CN208325613U - A kind of aerial photography aircraft can be improved landing safety - Google Patents
A kind of aerial photography aircraft can be improved landing safety Download PDFInfo
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- CN208325613U CN208325613U CN201820621221.4U CN201820621221U CN208325613U CN 208325613 U CN208325613 U CN 208325613U CN 201820621221 U CN201820621221 U CN 201820621221U CN 208325613 U CN208325613 U CN 208325613U
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- aircraft
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- damping
- fixedly installed
- aircraft body
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Abstract
The utility model discloses a kind of aerial photography aircrafts that can be improved landing safety, including aircraft body, the leading exterior surface of the aircraft body is fixedly installed with damping box, and the upper end outer surface of damping box is fixedly installed with brake box, the upper end of the brake box is movably installed with propeller, the lower end outer surface of the aircraft body is movably installed with pressure-bearing column, and the lower end outer surface splicing of pressure-bearing column has buffering foot pad, a side external surface of the aircraft body is fixedly installed with connection cross bar close to the position of front end.A kind of aerial photography aircraft can be improved landing safety described in the utility model, equipped with damping box, shield and storage box, safety of the aircraft in landing can be allowed higher, avoid aircraft damage, and the situation that can prevent propeller blade from hurting sb.'s feelings occurs, the aircraft can also be allowed to be provided with the function of goods transportation simultaneously, bring better prospect of the application.
Description
Technical field
The utility model relates to a kind of aerial photography aircraft fields, in particular to a kind of to can be improved taking photo by plane for landing safety
Aircraft.
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, and taken photo by plane and used aircraft more
Shooting operation is carried out, to say exactly a kind of aerial photography aircraft that can be improved landing safety here；Existing aerial photography aircraft
There are certain drawbacks when in use, protection effect is poor, and safety when being easy to hurt sb.'s feelings, and landing is lower, cannot
Meet the use demand of user, for this purpose, it is proposed that a kind of aerial photography aircraft that can be improved landing safety.
Utility model content
The main purpose of the utility model is to provide a kind of aerial photography aircraft that can be improved landing safety, Ke Yiyou
Effect solves the problems in background technique.
To achieve the above object, the technical solution that the utility model is taken are as follows:
A kind of aerial photography aircraft can be improved landing safety, including aircraft body, before the aircraft body
End outer surface is fixedly installed with damping box, and the upper end outer surface of damping box is fixedly installed with brake box, the brake box it is upper
End is movably installed with propeller, and the lower end outer surface of the aircraft body is movably installed with pressure-bearing column, and the lower end of pressure-bearing column
Outer surface, which is glued, buffering foot pad, and a side external surface of the aircraft body is fixedly installed with connection cross close to the position of front end
Bar, and the lower end for connecting cross bar is fixedly installed with No.1 camera, the leading exterior surface of the aircraft body is close to side
Position is fixedly installed with No. two cameras, and the upper end outer surface of the aircraft body is fixedly installed with buzzer, the damping
The external activity of box is equipped with shield, and the inner surface of the aircraft body is equipped with threaded hole, and the lower end of aircraft body
Outer surface is equipped with hanging hook and attachment base, and the side of hanging hook is arranged in attachment base, and the hanging hook passes through threaded hole and flies
The connection of row device subject activity, the inside of the attachment base are equipped with connecting hole, and the inside of connecting hole is through there is connecting screw, adjacent
Position between attachment base described in two groups is movably installed with storage box.
Preferably, the inner surface of the damping box is equipped with limiting slot, and the inside of damping box is close to the position activity on top
Main damping spring and auxiliary damping spring are installed, and the side of main damping spring, the damping is arranged in auxiliary damping spring
The inside of box is movably installed with buffer spring close to the position of bottom end, the position between the buffer spring and auxiliary damping spring
It is movably installed with pressure block, and pressure block is fixedly connected with one end of pressure-bearing column.
Preferably, the inside of the aircraft body is fixedly installed with battery, gyroscope and signal receiving module, and stores
The side of gyroscope is arranged in battery, and the other side of gyroscope is arranged in the signal receiving module.
Preferably, the inner surface of the shield is fixedly installed with connecting rod, and the outer surface of the damping box is equipped with connection
One end of slot, the connecting rod is flexibly connected by link slot with damping box.
Preferably, the output end of the battery is electrically connected the input terminal of buzzer, gyroscope and brake box, described to subtract
The quantity for shaking box is four groups, and damping box is equidistantly placed in a ring centered on the midpoint of aircraft body.
Compared with prior art, the utility model has the following beneficial effects: this can be improved taking photo by plane for landing safety
Aircraft can absorb the impact force that the aircraft is generated in landing, substantially increase the flight by the damping box of setting
The landing safety of device can play protective action by the shield of setting, it is therefore prevented that aircraft landing rear screw shaft wound
The situation of people occurs, and can easily be dismantled, and by the storage box and hanging hook of setting, the aircraft is allowed to be provided with one
The ability of fixed goods transportation, while also can allow the aircraft that can transport different types of article, whole device is simple, behaviour
Facilitate, the effect used is more preferable relative to traditional approach.
Detailed description of the invention
Fig. 1 is the overall structure diagram of the utility model.
Fig. 2 is that the aircraft body of the utility model combines view with storage box.
Fig. 3 is the damping box interior views of the utility model.
Fig. 4 is that the damping box of the utility model combines view with shield.
In figure: 1, aircraft body；2, damping box；3, brake box；4, propeller；5, pressure-bearing column；6, buffering foot pad；7, even
Connect cross bar；8, No.1 camera；9, No. two cameras；10, buzzer；11, shield；12, battery；13, gyroscope；14,
Signal receiving module；15, threaded hole；16, hanging hook；17, attachment base；18, connecting hole；19, connecting screw；20, storage box；
21, limiting slot；22, main damping spring；23, damping spring is assisted；24, buffer spring；25, pressure block；26, link slot；27, even
Extension bar.
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.
As shown in Figs 1-4, a kind of aerial photography aircraft can be improved landing safety, including aircraft body 1, aircraft
The leading exterior surface of main body 1 is fixedly installed with damping box 2, and damping box 2 plays damping, and the upper end outer surface of damping box 2
It is fixedly installed with brake box 3, brake box 3 provides power for aircraft, and the upper end of brake box 3 is movably installed with propeller 4, flight
The lower end outer surface of device main body 1 is movably installed with pressure-bearing column 5, and the lower end outer surface splicing of pressure-bearing column 5 has buffering foot pad 6, flies
One side external surface of row device main body 1 is fixedly installed with connection cross bar 7 close to the position of front end, and the lower end for connecting cross bar 7 is fixed
No.1 camera 8 is installed, the leading exterior surface of aircraft body 1 is fixedly installed with No. two cameras 9 close to the position of side,
The upper end outer surface of aircraft body 1 is fixedly installed with buzzer 10, and the external activity of damping box 2 is equipped with shield 11, prevents
Shield 11 can prevent propeller 4 from hurting sb.'s feelings, and the inner surface of aircraft body 1 is equipped with threaded hole 15, and the lower end of aircraft body 1
Outer surface is equipped with hanging hook 16 and attachment base 17, and the side of hanging hook 16 is arranged in attachment base 17, and hanging hook 16 passes through screw thread
Hole 15 is flexibly connected with aircraft body 1, and the inside of attachment base 17 is equipped with connecting hole 18, and the inside of connecting hole 18 is through there is company
Connect screw 19, the position between two adjacent groups attachment base 17 is movably installed with storage box 20, and the setting of storage box 20 allows the flight
Device is provided with the function of goods transportation.
The inner surface of damping box 2 is equipped with limiting slot 21, and the inside of damping box 2 is movably installed with master close to the position on top
Damping spring 22 and auxiliary damping spring 23, main damping spring 22 play bumper and absorbing shock with auxiliary damping spring 23, and auxiliary
Help damping spring 23 that the side of main damping spring 22 is set, the inside of damping box 2 is movably installed with slow close to the position of bottom end
Spring 24 is rushed, the position between buffer spring 24 and auxiliary damping spring 23 is movably installed with pressure block 25, and pressure block 25 is used to
Transmission force, and pressure block 25 is fixedly connected with one end of pressure-bearing column 5；The inside of aircraft body 1 be fixedly installed with battery 12,
Gyroscope 13 and signal receiving module 14, and the side of gyroscope 13 is arranged in battery 12, the setting of signal receiving module 14 exists
The other side of gyroscope 13；The inner surface of shield 11 is fixedly installed with connecting rod 27, and the outer surface of damping box 2 is equipped with link slot
26, link slot 26 plays connection function, and one end of connecting rod 27 is flexibly connected by link slot 26 with damping box 2；Battery 12
Output end is electrically connected the input terminal of buzzer 10, gyroscope 13 and brake box 3, and the quantity of damping box 2 is four groups, and damping box
2 are equidistantly placed in a ring centered on the midpoint of aircraft body 1.
It should be noted that the utility model is a kind of aerial photography aircraft that can be improved landing safety, fly when use
Battery 12 in row device main body 1 provides power supply for the aircraft, and the brake motor in flight in brake box 3 drives propeller
4 rotations provide lift, so that the aircraft is able to carry out flight, gyroscope 13 ensure that the aircraft flight while flight
Stability, the model M3110758 of gyroscope 13, the signal receiving module 14 in aircraft body 1 is used to receive control letter
Number, when aircraft landing, the power being subject to is transferred on pressure-bearing column 5 by the first stress of buffering foot pad 6, buffering foot pad 6, pressure-bearing column 5
Power is transmitted to main damping spring 22 and assisted on damping spring 23 by pressure block 25 again, main damping spring 22 and auxiliary damping
23 deformation absorbability of spring, and power is transferred on buffer spring 24 again by pressure block 25, power passes through the suction of spring repeatedly
Receipts can die down, thus reduce the impact force that the aircraft is generated in landing, so that the landing safety of the aircraft is higher,
When user needs to transport article with the aircraft, it can be selected according to type of items using storage box 20 or hang object
Hook 16, shield 11 are mounted on brake box 3 by connecting rod 27, and shield 11 can prevent aircraft spiral in landing
Paddle 4 rotates the situation hurted sb.'s feelings and occurs, and can disassemble shield 11 when needing to transport article, and it is automatic to reach mitigation
The purpose of hauled weight is improved, buzzer 10 can release sound and drive birds when having birds to attack aircraft in flight course,
The model NPN9013 of buzzer 10 is more practical.
