CN208665556U - A kind of novel equipment of taking photo by plane for low latitude monitoring - Google Patents
A kind of novel equipment of taking photo by plane for low latitude monitoring Download PDFInfo
- Publication number
- CN208665556U CN208665556U CN201820926201.8U CN201820926201U CN208665556U CN 208665556 U CN208665556 U CN 208665556U CN 201820926201 U CN201820926201 U CN 201820926201U CN 208665556 U CN208665556 U CN 208665556U
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- Prior art keywords
- plane
- gear
- taking photo
- supporting plate
- spring
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- 238000012544 monitoring process Methods 0.000 title claims abstract description 15
- 239000000872 buffer Substances 0.000 claims abstract description 17
- 230000003139 buffering effect Effects 0.000 claims abstract description 12
- 238000003780 insertion Methods 0.000 claims description 9
- 230000037431 insertion Effects 0.000 claims description 9
- 230000017525 heat dissipation Effects 0.000 claims 1
- 230000006835 compression Effects 0.000 abstract description 6
- 238000007906 compression Methods 0.000 abstract description 6
- 229910000639 Spring steel Inorganic materials 0.000 description 3
- 238000009434 installation Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000006641 stabilisation Effects 0.000 description 2
- 238000011105 stabilization Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000001934 delay Effects 0.000 description 1
- 239000013013 elastic material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012806 monitoring device Methods 0.000 description 1
- 210000000056 organ Anatomy 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
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Abstract
The utility model discloses a kind of novel equipment of taking photo by plane for low latitude monitoring, its structure includes propeller, rotator, indicator light, buffering take-off and landing device includes shell, upper backup pad, two-way rack bar, sliding block, hinge device, lower supporting plate, a kind of novel equipment of taking photo by plane for low latitude monitoring of the utility model, buffering take-off and landing device is provided in structure, it is moved down by upper backup pad, two-way rack bar is driven to move down, being meshed by two-way rack bar with gear rotates gear, it is meshed by wheel and rack, move up rack gear, it is moved up by rack gear and buffers spring-compressed, it is above pushed away by lower supporting plate, spring-compressed is buffered, hinge device is driven by lower supporting plate, making hinge device upper end, both ends push to the left and right, it is slided by hinge device band movable slider, buffer spring compression is buffered by sliding block, in this way The backwardness under equipment that can prevent from taking photo by plane knocks ground, improves the impact resistance of equipment.
Description
Technical field
The utility model is a kind of novel equipment of taking photo by plane for low latitude monitoring, belongs to the field of taking photo by plane.
Background technique
It takes photo by plane also known as aerophotography or aeroplane photography, refers to from aerial photographing earth landforms, obtain top view, this figure is
Photo map, the video camera taken photo by plane can be controlled by photographer, can also be automatically snapped or remotely be controlled.Platform packet used in taking photo by plane
Model airplane, aircraft, helicopter, fire balloon, blimp, rocket, kite, parachute etc. are included, in order to allow aerial photograph to stablize,
It will use advanced photographic equipment sometimes, it utilizes three-axis gyroscope stabilization function, provides the stabilization picture of high quality, even
Also highly stable under long focal length lens, figure of taking photo by plane can clearly show geographical form, therefore in addition to as photography art
Except one ring, it is also employed for military affairs, transport development, hydraulic engineering, ecological Studies, urban planning etc..
