CN206683639U - Aeroplane photography instrument - Google Patents
Aeroplane photography instrument Download PDFInfo
- Publication number
- CN206683639U CN206683639U CN201720546999.9U CN201720546999U CN206683639U CN 206683639 U CN206683639 U CN 206683639U CN 201720546999 U CN201720546999 U CN 201720546999U CN 206683639 U CN206683639 U CN 206683639U
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- control platform
- casing
- side wall
- aeroplane photography
- adjustment hole
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Abstract
It the utility model is related to aerophotogrammetry technical field, a kind of more particularly to aeroplane photography instrument, including casing, control platform, GPS is placed with the casing, the mainboard electrically connected with the GPS is provided with the control platform, the control platform is provided with the display screen and console electrically connected with the mainboard；The side wall of the control platform is provided with the interface for being used for electrically connecting with navigator's screen, and the interface electrically connects with mainboard.The utility model is by the way that the navigator being placed in aircraft cockpit screen is connected with USB interface, so that pilot can be with real-time judge flight reappearance and camera exposure situation, improve the precision in aerial surveying camera use, it has been reduced or avoided simultaneously and has mended winged situation, and reduce the laying quantity of ground photo control point, cost is greatly reduced, pilot can carry out contrast reference by the voyage conditions and aerial survey route of aircraft, reduce flight difficulty.
Description
Technical field
It the utility model is related to aerophotogrammetry technical field, more particularly to a kind of aeroplane photography instrument.
Background technology
Aerophotogrammetry is that the continuous intake photo in ground, combined ground control point are surveyed with aerophotographic apparatus aboard
Amount, adjust paint with the step such as stereo mapping, draw out the operation of topographic map.Because China's topographic structure is complicated, topography variation is fast, passes
The e measurement technology of system can not meet the requirement of extreme terrain measurement, therefore can effectively solve this by air photo technique
A little problems.In Fundamental Geographic Information System collection, photogrammetric Aviation Digital is one of maximally effective means.
Current aeroplane photography instrument is based on several cameras, by reinforcing, accurate unit calibration, platform splicing, precision surface plate
Calibration, outfit measurement type GPS, aeroplane photography management computer, ground post processing computer and substantial amounts of aerial software,
Software on ground, small light, at a high speed high-speed synchronous exposure, the core technology such as storage are broken through, realize amateur measurement camera and exist
Applied in aerial survey, greatly reduce aerial survey cost.
But the boat in reality is taken the photograph in the course of work, built in the airborne alignment system on aircraft and aerial surveying camera GPS without
Method sync bit information, pilot can not understand practical flight positional information in real time during practical flight, result in flight
There is larger error in track, the course line of height and design and height, it is possible to cause course line degree of overlapping and photographic resolving power
The situation of design requirement can not be met.
Above-mentioned consideration is based on, the utility model devises a kind of aeroplane photography instrument, makes pilot can be with real-time judge
Flight reappearance and camera exposure situation, the precision in the aerial surveying camera use is improved, winged situation is mended so as to be reduced or avoided,
And reduce the laying quantity of ground photo control point.
Utility model content
The purpose of this utility model is overcome the deficiencies in the prior art, adapts to real needs, there is provided a kind of aeroplane photography
Instrument.
In order to realize the purpose of this utility model, the technical solution adopted in the utility model is：
The utility model discloses a kind of aeroplane photography instrument, including casing, control platform, GPS is placed with the casing
Receiver, is provided with mainboard electrically connect with the GPS in the control platform, the control platform provided with it is described
The display screen and console of mainboard electrical connection；The side wall of the control platform, which is provided with, to be used to connect with what navigator's screen electrically connected
Mouthful, the interface electrically connects with mainboard.
The interface is USB interface.
The control platform is arranged above the casing, and one end of the control platform and one end of the casing are cut with scissors
Connect；The bottom of the control platform is provided with the supporting member for support and control platform with the casing top.
The end of the side wall of the control platform, which is provided with, is used for the through hole that pivot pin passes through, and the top both sides of the casing are provided with
Support base, the support base, which is provided with, is used for the axis hole that pivot pin passes through.
The side wall of the axis hole, which is provided with, is used for the spacing hole that gag lever post passes through.
The supporting member includes being arranged at the control platform bottom support bar be hinged with it, being arranged at the casing
The supporting table at top, the supporting table are provided with the width identical groove of the support bar, the side wall two of the supporting table
Side, which is provided with, is used for the screwed hole that fixing bolt passes through.
The side wall of supporting table one is provided with the governor motion for being used for adjusting the fixing bolt horizontal level, the regulation
Mechanism includes the first elongated adjustment hole of section, the second regulation in communication formed below of first adjustment hole
Hole, the cross-sectional width of second adjustment hole is identical with the external diameter of the screw rod of the fixing bolt, between described second adjustment hole etc.
