CN208325612U - It is a kind of to decline stable mapping unmanned plane - Google Patents
It is a kind of to decline stable mapping unmanned plane Download PDFInfo
- Publication number
- CN208325612U CN208325612U CN201820490731.2U CN201820490731U CN208325612U CN 208325612 U CN208325612 U CN 208325612U CN 201820490731 U CN201820490731 U CN 201820490731U CN 208325612 U CN208325612 U CN 208325612U
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- China
- Prior art keywords
- unmanned plane
- fuselage
- supporting leg
- rotation button
- fixedly connected
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Abstract
Decline stable mapping unmanned plane the utility model discloses a kind of, including casing assembly and fixation kit, the casing assembly includes fuselage, rotation button, propeller, mounting base, wing, fixing seat, camera and pedestal, the rotation button is located above the left side of the fuselage, and it is rotatablely connected with the fuselage, the fixed seating is fixedly connected in the bottom surface of the rotation button, and with the rotation button, and the wing is located at the left outer surface of the rotation button；In the outside of attachment base, there are four connecting rods for setting, the bottom surface of connecting rod is provided with supporting leg, supporting leg is internally provided with spring, when unmanned plane landing, the inertia that generates when can buffer unmanned plane decline by spring enables what unmanned plane consolidated to be parked in ground, the bottom surface of supporting leg is provided with elastic cushion, the frictional force between unmanned plane and ground can be increased, stablize unmanned plane also can on uneven ground and park, increase the safety of unmanned plane.
Description
Technical field
The utility model belongs to mapping air vehicle technique field, and in particular to a kind of to decline stable mapping unmanned plane.
Background technique
Unmanned plane is surveyed and drawn, is the not manned aircraft manipulated using radio robot and the presetting apparatus provided for oneself,
Or it fully or is intermittently automatically operated by car-mounted computer.
Original mapping unmanned plane may drop on the uneven bottom surface of topography since unmanned plane is in decline, existing
The decline bracket of some unmanned planes uses the bracket of surface smoother, and may cause unmanned plane, run-off the straight is fallen on ground
, damage unmanned plane.
Utility model content
Decline stable mapping unmanned plane the purpose of this utility model is to provide a kind of, to solve in above-mentioned background technique
The original mapping unmanned plane proposed may drop on the uneven bottom surface of topography since unmanned plane is in decline, existing
The decline bracket of unmanned plane use the bracket of surface smoother, may cause unmanned plane, run-off the straight is fallen on ground
, the problem of damaging unmanned plane.
To achieve the above object, the utility model provides the following technical solutions: a kind of to decline stable mapping unmanned plane, packet
Casing assembly and fixation kit are included, the casing assembly includes fuselage, rotation button, propeller, mounting base, wing, fixing seat, takes the photograph
As head and pedestal, the rotation button is located above the left side of the fuselage, and is rotatablely connected with the fuselage, the fixed seating
It being fixedly connected in the bottom surface of the rotation button, and with the rotation button, the wing is located at the left outer surface of the rotation button,
And be fixedly connected with the rotation button, the mounting base is located at the left end of the wing, and is fixedly connected with the wing, described
Propeller is located at the upper surface of the mounting base, and is rotatablely connected with the mounting base, and the pedestal is located at the bottom of the fuselage
Face, and be fixedly connected with the fuselage, the camera is located at the bottom surface of the pedestal, and connect with the base rotation, institute
Stating fuselage includes locator, and the locator is located at the upper surface of the fuselage, and is fixedly connected with the fuselage, the fixation
Component includes connecting rod, elastic cushion, supporting leg and attachment base, and the attachment base is located at the bottom surface of the fuselage close to the pedestal
Rear, and be fixedly connected with the fuselage, the connecting rod is located at the front surface of the attachment base, and solid with the attachment base
Fixed connection, the supporting leg is located at the bottom surface of the connecting rod, and is fixedly connected with the connecting rod, and the elastic cushion is located at institute
The bottom surface of supporting leg is stated, and is fixedly connected with the supporting leg.
Preferably, the inside of the supporting leg offers the first cavity, and first cavity is internally provided with spring, institute
Spring is stated to be fixedly connected with the supporting leg.
Preferably, the quantity of the connecting rod is four, and four connecting rods are in cross arrangement in the attachment base
Outside.
Preferably, the quantity of the mounting base is four, and four mounting bases are symmetrical along the longitudinal section of the fuselage
Distribution.
Preferably, the inside of the mounting base offers the second cavity, and second cavity is internally provided with motor, institute
Motor is stated to be fixedly connected with the mounting base.
