CN206345003U - Robot unmanned plane - Google Patents
Robot unmanned plane Download PDFInfo
- Publication number
- CN206345003U CN206345003U CN201621479243.9U CN201621479243U CN206345003U CN 206345003 U CN206345003 U CN 206345003U CN 201621479243 U CN201621479243 U CN 201621479243U CN 206345003 U CN206345003 U CN 206345003U
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- Prior art keywords
- wing
- gear
- unmanned plane
- robot
- shield
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Abstract
The utility model discloses robot unmanned plane, it is related to aircraft field, robot unmanned plane, including robot chassis, wing elevating mechanism, wing rotating mechanism, wing shield mechanism, robot sets organism on chassis, wing shield mechanism is provided with body, it is provided with to slide to be provided with wing elevating mechanism, wing elevating mechanism in liftway, liftway in body and is provided with wing rotating mechanism.The utility model robot unmanned plane, occupies little space with compact conformation, the characteristics of with DCB Specimen flight stability.
Description
Technical field
The utility model is related to aircraft field, specifically, is related to a kind of robot unmanned plane.
Background technology
Current civilian unmanned plane is widely used in taking photo by plane, fire-fighting, police investigation, land mapping, to ocean, high-tension line,
The condition of a disaster, meteorology etc. is monitored.Traditional unmanned plane is to use four axle rotors mostly, and this unmanned plane is in use, due to four
Scope is very big when rotor deploys, and is often unfavorable for flying in narrow scope, or easily encountering barrier occurs air crash.
The content of the invention
Technical problem to be solved in the utility model is：A kind of robot unmanned plane is provided, the device has structure tight
Gather and occupy little space, the characteristics of with DCB Specimen flight stability.
In order to solve the above technical problems, the technical solution of the utility model is：
Robot unmanned plane, including robot chassis, wing elevating mechanism, wing rotating mechanism, wing shield mechanism, institute
State and organism is set on robot chassis, be provided with wing shield mechanism, the body to be provided with to lift on the body and lead to
Slide to be provided with the wing elevating mechanism, the wing elevating mechanism in road, the liftway and be provided with the wing
Rotating mechanism.
Preferably, being provided with guide groove on the liftway, the wing elevating mechanism is stretched including hollow wing
The guide ledges being adapted with the guide groove are provided with shaft, the wing projecting shaft, the guide ledges are embedded in described
In guide groove, the lower end of the wing projecting shaft is connected by feed screw nut with leading screw, and the leading screw is with being arranged on the machine
The output shaft connection of spindle motor on people chassis, the bottom of the body is provided with some machine fans.
Preferably, the guide groove quantity is two, and opposing parallel setting；The machine fan quantity is four, and right
Title is arranged on underpart.
Preferably, the wing rotating mechanism includes the wing steering wheel for being arranged on the wing projecting shaft upper end and solid
The top rotary setting being scheduled in the gear fixed mount at the top of the wing projecting shaft, the gear fixed mount has upper rotor tooth
Bottom in wheel, the gear fixed mount, which is fixed with the middle of fixed helical gear, the gear fixed mount, is provided with swing pinion
Connecting shaft, the swing pinion connecting shaft middle part is fixedly connected with sprocket drive spindle, and the two ends of the gear shaft are connected to
One swing pinion, the top and bottom of the swing pinion are engaged with the upper rotor gear and fixed helical gear respectively, institute
The lower end for stating swing pinion connecting shaft is connected through the bottom of the gear fixed mount with the output shaft of the wing steering wheel, described
The upper end of swing pinion connecting shaft is connected through the top of the gear fixed mount with upper rotor connecting bushing, and the upper rotor connects
Spindle set lower, outer perimeter is enclosed provided with lower rotor connecting bushing, and the lower rotor connecting bushing lower end connects with the upper rotor gear
Connect, lower rotor wing disk and upper rotor wing disk be separately installed with the lower rotor connecting bushing and upper rotor connecting bushing,
Wing-folding device is provided with the lower rotor wing disk and the upper rotor wing disk.
Preferably, the wing-folding device includes wing-folding motor and folds gear, the folding motor connection
There is worm screw, the worm screw is engaged with the folding gear, and the folding gear is connected with wing.
Preferably, being provided with bearing between the lower rotor connecting bushing and the upper rotor connecting bushing.
Preferably, described wing shield mechanism includes being hinged on the wing shield above the body, the wing
Shield is connected by shield connecting rod with the middle part of the wing projecting shaft.
Preferably, being additionally provided with wing hole and shield company at the top of the body of the surrounding edge of the wing projecting shaft
Bar slotted eye.
Preferably, being additionally provided with the robot chassis on steering engine driver, the output shaft of the steering engine driver
Omnidirectional driving wheel is installed.
Preferably, the quantity of the steering engine driver is four.
Employ after above-mentioned technical proposal, the beneficial effects of the utility model are：
Due to robot unmanned plane, including robot chassis, wing elevating mechanism, wing rotating mechanism, wing shield machine
Structure, when robot unmanned plane storage, wing-folding can be stored in body by wing rotating mechanism by wing elevating mechanism again
It is interior, and the closing of wing shield mechanism so that compact overall structure occupies little space, when robot unmanned plane lets startup fly away,
Wing elevating mechanism will rise in wing slave body, and wing rotating mechanism deploys wing, starts flight.
Because the bottom of body is provided with some machine fans, when robot unmanned plane takes off, it can not only be controlled by machine fan
The horizontal direction of robot unmanned plane processed, power can also be provided in the horizontal direction.
Due to being separately installed with lower rotor wing disk and upper gyroplane on lower rotor connecting bushing and upper rotor connecting bushing
The direction of rotation of wing disk, lower rotor wing disk and upper rotor wing disk on the contrary, therefore robot unmanned plane has bispin wing structure,
Flight stability.
Due to wing-folding device include wing-folding motor and fold gear, wing-folding motor can by rotate forward and
Invert to control the expansion and folding of wing.
Due to being provided with bearing, therefore robot unmanned plane during flying between lower rotor connecting bushing and upper rotor connecting bushing
When avoid wing from shaking, fly it is more stable.
Because wing shield is connected by shield connecting rod with the middle part of wing projecting shaft, therefore pass through the liter of wing projecting shaft
Drop just can control the switch of wing shield.
In summary, the utility model robot unmanned plane solves four axle unmanned plane in the prior art, when four rotors
Scope is very big during expansion, is unfavorable for flying in narrow scope, or easily encounter the problem of air crash occurs for barrier.This reality
Novel robot unmanned plane is used, is occupied little space with compact conformation, the characteristics of with DCB Specimen flight stability.
Brief description of the drawings
Structural representation when Fig. 1 is the wing shield mechanism closing of the utility model robot unmanned plane；
Structural representation when Fig. 2 is the wing shield mechanism opening of the utility model robot unmanned plane；
Fig. 3 is the top view of the utility model robot unmanned plane；
Fig. 4 is Fig. 3 left view；
Fig. 5 is the sectional view on Fig. 3 middle B-B directions；
Fig. 6 is the structural representation of wing-folding device in Fig. 5；
Fig. 7 is the structural scheme of mechanism of Fig. 5 middle gears fixed mount and internal part；
In figure：1. robot chassis, 2. wing elevating mechanisms, 3. wing rotating mechanisms, 4. wing shield mechanisms, 5. machines
Body, 6. guide grooves, 7. steering engine drivers, 8. omnidirectional driving wheels, 9. wings, 10. wing projecting shafts, 11. guide ledges, 12.
Thick stick nut, 13. leading screws, 14. spindle motors, 15. wing steering wheels, 16. gear fixed mounts, rotor gear on 17., 18. fix oblique
Gear, 19. swing pinion connecting shafts, 20. gear shafts, rotor connecting bushing, 22. times rotor connecting bushings, 23. backspins on 21.
Wing wing disk, rotor wing disk on 24., 25. wing-folding devices, 26. wing-folding motors, 27. fold gears, 28. worm screws,
29. machine is fanned, 30 liftways, 31 wing shields, 32. shield connecting rods, 33. wing holes, 34. shield link slots.
Embodiment
The utility model is further illustrated with reference to the accompanying drawings and examples.
As shown in Figure 1, Figure 2, Fig. 5 is jointly shown, robot unmanned plane, including robot chassis 1, wing elevating mechanism 2, wing
Set on rotating mechanism 3, wing shield mechanism 4, robot chassis 1 on organism 5, body 5 and be provided with wing shield mechanism 4,
It is provided with to slide to be provided with wing elevating mechanism 2, wing elevating mechanism 2 on liftway 30, liftway 30 in body 5 and sets
It is equipped with wing rotating mechanism 3, body people chassis 1 and is additionally provided with four steering engine drivers 7, the output shaft of steering engine driver 7
Omnidirectional driving wheel 8 is installed.