Prior art discloses a kind of novel take photo by plane for low latitude monitoring application No. is: CN201520445720.9 to set
It is standby, including apparatus body of taking photo by plane, equipment camera of taking photo by plane, equipment of taking photo by plane electrical storage device, the apparatus body lower end placement institute that takes photo by plane
State equipment camera of taking photo by plane；The equipment electrical storage device of taking photo by plane described in the installation of equipment camera rear end of taking photo by plane；The equipment storage of taking photo by plane
Electric appliance or so installs equipment servo motor of taking photo by plane；Install installation electromagnetical coil of taking photo by plane in the equipment servo motor upper end of taking photo by plane；Institute
It states installation electromagnetical coil right end of taking photo by plane and device orientation controller of taking photo by plane is installed；Boat is inlayed inside the device orientation controller of taking photo by plane
Clap device orientation controller chip；The apparatus body surrounding of taking photo by plane installs equipment propeller of taking photo by plane, but the prior art is navigated
Equipment is clapped when dropping to bottom surface, is easy mutually to collide with ground, causes equipment to be damaged, the later period is difficult to reuse.
Utility model content
In view of the deficienciess of the prior art, the utility model aim is to provide a kind of novel taking photo by plane for low latitude monitoring
Equipment takes photo by plane equipment when dropping to bottom surface to solve the prior art, is easy mutually to collide with ground, equipment is caused to be damaged
Wound, later period are difficult to the problem of reusing.
To achieve the goals above, the utility model is achieved through the following technical solutions: a kind of supervise for low latitude
The novel equipment of taking photo by plane of control, structure include propeller, rotator, wing fixed frame, main body, support leg, support frame, buffer
On the same axis, the rotator is installed on machine for dropping control device, monitor, heat release hole, indicator light, the propeller and rotator
On wing fixed frame outer end, main body is installed on the wing fixed frame, is connected with support leg, support frame as described above below the main body
It is installed in main body, the buffering take-off and landing device includes shell, upper backup pad, two-way rack bar, gear, rack gear, fixed plate, bullet
Spring, buffer spring, sliding block, hinge device, lower supporting plate are equipped with upper backup pad, the upper backup pad lower end surface on the shell
It is connected with two-way rack bar upper end, the two-way rack bar is meshed with gear, and the gear insertion is installed in shell, institute
It states rack and pinion to be meshed, spring, the lower spring end face and lower supporting plate upper surface phase is installed below the fixed plate
Fitting, the buffer spring right end are equipped with sliding block, and the sliding block is connected with hinge device upper end, and the hinge device lower end is installed on
On lower supporting plate, insertion is installed in shell on the lower supporting plate.
Further, the buffering take-off and landing device upper surface fits with support leg lower surface, and the monitor is installed on
In main body.
Further, for the heat release hole through on wing fixed frame, the indicator light insertion is installed on wing fixed frame
On.
Further, the upper backup pad upper surface fits with support leg lower end surface.
Further, the gear diameter is 5cm.
Further, the rotator is cylindrical structure.
Further, the spring is made of spring steel, has elastic effect.
Beneficial effect
A kind of novel equipment of taking photo by plane for low latitude monitoring of the utility model, is provided with buffering take-off and landing device in structure,
It is moved down by upper backup pad, two-way rack bar is driven to move down, being meshed by two-way rack bar with gear rotates gear, passes through
Wheel and rack is meshed, and moves up rack gear, is moved up by rack gear and buffers spring-compressed, is above pushed away by lower supporting plate,
Spring-compressed is buffered, hinge device is driven by lower supporting plate, making hinge device upper end, both ends push to the left and right, pass through hinge
Device band movable slider slides, and is buffered buffer spring compression by sliding block, backwardness is hit under the equipment that can prevent from taking photo by plane in this way
Upper ground surface improves the impact resistance of equipment.
Detailed description of the invention
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other spies of the utility model
Sign, objects and advantages will become more apparent upon:
Fig. 1 is a kind of structural schematic diagram of the novel equipment of taking photo by plane for low latitude monitoring of the utility model；
Fig. 2 is the buffering take-off and landing device the schematic diagram of the section structure of the utility model.