Every array in the lower section of the first adjustment hole；In another side wall of the supporting table formed with alignd with second adjustment hole etc.
The spaced screwed hole being connected with fixing bolt end thread.
The beneficial effects of the utility model are：
1. the utility model is by the way that the navigator being placed in aircraft cockpit screen is connected with USB interface so that flight
Member can be improved the precision in aerial surveying camera use, be reduced or avoided simultaneously with real-time judge flight reappearance and camera exposure situation
Winged situation is mended, and reduces the laying quantity of ground photo control point, greatly reduces cost, pilot can pass through aircraft
Voyage conditions and aerial survey route carry out contrast reference, reduce flight difficulty；
2. the utility model is hinged by one end of control platform and casing, and by supporting member that the control is flat
Platform is supported, and the display screen in control platform can be made to enter line tilt, be easy to the survey crew in cabin to be observed.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model；
Fig. 2 is another viewing angle constructions schematic diagram of the present utility model；
Fig. 3 is the structural representation of supporting mechanism and governor motion in the utility model.
In figure, 1 casing, 2 control platforms, 3 navigator's screens, 4 interfaces, 5 supporting members, 51 support bars, 52 supporting tables, 53 is recessed
Groove, 54 fixing bolts, 6 governor motions, 61 first adjustment holes, 62 second adjustment holes, 63 screwed holes, 7 support bases, 71 axis holes, 72
Gag lever post, 8 pivot pins.
Embodiment
The utility model is further illustrated with reference to the accompanying drawings and examples：
Referring to Fig. 1-Fig. 3.
The utility model discloses a kind of aeroplane photography instrument, including casing 1, control platform 2, it is placed with the casing 1
GPS, the control platform 2 is interior to be provided with the mainboard electrically connected with the GPS, and the control platform 2 is provided with
The display screen and console electrically connected with the mainboard；The side wall of the control platform 2, which is provided with, to be used to be electrically connected with navigator's screen 3
The interface 4 connect, the interface 4 electrically connect with mainboard, this case by by mainboard vision signal input chip on each stitch with
Each stitch on interface 4, which corresponds, to be welded, and then leads to the navigator's screen 3 being placed in aircraft cockpit with interface 4
Cross wire connection so that pilot can be improved in aerial surveying camera use with real-time judge flight reappearance and camera exposure situation
Precision, while be reduced or avoided and mended winged situation, and reduce the laying quantity of ground photo control point, cost is greatly reduced,
Pilot can carry out contrast reference by the voyage conditions and aerial survey route of aircraft, reduce flight difficulty.
The interface 4 is USB interface, and the display device cost of USB interface is minimum, cost-effective.
The control platform 2 is arranged at the top of casing 1, one end of the control platform 2 and one end of the casing 1
It is be hinged；The bottom of the control platform 2 is provided with the supporting member 5 for support and control platform 2 with the top of casing 1, passes through
Control platform 2 and one end of casing 1 are hinged, and are supported the control platform 2 by supporting member 5, can put down control
Display screen on platform 2 enters line tilt, is easy to the survey crew in cabin to be observed.
The end of the side wall of the control platform 2, which is provided with, is used for the through hole that pivot pin 8 passes through, the top both sides of the casing 1
Provided with support base 7, the support base 7, which is provided with, is used for the axis hole 71 that pivot pin 8 passes through, and sequentially passes through axis hole 71 by pivot pin 8, leads to
Hole allows control platform 2 to be rotated around pivot pin 8, realizes the be hinged of control platform 2 and casing 1.
The side wall of the axis hole 71, which is provided with, is used for the spacing hole that gag lever post 72 passes through, by setting gag lever post 72 to ensure axle
Pin 8 will not skid off in the course of the work, it is ensured that the security of equipment.
The supporting member 5 include be arranged at the bottom of control platform 2 support bar 51 be hinged with it, be arranged at described in
The supporting table 52 at the top of casing 1, the supporting table 52 are provided with the width identical groove 53 of the support bar 51, the branch
The side wall both sides of support platform 52, which are provided with, is used for the screwed hole that fixing bolt 54 passes through, logical when needing after the slant setting of control platform 2
When crossing supporting member 5 and being supported control platform 2, it is only necessary to which two be placed on one end of support bar 51 in groove 52 are solid
Determine between bolt 54；When needing control platform 2 being laid flat, it is hinged by support bar 51 and the bottom of control platform 2, i.e.,
It can complete.
The side wall of supporting table 52 1 is provided with the governor motion 6 for being used for adjusting the horizontal level of fixing bolt 54, institute
Stating governor motion 6 includes the first elongated adjustment hole 61 of section, and the formed below of the first adjustment hole 61 connects therewith
The second logical adjustment hole 62, the cross-sectional width of second adjustment hole 62 is identical with the external diameter of the screw rod of the fixing bolt 54,
Second adjustment hole 62 at equal intervals array in the lower section of the first adjustment hole 61；In another side wall of the supporting table 52 formed with
The screwed hole 63 being connected with the end thread of fixing bolt 54 set at equal intervals to be alignd with second adjustment hole 62, passes through tune
The position that mechanism 6 adjusts fixing bolt 54 is saved, so that the fulcrum of support bar 51 changes, that is, realizes that control platform 2 can
To need to adjust its gradient according to different situations, so as to meet the requirement of user so that user is more easypro when observing
It is suitable；Operation principle：When needing that the gradient of control platform 2 is larger, by the screw rod end of fixing bolt 54 by screwed hole 63
Back-out, screw rod is then moved upwards up to the first adjustment hole 61 by the second adjustment hole 62, it is mobile according to the gradient being actually needed
Into suitable second adjustment hole 62, screw rod end is then subjected to threaded connection fixation with corresponding screwed hole 63, that is, completed
The regulation of governor motion 6.
Embodiment of the present utility model is the foregoing is only, not thereby limits the scope of the claims of the present utility model, it is every
The equivalents or the direct or indirect technical field for being used in correlation made using the utility model specification and accompanying drawing content,
Similarly it is included in scope of patent protection of the present utility model.
Claims (7)
1. a kind of aeroplane photography instrument, including casing（1）, control platform（2）, it is characterised in that：The casing（1）Inside it is placed with
GPS, the control platform（2）It is interior provided with the mainboard electrically connected with the GPS, the control platform（2）On
Provided with the display screen and console electrically connected with the mainboard；The control platform（2）Side wall be provided be used for and navigate shield
Curtain（3）The interface of electrical connection（4）, the interface（4）Electrically connected with mainboard.
2. aeroplane photography instrument according to claim 1, it is characterised in that：The interface（4）For USB interface.
3. aeroplane photography instrument according to claim 2, it is characterised in that：The control platform（2）It is arranged at the casing
（1）Top, the control platform（2）One end and the casing（1）One end be hinged；The control platform（2）Bottom with
The casing（1）Top, which is provided with, is used for support and control platform（2）Supporting member（5）.
4. aeroplane photography instrument according to claim 3, it is characterised in that：The control platform（2）The end of side wall set
Have and be used for pivot pin（8）The through hole passed through, the casing（1）Top both sides be provided with support base（7）, the support base（7）On set
Have and be used for pivot pin（8）The axis hole passed through（71）.
5. aeroplane photography instrument according to claim 4, it is characterised in that：The axis hole（71）Side wall be provided be used for limit
Position bar（72）The spacing hole passed through.
6. aeroplane photography instrument according to claim 5, it is characterised in that：The supporting member（5）It is described including being arranged at
Control platform（2）The bottom support bar be hinged with it（51）, be arranged at the casing（1）The supporting table at top（52）, the branch
Support platform（52）It is provided with the support bar（51）Width identical groove（53）, the supporting table（52）Side wall both sides set
Have and be used for fixing bolt（54）The screwed hole passed through.
7. aeroplane photography instrument according to claim 6, it is characterised in that：The supporting table（52）One side wall, which is provided with, to be used for
Adjust the fixing bolt（54）The governor motion of horizontal level（6）, the governor motion（6）Including section it is elongated
One adjustment hole（61）, first adjustment hole（61）The second adjustment hole in communication formed below（62）, described second
Adjustment hole（62）Cross-sectional width and the fixing bolt（54）Screw rod external diameter it is identical, second adjustment hole（62）Deng between
Every array in the first adjustment hole（61）Lower section；The supporting table（52）Another side wall on formed with second adjustment hole
（62）The set at equal intervals and fixing bolt of alignment（54）The screwed hole of end thread connection（63）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720546999.9U CN206683639U (en) | 2017-05-17 | 2017-05-17 | Aeroplane photography instrument |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720546999.9U CN206683639U (en) | 2017-05-17 | 2017-05-17 | Aeroplane photography instrument |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206683639U true CN206683639U (en) | 2017-11-28 |
Family
ID=60406186
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720546999.9U Active CN206683639U (en) | 2017-05-17 | 2017-05-17 | Aeroplane photography instrument |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206683639U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109365382A (en) * | 2018-10-25 | 2019-02-22 | 广东合新材料研究院有限公司 | A kind of server cleaning equipment and its cleaning method |
-
2017
- 2017-05-17 CN CN201720546999.9U patent/CN206683639U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109365382A (en) * | 2018-10-25 | 2019-02-22 | 广东合新材料研究院有限公司 | A kind of server cleaning equipment and its cleaning method |
| CN109365382B (en) * | 2018-10-25 | 2024-03-12 | 广东西江数据科技有限公司 | Server cleaning equipment and cleaning method thereof |
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