When robot unmanned plane storage, wing rotating mechanism 3 can be folded wing 9 again by wing elevating mechanism 2
Be stored in body in, while wing shield mechanism 4 is closed so that compact overall structure occupies little space, when robot nobody
When machine lets startup fly away, wing elevating mechanism 2 will rise in the slave body of wing 9, and wing rotating mechanism 3 deploys wing 9, starts and flies
OK.
As Fig. 2, Fig. 3, Fig. 4, Fig. 5 jointly shown in, in the utility model, be provided with liftway 30 two it is relatively flat
Capable guide groove 6, wing elevating mechanism 2 includes being provided with and guide groove 6 on hollow wing projecting shaft 10, wing projecting shaft 10
The guide ledges 11 being adapted, guide ledges 11 are embedded in guide groove 6, the lower end of wing projecting shaft 10 by feed screw nut 12 with
Leading screw 13 is connected, and leading screw 13 is connected with being arranged on the output shaft of the One On The Chassis spindle motor 14 of robot, the bottom pair of body 5
Title is provided with four machine fans 29, and machine fan 29 not only can be with the horizontal direction of control machine people's unmanned plane, can also be in the horizontal direction
Upper offer power.
As Fig. 2, Fig. 5, Fig. 7 jointly shown in, in the utility model, wing rotating mechanism 3 include be arranged on wing stretching
In the wing steering wheel 15 of the upper end of axle 10 and the gear fixed mount 16 for being fixed on the top of wing projecting shaft 10, gear fixed mount 16
Top rotary setting has the bottom in upper rotor gear 17, gear fixed mount 16 to be fixed with fixed helical gear 18, and gear is fixed
Swing pinion connecting shaft 19 is provided with the middle of frame 16, the middle part of swing pinion connecting shaft 19 is fixedly connected with sprocket drive spindle 20, tooth
The two ends of wheel shaft 20 are connected to a swing pinion 21, the top and bottom of swing pinion 21 respectively with upper rotor gear 17
Engaged with fixed helical gear 18, the lower end of swing pinion connecting shaft 19 passes through bottom and the wing steering wheel 15 of gear fixed mount 16
Output shaft is connected, and the upper end of swing pinion connecting shaft 19 connects through the top of gear fixed mount 16 with upper rotor connecting bushing 21
Connect, the upper lower, outer perimeter of rotor connecting bushing 21, which is enclosed, is arranged with lower rotor connecting bushing 22, the lower lower end of rotor connecting bushing 22 with it is upper
Rotor gear 17 is connected, and the lower He of rotor wing disk 23 is separately installed with lower rotor connecting bushing 22 and upper rotor connecting bushing 21
Wing-folding device 25 is provided with upper rotor wing disk 24, lower rotor wing disk 23 and upper rotor wing disk 24.Due under
Lower rotor wing disk 23 and upper rotor wing disk 24 are separately installed with rotor connecting bushing 22 and upper rotor connecting bushing 21, under
The direction of rotation of rotor wing disk 23 and upper rotor wing disk 24 flies on the contrary, therefore robot unmanned plane has bispin wing structure
Row is stable.
As Fig. 5, Fig. 6 jointly shown in, in the utility model, wing-folding device 25 include wing-folding motor 26 and folding
Folded gear 27, folds motor 26 and is connected with 28, worm screw 28 engages with folding gear 27, fold gear 27 and be connected with wing 9, wing
The expansion and folding of wing 9 can be controlled by rotating and reverse by folding motor 26.
In the utility model, bearing is provided between lower rotor connecting bushing 22 and upper rotor connecting bushing 21, therefore
Avoid wing 9 to shake during robot unmanned plane during flying, fly more stable.
As shown in figure 5, in the utility model, wing shield mechanism 4 includes the wing shield 31 being hinged on body 5,
Wing shield 31 is hinged by the middle part of shield connecting rod 32 and wing projecting shaft 10.
As shown in Fig. 2 in the utility model, being also set up positioned at the top of body 5 of the surrounding edge of wing projecting shaft 10 organic
Foramen alare 33 and shield link slot 34.
Above-described embodiment is only the citing of the utility model embodiment, and protection domain of the present utility model is to weigh
The content that profit is required is defined, any equivalent transformation carried out based on technical inspiration of the present utility model, also in the utility model
Protection domain within.
Claims (10)
1. robot unmanned plane, including robot chassis, wing elevating mechanism, wing rotating mechanism, wing shield mechanism, it is special
Levy and be：Set on the robot chassis and wing shield mechanism is provided with organism, the body, set in the body
Have to slide to be provided with the wing elevating mechanism, the wing elevating mechanism in liftway, the liftway and be provided with
The wing rotating mechanism.
2. robot unmanned plane as claimed in claim 1, it is characterised in that：Guide groove, institute are provided with the liftway
Stating wing elevating mechanism includes being provided with what is be adapted with the guide groove on hollow wing projecting shaft, the wing projecting shaft
Guide ledges, the guide ledges are embedded in the guide groove, and the lower end of the wing projecting shaft passes through feed screw nut and leading screw
Connection, the output shaft of spindle motor of the leading screw with being arranged on the robot chassis is connected, and the bottom of the body is set
It is equipped with some machine fans.
3. robot unmanned plane as claimed in claim 2, it is characterised in that：The guide groove quantity is two, and relatively flat
Row is set；The machine fan quantity is four, and is symmetricly set on underpart.
4. robot unmanned plane as claimed in claim 2, it is characterised in that：The wing rotating mechanism is described including being arranged on
The wing steering wheel of wing projecting shaft upper end and the gear fixed mount being fixed at the top of the wing projecting shaft, the gear are fixed
Top rotary setting in frame has the bottom in upper rotor gear, the gear fixed mount to be fixed with fixed helical gear, described
Swing pinion connecting shaft is provided with the middle of gear fixed mount, the swing pinion connecting shaft middle part is fixedly connected with gear
Axle, the two ends of the gear shaft are connected to a swing pinion, the top and bottom of the swing pinion respectively with it is described
Upper rotor gear and the engagement of fixed helical gear, the lower end of the swing pinion connecting shaft through the bottom of the gear fixed mount with
The output shaft connection of the wing steering wheel, the upper end of the swing pinion connecting shaft passes through the top of gear fixed mount and upper rotor
Connecting bushing is connected, and the upper rotor connecting bushing lower, outer perimeter, which is enclosed, is arranged with lower rotor connecting bushing, the lower rotor connection
Axle sleeve lower end is connected with the upper rotor gear, is separately installed with down on the lower rotor connecting bushing and upper rotor connecting bushing
Wing-folding is provided with rotor wing disk and upper rotor wing disk, the lower rotor wing disk and the upper rotor wing disk
Device.
5. robot unmanned plane as claimed in claim 4, it is characterised in that：The wing-folding device includes wing-folding electricity
Machine and fold gear, the folding motor connection has a worm screw, and the worm screw engage with the folding gear, it is described fold gear and
Wing is connected.
6. robot unmanned plane as claimed in claim 4, it is characterised in that：The lower rotor connecting bushing and the upper rotor
Bearing is provided between connecting bushing.
7. robot unmanned plane as claimed in claim 2, it is characterised in that：Described wing shield mechanism includes being hinged on institute
The wing shield on body is stated, the wing shield is connected by shield connecting rod with the wing projecting shaft.
8. robot unmanned plane as claimed in claim 7, it is characterised in that：Described in surrounding edge positioned at the wing projecting shaft
Wing hole and shield link slot are additionally provided with the top of body.
9. the robot unmanned plane as described in any one of claim 1 to 8, it is characterised in that：Also set on the robot chassis
It is equipped with steering engine driver, the output shaft of the steering engine driver and omnidirectional driving wheel is installed.
10. robot unmanned plane as claimed in claim 9, it is characterised in that：The quantity of the steering engine driver is four.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621479243.9U CN206345003U (en) | 2016-12-30 | 2016-12-30 | Robot unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621479243.9U CN206345003U (en) | 2016-12-30 | 2016-12-30 | Robot unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206345003U true CN206345003U (en) | 2017-07-21 |
Family
ID=59319750
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621479243.9U Withdrawn - After Issue CN206345003U (en) | 2016-12-30 | 2016-12-30 | Robot unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206345003U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106741911A (en) * | 2016-12-30 | 2017-05-31 | 歌尔股份有限公司 | Robot unmanned plane |
-
2016
- 2016-12-30 CN CN201621479243.9U patent/CN206345003U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106741911A (en) * | 2016-12-30 | 2017-05-31 | 歌尔股份有限公司 | Robot unmanned plane |
| CN106741911B (en) * | 2016-12-30 | 2023-10-13 | 歌尔股份有限公司 | Unmanned plane of robot |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20170721 Effective date of abandoning: 20231013 |
|
| AV01 | Patent right actively abandoned |
Granted publication date: 20170721 Effective date of abandoning: 20231013 |