In figure: propeller -1, rotator -2, wing fixed frame -3, main body -4, support leg -5, support frame -6, buffering are risen and fallen
Device -7, monitor -8, heat release hole -9, indicator light -10, shell -701, upper backup pad -702, two-way rack bar -703, gear -
704, rack gear -705, fixed plate -706, spring -707, buffer spring -708, sliding block -709, hinge device -710, lower supporting plate -
711。
Specific embodiment
To be easy to understand the technical means, creative features, achievement of purpose, and effectiveness of the utility model, below
In conjunction with specific embodiment, the utility model is further described.
Fig. 1, Fig. 2 are please referred to, the utility model provides a kind of novel equipment and technology scheme of taking photo by plane for low latitude monitoring: its
Structure includes propeller 1, rotator 2, wing fixed frame 3, main body 4, support leg 5, support frame 6, buffering take-off and landing device 7, monitoring
Device 8, heat release hole 9, indicator light 10, on the same axis with rotator 2, it is solid that the rotator 2 is installed on wing to the propeller 1
Determine on 3 outer end of frame, main body 4 is installed on the wing fixed frame 3, support leg 5, the support are connected with below the main body 4
Frame 6 is installed in main body 4, and the buffering take-off and landing device 7 includes shell 701, upper backup pad 702, two-way rack bar 703, gear
704, rack gear 705, fixed plate 706, spring 707, buffer spring 708, sliding block 709, hinge device 710, lower supporting plate 711, it is described
Upper backup pad 702 is installed, 702 lower end surface of upper backup pad is connected with two-way 703 upper end of rack bar, institute on shell 701
It states two-way rack bar 703 to be meshed with gear 704, the insertion of gear 704 is installed in shell 701, the rack gear 705 and tooth
Wheel 704 is meshed, and spring 707,707 lower end surface of spring and 711 upper end of lower supporting plate are equipped with below the fixed plate 706
Face fits, and 708 right end of buffer spring is equipped with sliding block 709, and the sliding block 709 is connected with 710 upper end of hinge device, described
710 lower end of hinge device is installed on lower supporting plate 711, and insertion is installed in shell 701 on the lower supporting plate 711, described slow
It rushes 7 upper surface of take-off and landing device to fit with 5 lower surface of support leg, the monitor 8 is installed in main body 4, and the heat release hole 9 passes through
Be through on wing fixed frame 3, the indicator light 10 insertion is installed on wing fixed frame 3,702 upper surface of upper backup pad with
5 lower end surface of support leg fits, and 704 diameter of gear is 5cm, and the rotator 2 is cylindrical structure, the spring 707
It is made of spring steel, there is elastic effect.
Gear 704 described in this patent refers to the mechanical organ for having gear continuously to engage passing movement and power on wheel rim,
The spring 707 is a kind of using the elastic machine components come work, and the part made of elastic material is sent out under external force
Raw deformation restores to the original state again after removing external force, also makees " spring ", be generally made of spring steel.
Moved down in use, passing through upper backup pad 702, is driving two-way rack bar 703 to move down, pass through two-way rack bar
703 are meshed with gear 704 rotates gear 704, is meshed by gear 704 with rack gear 705, moves up rack gear 705, pass through
Rack gear 705, which moves up, buffers the compression of spring 707, is above pushed away by lower supporting plate 711, the compression of spring 707 is buffered, is led to
It crosses lower supporting plate 711 and drives hinge device 710, making 710 upper end of hinge device, both ends push to the left and right, are driven and are slided by hinge device 710
Block 709 slides, and is buffered the compression of buffer spring 708 by sliding block 709.
The utility model solves the prior art and takes photo by plane equipment when dropping to bottom surface, is easy mutually to collide with ground, lead
Equipment is caused to be damaged, the later period is difficult to the problem of reusing, and the utility model is combined with each other by above-mentioned component, in structure
It is upper to be provided with buffering take-off and landing device, it is moved down by upper backup pad, two-way rack bar is driven to move down, pass through two-way rack bar and gear
Being meshed rotates gear, is meshed by wheel and rack, moves up rack gear, is moved up by rack gear and delays spring-compressed
Punching, above pushed away by lower supporting plate, spring-compressed buffered, by lower supporting plate drive hinge device, make hinge device upper end to
Left and right ends push, and are slided by hinge device band movable slider, buffer buffer spring compression by sliding block, in this way can
The backwardness under equipment that prevents from taking photo by plane knocks ground, improves the impact resistance of equipment.
The basic principles and main features of the present invention and the advantages of the present invention have been shown and described above, for
For those skilled in the art, it is clear that the present invention is not limited to the details of the above exemplary embodiments, and without departing substantially from this
In the case where the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter
From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the utility model is by institute
Attached claim rather than above description limit, it is intended that will fall within the meaning and scope of the equivalent elements of the claims
All changes are embraced therein.It should not treat any reference in the claims as limiting related right
It is required that.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
The other embodiments being understood that.
Claims (5)
1. a kind of novel equipment of taking photo by plane for low latitude monitoring, it is characterised in that: its structure includes propeller (1), rotator
(2), wing fixed frame (3), main body (4), support leg (5), support frame (6), buffering take-off and landing device (7), monitor (8), heat dissipation
Hole (9), indicator light (10), on the same axis, the rotator (2) is installed on wing for the propeller (1) and rotator (2)
It on fixed frame (3) outer end, is equipped with main body (4) on the wing fixed frame (3), is connected with support leg below the main body (4)
(5), support frame as described above (6) is installed on main body (4), and the buffering take-off and landing device (7) includes shell (701), upper backup pad
(702), two-way rack bar (703), gear (704), rack gear (705), fixed plate (706), spring (707), buffer spring
(708), sliding block (709), hinge device (710), lower supporting plate (711) are equipped with upper backup pad (702) on the shell (701),
Upper backup pad (702) lower end surface is connected with two-way rack bar (703) upper end, the two-way rack bar (703) and gear
(704) it is meshed, gear (704) insertion is installed in shell (701), and the rack gear (705) is mutually nibbled with gear (704)
It closes, is equipped with spring (707) below the fixed plate (706), spring (707) lower end surface and lower supporting plate (711) upper end
Face fits, and buffer spring (708) right end is equipped with sliding block (709), the sliding block (709) and hinge device (710) upper end phase
Connection, hinge device (710) lower end are installed on lower supporting plate (711), and insertion is installed on outer on the lower supporting plate (711)
In shell (701).
2. a kind of novel equipment of taking photo by plane for low latitude monitoring according to claim 1, it is characterised in that: described to buffer
Dropping control device (7) upper surface fits with support leg (5) lower surface, and the monitor (8) is installed on main body (4).
3. a kind of novel equipment of taking photo by plane for low latitude monitoring according to claim 1, it is characterised in that: the heat release hole
(9) through on wing fixed frame (3), indicator light (10) insertion is installed on wing fixed frame (3).
4. a kind of novel equipment of taking photo by plane for low latitude monitoring according to claim 1, it is characterised in that: the upper support
Plate (702) upper surface fits with support leg (5) lower end surface.
5. a kind of novel equipment of taking photo by plane for low latitude monitoring according to claim 1, it is characterised in that: the gear
(704) diameter is 5cm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820926201.8U CN208665556U (en) | 2018-06-14 | 2018-06-14 | A kind of novel equipment of taking photo by plane for low latitude monitoring |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820926201.8U CN208665556U (en) | 2018-06-14 | 2018-06-14 | A kind of novel equipment of taking photo by plane for low latitude monitoring |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208665556U true CN208665556U (en) | 2019-03-29 |
Family
ID=65824628
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820926201.8U Expired - Fee Related CN208665556U (en) | 2018-06-14 | 2018-06-14 | A kind of novel equipment of taking photo by plane for low latitude monitoring |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208665556U (en) |
-
2018
- 2018-06-14 CN CN201820926201.8U patent/CN208665556U/en not_active Expired - Fee Related
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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: 20190329 |