The basic principles and main features of the present invention and the advantages of the present invention have been shown and described above.Current row
The technical staff of industry is described in above embodiments and description it should be appreciated that the present utility model is not limited to the above embodiments
Only illustrate the principles of the present invention, on the premise of not departing from the spirit and scope of the utility model, the utility model is also
It will have various changes and improvements, these various changes and improvements fall within the scope of the claimed invention.The utility model
Claimed range is defined by the appending claims and its equivalent thereof.
Claims (5)
1. a kind of aerial photography aircraft that can be improved landing safety, including aircraft body (1), it is characterised in that: described to fly
The leading exterior surface of row device main body (1) is fixedly installed with damping box (2), and the upper end outer surface of damping box (2) is fixedly installed with
The upper end of brake box (3), the brake box (3) is movably installed with propeller (4), the lower end appearance of the aircraft body (1)
Face is movably installed with pressure-bearing column (5), and the lower end outer surface splicing of pressure-bearing column (5) has buffering foot pad (6), the aircraft body
(1) a side external surface is fixedly installed with connection cross bar (7) close to the position of front end, and the fixed peace in the lower end for connecting cross bar (7)
Equipped with No.1 camera (8), the leading exterior surface of the aircraft body (1) is fixedly installed with No. two close to the position of side and takes the photograph
As head (9), the upper end outer surface of the aircraft body (1) is fixedly installed with buzzer (10), the outside of the damping box (2)
It is movably installed with shield (11), the inner surface of the aircraft body (1) is equipped with threaded hole (15), and aircraft body (1)
Lower end outer surface be equipped with hanging hook (16) and attachment base (17), and attachment base (17) is arranged in the side of hanging hook (16), institute
It states hanging hook (16) to be flexibly connected across threaded hole (15) with aircraft body (1), the inside of the attachment base (17), which is equipped with, to be connected
It connects hole (18), and the inside of connecting hole (18) is through having connecting screw (19), the position between attachment base (17) described in two adjacent groups
It sets and is movably installed with storage box (20).
2. a kind of aerial photography aircraft that can be improved landing safety according to claim 1, it is characterised in that: described to subtract
The inner surface for shaking box (2) is equipped with limiting slot (21), and the inside of damping box (2) is movably installed with main damping close to the position on top
Spring (22) and auxiliary damping spring (23), and assist damping spring (23) setting described in the side of main damping spring (22)
The inside of damping box (2) is movably installed with buffer spring (24) close to the position of bottom end, and the buffer spring (24) subtracts with auxiliary
Position between shake spring (23) is movably installed with pressure block (25), and the fixed company in one end of pressure block (25) and pressure-bearing column (5)
It connects.
3. a kind of aerial photography aircraft that can be improved landing safety according to claim 1, it is characterised in that: described to fly
The inside of row device main body (1) is fixedly installed with battery (12), gyroscope (13) and signal receiving module (14), and battery
(12) setting is in the side of gyroscope (13), and signal receiving module (14) setting is described in the other side of gyroscope (13)
The output end of battery (12) is electrically connected the input terminal of buzzer (10), gyroscope (13) and brake box (3).
4. a kind of aerial photography aircraft that can be improved landing safety according to claim 1, it is characterised in that: described anti-
The inner surface of shield (11) is fixedly installed with connecting rod (27), and the outer surface of the damping box (2) is equipped with link slot (26), described
One end of connecting rod (27) is flexibly connected by link slot (26) with damping box (2).
5. a kind of aerial photography aircraft that can be improved landing safety according to claim 1, it is characterised in that: described to subtract
The quantity for shaking box (2) is four groups, and damping box (2) is equidistantly placed in a ring centered on the midpoint of aircraft body (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820621221.4U CN208325613U (en) | 2018-04-27 | 2018-04-27 | A kind of aerial photography aircraft can be improved landing safety |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820621221.4U CN208325613U (en) | 2018-04-27 | 2018-04-27 | A kind of aerial photography aircraft can be improved landing safety |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208325613U true CN208325613U (en) | 2019-01-04 |
Family
ID=64778786
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820621221.4U Expired - Fee Related CN208325613U (en) | 2018-04-27 | 2018-04-27 | A kind of aerial photography aircraft can be improved landing safety |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208325613U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109823538A (en) * | 2019-01-22 | 2019-05-31 | 广州林电科技有限公司 | A kind of unmanned flight's transport device with anti-interference function for logistics |
-
2018
- 2018-04-27 CN CN201820621221.4U patent/CN208325613U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109823538A (en) * | 2019-01-22 | 2019-05-31 | 广州林电科技有限公司 | A kind of unmanned flight's transport device with anti-interference function for logistics |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190104 Termination date: 20200427 |