioned at driver's cabin.Optionally, during the work time, the image of record monitor camera shooting.
Implement use-case three
As shown in figure 3, it is a kind of structural representation of another embodiment of fixed exploratory heading depth measurement aircraft of the present invention
Figure, including aircraft 31, fixed exploratory heading sounding gear 32, positioning device 33, connecting line 34, controller of aircraft 35, operation
Hole 36.
Implement use-case three and be with implementing the difference of use-case two, implement use-case three and increase positioning device 33.
The cooperation of positioning device 33 is fixed on aircraft 31；
The controller of aircraft 35 passes through 34 mating connection positioning device 33 of connecting line.
The positioning device 33 is used for determining the position of aircraft.
Optionally, the positioning device 33 is the combination of satellite positioning device, inertial positioning device, base station location device,
Preferably, the positioning device 33 is to combine the double source positioning device of satellite positioning device and inertial positioning device.
The present invention provides a kind of fixed exploratory heading depth measurement aircraft, can measure the depth of exploratory heading, mobile quick, side
Just.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all essences in the present invention
All any modification, equivalent and improvement made within refreshing and principle etc., should all be included in the protection scope of the present invention.
Claims (8)
1. a kind of fixed exploratory heading depth measurement aircraft, it is characterised in that：Including fixed exploratory heading sounding gear, aircraft, flight
Device controller, operation hole；
The fixed exploratory heading sounding gear cooperation fixed setting is on board the aircraft；
The controller of aircraft cooperation is fixedly mounted on board the aircraft；
The operation hole is located on aircraft, the cooperation fixed exploratory heading sounding gear setting；The fixed exploratory heading depth measurement
The depth that device passes through the operation hole measurement exploratory heading；
The controller of aircraft is fixedly connected formula exploratory heading sounding gear；
The fixed exploratory heading sounding gear is used to measure the depth of exploratory heading；
The controller of aircraft is computer control；
The fixed exploratory heading sounding gear is used for after aircraft is stayed in above exploratory heading, measures exploratory heading；
The fixed exploratory heading sounding gear includes depth measurement stent, detection hole, sounding gear, depth measurement controller；
The depth measurement stent includes bottom surface；
In the bottom surface of the depth measurement stent, the position of the corresponding sounding gear detection direction is equipped with the detection hole, makes
The sounding gear can detect the exploratory heading below the depth measurement stent by the detection hole；
The sounding gear cooperation is fixed on the depth measurement stent；
The depth measurement controller is fixed with the depth measurement support assorted；
The depth measurement controller is computer control；
The depth measurement controller is connected with the controller of aircraft；
The depth measurement controller is connected with peripheral control unit and/or power supply；
The depth measurement controller is connected with the sounding gear；
The sounding gear is non-contact type distance measuring apparatus.
2. fixed exploratory heading depth measurement aircraft according to claim 1, it is characterised in that：Further include positioning device；
The positioning device cooperation fixed setting is on board the aircraft；
The controller of aircraft mating connection positioning device.
3. fixed exploratory heading depth measurement aircraft according to claim 2, it is characterised in that：The positioning device is satellite
The combination of position device, inertial positioning device, base station location device.
4. the fixed exploratory heading depth measurement aircraft according to one of claim 1-3, it is characterised in that：The sounding gear is
Rangefinder.
5. fixed exploratory heading depth measurement aircraft according to claim 4, it is characterised in that：The rangefinder is ultrasound
Distance meter or laser range finder or infrared range-measurement system or electromagnetic distance measuring instrument.
6. the fixed exploratory heading depth measurement aircraft according to one of claim 1-3, it is characterised in that：By communication line or
Analog signal is to external transmission measurement result.
7. the fixed exploratory heading depth measurement aircraft according to one of claim 1-3, it is characterised in that：The depth measurement controller
A controller is shared with the controller of aircraft.
8. fixed exploratory heading depth measurement aircraft according to claim 1, it is characterised in that：Further include monitor camera；Institute
State the monitor camera of cooperation installation monitoring search coverage on fixed exploratory heading depth measurement aircraft；The monitor camera cooperation connects
Connect monitor；The monitor is included positioned at the monitor of driver's cabin and/or the monitor positioned at vehicle-mounted manipulation position and/or remote control
Device and/or remote monitor and/or mobile phone.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611261115.1A CN108267091A (en) | 2016-12-30 | 2016-12-30 | A kind of fixed exploratory heading depth measurement aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611261115.1A CN108267091A (en) | 2016-12-30 | 2016-12-30 | A kind of fixed exploratory heading depth measurement aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108267091A true CN108267091A (en) | 2018-07-10 |
Family
ID=62754897
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611261115.1A Pending CN108267091A (en) | 2016-12-30 | 2016-12-30 | A kind of fixed exploratory heading depth measurement aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108267091A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101776434A (en) * | 2010-03-10 | 2010-07-14 | 南开大学 | Method and device for measuring small blind hole based on tunnel current feedback collimation |
| CN202114713U (en) * | 2011-05-31 | 2012-01-18 | 博世电动工具（中国）有限公司 | Electric tool with non-contact distance measurement device |
| CN103234486A (en) * | 2013-03-28 | 2013-08-07 | 东华大学 | Non-contact measuring equipment and non-contact measuring method of inner hole straightness |
| CN103429395A (en) * | 2011-03-23 | 2013-12-04 | 赫克斯冈技术中心 | Working tool positioning system |
| CN205277403U (en) * | 2016-01-22 | 2016-06-01 | 重庆三峡学院 | Drilling depth measurement device |
-
2016
- 2016-12-30 CN CN201611261115.1A patent/CN108267091A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101776434A (en) * | 2010-03-10 | 2010-07-14 | 南开大学 | Method and device for measuring small blind hole based on tunnel current feedback collimation |
| CN103429395A (en) * | 2011-03-23 | 2013-12-04 | 赫克斯冈技术中心 | Working tool positioning system |
| CN202114713U (en) * | 2011-05-31 | 2012-01-18 | 博世电动工具（中国）有限公司 | Electric tool with non-contact distance measurement device |
| CN103234486A (en) * | 2013-03-28 | 2013-08-07 | 东华大学 | Non-contact measuring equipment and non-contact measuring method of inner hole straightness |
| CN205277403U (en) * | 2016-01-22 | 2016-06-01 | 重庆三峡学院 | Drilling depth measurement device |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN111288963B (en) | High-risk deformable body GNSS monitoring terminal non-contact throwing device and method | |
| AU2016102409A4 (en) | Local Positioning System for an Unmanned Aerial Vehicle | |
| EP2818958A3 (en) | Flying vehicle guiding system and flying vehicle guiding method | |
| CN109581365B (en) | Life detection system and method based on multi-rotor unmanned aerial vehicle | |
| EP3384309B1 (en) | Monitoring and/or logging a position of a tool within an elevator shaft | |
| US20150160006A1 (en) | Derivation of sea ice thickness using isostacy and upward looking sonar profiles | |
| CN105445729A (en) | Unmanned plane three-dimensional flight track precision detection method and system | |
| CN208367546U (en) | Skyscraper natural gas standpipe safety pre-warning system based on unmanned machine testing | |
| KR102112340B1 (en) | Near field drone detection and identifying device | |
| Hartmann et al. | Design of an embedded UWB hardware platform for navigation in GPS denied environments | |
| US20180122247A1 (en) | Integrated system to determine turbulent effects, in particular in aircrafts in flight | |
| CN111694001A (en) | Real-time distance measurement positioning system for unmanned aerial vehicle | |
| JP2017026411A5 (en) | ||
| CN105372650A (en) | Unmanned plane flight track precision detection method and device | |
| CN108267130A (en) | A kind of fixed exploratory heading depth measurement vehicle | |
| KR101406061B1 (en) | System for River Management | |
| CN112378352B (en) | Real-time remote online monitoring system for cargo displacement in railway transportation process | |
| CN108267091A (en) | A kind of fixed exploratory heading depth measurement aircraft | |
| RU2540982C1 (en) | Method of determining coordinates of targets (versions) and system therefor (versions) | |
| CN203259148U (en) | Measuring apparatus with built-in height measuring device | |
| CN104501770A (en) | Laser fuze height determining method without influence of missile attitudes | |
| CN208224499U (en) | The anticollision device, collision-prevention device of telemeasurement ship superelevation | |
| CN108267092A (en) | A kind of fixed exploratory heading sounding gear | |
| WO2014195812A1 (en) | Ground-based geo-referenced interferometric radar | |
| CN202362458U (en) | Dynamic parachute laser radar three-dimensional distance measuring system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180710 |
|
| WD01 | Invention patent application deemed withdrawn after publication |