Compared with prior art, the utility model has the beneficial effects that being arranged in the bottom surface of fuselage close to the rear of pedestal
Have attachment base, in the outside of attachment base, setting is there are four connecting rod, the bottom surface of connecting rod is provided with supporting leg, supporting leg it is interior
Portion is provided with spring, when unmanned plane landing, can buffer the inertia generated when unmanned plane decline by spring, make unmanned function
Enough firm is parked in ground, and the bottom surface of supporting leg is provided with elastic cushion, can increase the frictional force between unmanned plane and ground,
It stablize unmanned plane also can on uneven ground to park, be improved the safety of unmanned plane.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the overlooking structure diagram of the utility model；
Fig. 3 is the connecting rod structural schematic diagram in the utility model；
In figure: 10- casing assembly, 11- fuselage, 12- rotation button, 13- propeller, 14- mounting base, 15- wing, 16- are solid
Reservation, 17- camera, 18- pedestal, 111- locator, 20- fixation kit, 21- connecting rod, 22- elastic cushion, 23- supporting leg,
24- attachment base.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Fig. 1-3 is please referred to, the utility model provides a kind of technical solution: it is a kind of to decline stable mapping unmanned plane, including
Casing assembly 10 and fixation kit 20, casing assembly 10 include fuselage 11, rotation button 12, propeller 13, mounting base 14, wing
15, fixing seat 16, camera 17 and pedestal 18, rotation button 12 are located above the left side of fuselage 11, and rotate and connect with fuselage 11
It connects, fixing seat 16 is located at the bottom surface of rotation button 12, and is fixedly connected with rotation button 12, and wing 15 is located at the left side of rotation button 12
Outer surface, and be fixedly connected with rotation button 12, mounting base 14 is located at the left end of wing 15, and is fixedly connected with wing 15, spiral
Paddle 13 is located at the upper surface of mounting base 14, and is rotatablely connected with mounting base 14, and pedestal 18 is located at the bottom surface of fuselage 11, and and machine
Body 11 is fixedly connected, and camera 17 is located at the bottom surface of pedestal 18, and is rotatablely connected with pedestal 18, and fuselage 11 includes locator 111,
Locator 111 is located at the upper surface of fuselage 11, and is fixedly connected with fuselage 11, and fixation kit 20 includes connecting rod 21, elastic cushion
22, supporting leg 23 and attachment base 24, attachment base 24 are located at the bottom surface of fuselage 11 close to the rear of pedestal 18, and fixed with fuselage 11
Connection, connecting rod 21 is located at the front surface of attachment base 24, and is fixedly connected with attachment base 24, and supporting leg 23 is located at connecting rod 21
Bottom surface, and be fixedly connected with connecting rod 21, elastic cushion 22 is located at the bottom surface of supporting leg 23, and is fixedly connected with supporting leg 23.
In the present embodiment, motor drive end has transmission shaft, and transmission shaft and propeller 13 are rotatablely connected, to make propeller
13 rotations, the model of motor is kv950.
In the present embodiment, the rear of pedestal 18 is provided with attachment base 24 in the bottom surface of fuselage 11, in attachment base 24
Outside setting there are four connecting rod 21, the bottom surface of connecting rod 21 is provided with supporting leg 23, supporting leg 23 is internally provided with
Spring can buffer the inertia generated when unmanned plane decline by spring, unmanned plane is enable to consolidate when unmanned plane landing
It is parked in ground, the bottom surface of supporting leg 23 is provided with elastic cushion 22, the frictional force between unmanned plane and ground can be increased, make nothing
Man-machine can also stablize on uneven ground is parked, and the safety of unmanned plane is improved.
Further, the inside of supporting leg 23 offers the first cavity, and the first cavity is internally provided with spring, spring with
Supporting leg 23 is fixedly connected.
In the present embodiment, the inside of supporting leg 23 offers the first cavity, and the first cavity is internally provided with spring, spring
It is fixedly connected with supporting leg 23, it, can be used by spring buffer a part in unmanned plane decline due to the elasticity of spring itself
Property enables what unmanned plane consolidated to be parked in ground.
Further, the quantity of connecting rod 21 is four, and four connecting rods 21 are in cross arrangement in the outside of attachment base 24.
In the present embodiment, the quantity of connecting rod 21 is four, and four connecting rods 21 are in cross arrangement in the outer of attachment base 24
Side can increase the stability of object since the spread geometry of four connecting rods is special, to make the lowering means of unmanned plane more
What is added is firm.
Further, the quantity of mounting base 14 is four, and four mounting bases 14 are symmetrical along the longitudinal section of fuselage 11.
In the present embodiment, the quantity of mounting base 14 is four, and four mounting bases 14 are symmetrically divided along the longitudinal section of fuselage 11
Cloth, the top of four mounting bases 14 are equipped with propeller 13, so that unmanned plane is taken off by the rotation of propeller 13, also make in unmanned plane
Propeller 13 it is more stable.
Further, the inside of mounting base 14 offers the second cavity, and the second cavity is internally provided with motor, motor with
Mounting base 14 is fixedly connected.
In the present embodiment, the inside of mounting base 14 offers the second cavity, and the second cavity is internally provided with motor, motor
It is fixedly connected with mounting base 14, is connected to power supply by motor, make motor that propeller 13 be driven to rotate, so that unmanned plane is driven,
Power is provided to unmanned plane.
The working principle and process for using of the utility model: after the utility model installs, mapping unmanned plane is carried
To work-yard, user of service is monitored external environment, by remote control unmanned plane in the inside of unmanned aerial vehicle body 11
With battery, the motor inside mounting base 14 is connect with battery, and the transmission shaft at motor drive end is connect with propeller 13, into
And propeller 13 is driven to rotate, so that unmanned plane is flown to high-altitude, the bottom surface of unmanned aerial vehicle body 11 is provided with pedestal 18, the bottom of at
The bottom surface of seat 18 is equipped with camera 17, shoots the picture come by camera 17 and is transported in display screen, convenient for user
The picture come will be transmitted back to and be monitored analysis, the rear of pedestal 18 is provided with attachment base 24 in the bottom surface of fuselage 11,
The outside of attachment base 24 is provided with connecting rod 21, the bottom surface of connecting rod 21 is provided with supporting leg 23, the inside of supporting leg 23 is set
It is equipped with spring, the inertia that generates when can buffer unmanned plane decline by spring enables what unmanned plane consolidated to be parked in ground,
The bottom surface of supporting leg 23 is provided with elastic cushion 22, can increase the frictional force between unmanned plane and ground by elastic cushion 22, make
Unmanned plane can also be stablized on uneven ground to be parked, and after mapping unmanned plane completes work, closes power supply, user of service couple
Unmanned plane is detected, for use next time.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (5)
1. a kind of decline stable mapping unmanned plane, it is characterised in that: described including casing assembly (10) and fixation kit (20)
Casing assembly (10) includes fuselage (11), rotation button (12), propeller (13), mounting base (14), wing (15), fixing seat
(16), camera (17) and pedestal (18), the rotation button (12) are located above the left side of the fuselage (11), and with the machine
Body (11) rotation connection, the fixing seat (16) are located at the bottom surface of the rotation button (12), and fixed with the rotation button (12)
Connection, the wing (15) is located at the left outer surface of the rotation button (12), and is fixedly connected with the rotation button (12), institute
The left end that mounting base (14) are located at the wing (15) is stated, and is fixedly connected with the wing (15), propeller (13) position
It is rotatablely connected in the upper surface of the mounting base (14), and with the mounting base (14), the pedestal (18) is located at the fuselage
(11) bottom surface, and being fixedly connected with the fuselage (11), the camera (17) are located at the bottom surface of the pedestal (18), and with
Pedestal (18) rotation connection, the fuselage (11) includes locator (111), and the locator (111) is located at the fuselage
(11) upper surface, and be fixedly connected with the fuselage (11), the fixation kit (20) includes connecting rod (21), elastic cushion
(22), supporting leg (23) and attachment base (24), the attachment base (24) are located at the bottom surface of the fuselage (11) close to the pedestal
(18) rear, and be fixedly connected with the fuselage (11), the connecting rod (21) is located at the front surface of the attachment base (24),
And be fixedly connected with the attachment base (24), the supporting leg (23) is located at the bottom surface of the connecting rod (21), and with the company
Extension bar (21) is fixedly connected, and the elastic cushion (22) is located at the bottom surface of the supporting leg (23), and solid with the supporting leg (23)
Fixed connection.
A kind of decline stable mapping unmanned plane 2. according to claim 1, it is characterised in that: the supporting leg (23)
Inside offers the first cavity, and first cavity is internally provided with spring, and the spring and the supporting leg (23) are fixed
Connection.
A kind of decline stable mapping unmanned plane 3. according to claim 1, it is characterised in that: the connecting rod (21)
Quantity is four, and four connecting rods (21) are in outside of the cross arrangement in the attachment base (24).
A kind of decline stable mapping unmanned plane 4. according to claim 1, it is characterised in that: the mounting base (14)
Quantity is four, and four mounting bases (14) are symmetrical along the longitudinal section of the fuselage (11).
A kind of decline stable mapping unmanned plane 5. according to claim 1, it is characterised in that: the mounting base (14)
Inside offers the second cavity, and second cavity is internally provided with motor, and the motor and the mounting base (14) are fixed
Connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820490731.2U CN208325612U (en) | 2018-04-09 | 2018-04-09 | It is a kind of to decline stable mapping unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820490731.2U CN208325612U (en) | 2018-04-09 | 2018-04-09 | It is a kind of to decline stable mapping unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208325612U true CN208325612U (en) | 2019-01-04 |
Family
ID=64780733
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820490731.2U Expired - Fee Related CN208325612U (en) | 2018-04-09 | 2018-04-09 | It is a kind of to decline stable mapping unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208325612U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110406663A (en) * | 2019-07-30 | 2019-11-05 | 南京精微迅智能科技有限公司 | A kind of unmanned plane of the mapping based on Internet of Things |
-
2018
- 2018-04-09 CN CN201820490731.2U patent/CN208325612U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110406663A (en) * | 2019-07-30 | 2019-11-05 | 南京精微迅智能科技有限公司 | A kind of unmanned plane of the mapping based on Internet of Things |
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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: 20190104 Termination date: 20200409 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |