CN206782050U - Fixed-wing and more rotor one unmanned aerial vehicles - Google Patents
Fixed-wing and more rotor one unmanned aerial vehicles Download PDFInfo
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- CN206782050U CN206782050U CN201720506574.5U CN201720506574U CN206782050U CN 206782050 U CN206782050 U CN 206782050U CN 201720506574 U CN201720506574 U CN 201720506574U CN 206782050 U CN206782050 U CN 206782050U
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- wing
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- unmanned aerial
- propeller
- empennage
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Abstract
The utility model discloses a kind of fixed-wing and more rotor one unmanned aerial vehicles, has fixed-wing offline mode and more rotor flying patterns, it includes unmanned aerial vehicle body, more propeller aircrafts, fixed-wing empennage, fixed-wing wing and fixed-wing propeller.The detachably connected more propeller aircrafts of unmanned aerial vehicle body, the unmanned aerial vehicle body or be removably connected simultaneously wing empennage, fixed-wing wing and fixed-wing propeller.There is fixed-wing propeller fixing hole and fixed-wing empennage fixing hole respectively in the both ends end of the unmanned aerial vehicle body, symmetrically there is the mounting hole of fixed-wing wing first and the mounting hole of fixed-wing wing second in the relative two sides of the unmanned aerial vehicle body, symmetrically there is propeller aircraft mounting hole more than two groups in the side side of the unmanned aerial vehicle body.Can neatly assembly and disassembly turn into multi-rotor unmanned aerial vehicle or fixed-wing unmanned plane according to operating personnel's actual demand.
Description
Technical field
The utility model belongs to unmanned air vehicle technique field, and in particular to a kind of fixed-wing and more rotor one unmanned aerial vehicles.
Background technology
Existing civilian unmanned plane can be divided into fixed-wing unmanned plane and multi-rotor unmanned aerial vehicle, two kinds of nothing by wing classification
Man-machine mutual advantage and disadvantage.
Multi-rotor unmanned aerial vehicle relies primarily on lift caused by multiple rotors to balance the caused gravity of aircraft itself, passes through
Change the rotating speed of each rotor to control attitude of flight vehicle.Usually, multi-rotor unmanned aerial vehicle can realize hovering, or default
Speed interval in flown with arbitrary speed.
It is main as power, its lift that fixed-wing unmanned plane relies primarily on thrust caused by propeller or turbogenerator
Relative motion from wing and air.Usually, fixed-wing unmanned plane must produce certain relative velocity ability with air
Realize flight.Fixed-wing unmanned plane is compared with multi-rotor unmanned aerial vehicle, with flying speed is fast, carrying capacity is big, course continuation mileage length
The features such as, it is generally applied to need the empty occasion stopped stagnant for a long time, such as high-voltage line line walking, freeway surveillance and control etc..
Fixed-wing unmanned plane has a high requirement for landing place, and the large area operation efficiency of multi-rotor unmanned aerial vehicle compared with
It is low.To sum up, it is necessary to propose a kind of new unmanned plane of the respective advantage of combination fixed-wing and more rotors, overcome above-mentioned technology to be stranded
It is difficult.
Utility model content
The utility model is directed to the situation of prior art, there is provided a kind of fixed-wing and more rotor one unmanned aerial vehicles.
The utility model uses following technical scheme, the fixed-wing and more rotor one unmanned aerial vehicles, has fixed-wing
Offline mode and more rotor flying patterns, it includes unmanned aerial vehicle body, more propeller aircrafts, fixed-wing empennage, fixed-wing wing
With fixed-wing propeller, wherein：
The detachably connected more propeller aircrafts of unmanned aerial vehicle body, the unmanned aerial vehicle body or removably simultaneously
Be connected wing empennage, fixed-wing wing and fixed-wing propeller；
Respectively there is fixed-wing propeller fixing hole and fixed-wing empennage to fix in the both ends end of the unmanned aerial vehicle body
Hole, symmetrically there is the mounting hole of fixed-wing wing first and fixed-wing wing the in the relative two sides of the unmanned aerial vehicle body
Two mounting holes, symmetrically there is propeller aircraft mounting hole more than two groups in the side side of the unmanned aerial vehicle body.
According to above-mentioned technical proposal, more propeller aircrafts are provided with more propeller aircraft supports, more rotor spirals
Oar support is fixedly installed in more propeller aircraft mounting holes, and more propeller aircraft supports are provided with more propeller aircraft connecting rods,
More propeller aircraft connecting rods are fixedly connected on more propeller aircraft supports, and more propeller aircraft connecting rods are able to revolve more
Wing propeller bracket rotates for pivot.
According to above-mentioned technical proposal, the both ends end of more propeller aircraft connecting rods is respectively equipped with more propeller aircraft electricity
Machine and motor contact, more propeller aircraft motors positioned at both sides are fixedly connected on more rotor spiral shells by motor contact respectively
Oar connecting rod is revolved, more propeller aircraft motors electrically connect more propeller aircrafts and drive its rotation.
According to above-mentioned technical proposal, the fixed-wing empennage is provided with fixed-wing empennage fixed support, the fixed-wing empennage
Fixed support includes fixed-wing empennage connecting rod and fixed-wing empennage connector, and the both ends of the fixed-wing empennage connecting rod are fixed respectively
Unmanned aerial vehicle body and fixed-wing empennage connector are connected to, the both sides of the fixed-wing empennage connector are fixedly connected with fixation simultaneously
Wing empennage.
According to above-mentioned technical proposal, one end end of the fixed-wing empennage connecting rod is fixedly installed in positioned at unmanned aerial vehicle body
Fixed-wing empennage fixing hole, the other end end of the fixed-wing empennage connecting rod is fixedly installed in fixed-wing empennage connector,
The fixed-wing wing includes the first mounting rod and the second mounting rod, be fixedly installed in respectively the mounting hole of fixed-wing wing first and
The mounting hole of fixed-wing wing second, the fixed-wing propeller are fixedly installed in fixed-wing propeller fixing hole.
According to above-mentioned technical proposal, the unmanned aerial vehicle body is made of fiber carbon plate disposal molding.
According to above-mentioned technical proposal, the quantity of more propeller aircraft motors, motor contact and more propeller aircrafts
It is 4.
According to above-mentioned technical proposal, the aperture of the mounting hole of fixed-wing wing first is installed more than fixed-wing wing second
The aperture in hole.
According to above-mentioned technical proposal, more propeller aircraft connecting rods are made of fibrous carbon pipe disposal molding, described
More propeller aircraft supports are made of aluminium alloy disposal molding.
According to above-mentioned technical proposal, the fixed-wing empennage connecting rod is made of fibrous carbon pipe disposal molding, described solid
Determine wing empennage connector to be made of fiber carbon plate disposal molding.
Fixed-wing disclosed in the utility model and more rotor one unmanned aerial vehicles, its advantage are there is fixed-wing
Offline mode and more rotor flying patterns, as needed neatly assembly and disassembly turn into multi-rotor unmanned aerial vehicle or fixed-wing without
It is man-machine.
Brief description of the drawings
Fig. 1 is the structural representation of the unmanned aerial vehicle body of the utility model preferred embodiment.
Fig. 2 is the structural representation of more propeller aircrafts of the utility model preferred embodiment.
Fig. 3 is combination diagram of the unmanned aerial vehicle body with more propeller aircrafts of the utility model preferred embodiment.
Fig. 4 is the support bracket fastened structural representation of fixed-wing empennage of the utility model preferred embodiment.
Fig. 5 be the utility model preferred embodiment unmanned aerial vehicle body with fixed-wing empennage is support bracket fastened combines signal
Figure.
Fig. 6 is the overall structure diagram of the utility model preferred embodiment.
Fig. 7 is the function structure chart of the utility model preferred embodiment.
Reference includes：10- unmanned aerial vehicle bodies；11- fixed-wing propeller fixing holes；12- fixed-wings wing first is pacified
Fill hole；13- fixed-wings the second mounting hole of wing；14- fixed-wing empennage fixing holes；The more propeller aircraft mounting holes of 15-；20- is more
Propeller aircraft 20；The more propeller aircraft supports of 21-；The more propeller aircraft connecting rods 22 of 22-；The more propeller aircraft motors of 23-；
24- motor contacts；30- fixed-wing empennages；31- fixed-wing empennage fixed supports；32- fixed-wing empennage connecting rods；33- fixed-wings
Empennage connector；40- fixed-wing wings；50- fixed-wing propellers.
Embodiment
It is right with reference to preferred embodiment the utility model discloses a kind of fixed-wing and more rotor one unmanned aerial vehicles
Specific embodiment of the present utility model is further described.
Referring to Fig. 6 and Fig. 7 of accompanying drawing, the fixed-wing and more rotor one unmanned aerial vehicles have fixed-wing offline mode and
More rotor flying patterns, including unmanned aerial vehicle body 10, more propeller aircrafts 20, fixed-wing empennage 30, fixed-wing wing 40 and solid
Determine wing propeller 50, the detachably connected more propeller aircrafts 20 of unmanned aerial vehicle body 10, or the unmanned aerial vehicle body 10
Removably be connected wing empennage 30, fixed-wing wing 40 and fixed-wing propeller 50 simultaneously.When the unmanned aerial vehicle body 10
When connecting more propeller aircrafts 20, the utility model fixed-wing is changed into multi-rotor unmanned aerial vehicle with more rotor one unmanned aerial vehicles.
When the unmanned aerial vehicle body 10 is connected wing empennage 30, fixed-wing wing 40 and fixed-wing propeller 50 simultaneously, this practicality
New fixed-wing is changed into fixed-wing unmanned plane with more rotor one unmanned aerial vehicles, and assembly and disassembly are simple and easy to do, help to grasp
Make personnel and offline mode is flexibly selected according to use demand.
Referring to Fig. 1 of accompanying drawing, unmanned aerial vehicle body 10 is shown.To be adapted to fixed-wing offline mode and more rotor flyings simultaneously
Pattern, the unmanned aerial vehicle body 10 have some mounting holes and fixing hole simultaneously.Preferably, the two of the unmanned aerial vehicle body 10
End end has fixed-wing propeller fixing hole 11 and fixed-wing empennage fixing hole 14 respectively, in the phase of the unmanned aerial vehicle body 10
To two sides（For example, the leading flank shown in figure and trailing flank）Symmetrically with the first mounting hole of fixed-wing wing 12 and admittedly
The second mounting hole of the fixed wing machine wing 13.Preferably, in the side side of the unmanned aerial vehicle body 10（For example, the top side shown in figure
Face, it is not located at same side with above-mentioned fixed-wing wing first/second mounting hole）Symmetrically there is the peace of propeller aircraft more than two groups
Fill hole 15.
Further, the unmanned aerial vehicle body 10 is made of the fiber carbon plate disposal molding of high intensity, in light weight, anti-
Excellent performance is fallen, is easy to assembly and disassembly.
Referring to Fig. 2 of accompanying drawing, more propeller aircrafts 20 are shown.Preferably, more propeller aircrafts 20 are provided with more rotations
Wing propeller bracket 21, more propeller aircraft supports 21 are fixedly installed in more propeller aircrafts positioned at unmanned aerial vehicle body 10
Mounting hole 15.Wherein, more propeller aircraft supports 21 are provided with more propeller aircraft connecting rods 22, and more propeller aircrafts connect
Bar 22 is fixedly connected on more propeller aircraft supports 21 so that more propeller aircraft connecting rods 22 are with more propeller aircraft supports
21 be that pivot rotates.
Referring to Fig. 3 of accompanying drawing, the combining structure of unmanned aerial vehicle body 10 and more propeller aircrafts 20 is shown.Preferably, institute
The both ends end for stating more propeller aircraft connecting rods 22 is respectively equipped with more propeller aircraft motors 23 and motor contact 24, positioned at two
More propeller aircraft motors 23 of side are fixedly connected on more propeller aircraft connecting rods 22 by motor contact 24 respectively.It is described more
Propeller aircraft motor 23 electrically connects more propeller aircrafts 20, and drives its rotation, so as to produce in more rotor flying patterns
Under lift.Each more propeller aircraft motors 23 can simultaneously or selectively adjust turning for corresponding more propeller aircrafts 20
Speed, to control the UAV Attitude under more rotor flying patterns.
Further, the quantity of more propeller aircraft motors 23, motor contact 24 and more propeller aircrafts 20 is equal
For 4；More propeller aircraft connecting rods 22 are made of the fibrous carbon pipe disposal molding of high intensity；More rotor spirals
Oar support 21 is made of the aluminium alloy disposal molding of lightweight and high intensity.
Referring to Fig. 4 of accompanying drawing, the concrete structure of fixed-wing empennage fixed support 31 is shown.Preferably, the fixed-wing
Empennage 30 is provided with fixed-wing empennage fixed support 31, and the fixed-wing empennage fixed support 31 includes the He of fixed-wing empennage connecting rod 32
Fixed-wing empennage connector 33.
Referring to Fig. 5 and Fig. 6 of accompanying drawing, the combination knot of fixed-wing empennage fixed support 31 and fixed-wing empennage 30 is shown
Structure.Preferably, the both ends of the fixed-wing empennage connecting rod 32 are respectively fixedly connected with unmanned aerial vehicle body 10 and fixed-wing empennage company
Fitting 33, the both sides of the fixed-wing empennage connector 33 are fixedly connected with fixed-wing empennage 30 simultaneously.Preferably, the fixed-wing
One end end of empennage connecting rod 32 is fixedly installed in the fixed-wing empennage fixing hole 14 positioned at unmanned aerial vehicle body 10, the fixed-wing
The other end end of empennage connecting rod 32 is fixedly installed in fixed-wing empennage connector 33.Preferably, the fixed-wing wing 40 wraps
The first mounting rod and the second mounting rod are included, is fixedly installed in the mounting hole of fixed-wing wing first positioned at unmanned aerial vehicle body 10 respectively
12 and the second mounting hole of fixed-wing wing 13（The mounting hole of first mounting hole/second matches the mounting rod of the first mounting rod/second respectively
Caliber）.Preferably, the fixed-wing propeller that the fixed-wing propeller 50 is fixedly installed in positioned at unmanned aerial vehicle body 10 is fixed
Hole 11.
Further, for ease of counterweight and holding position, it is preferable that the aperture of first mounting hole of fixed-wing wing 12
More than the aperture of the second mounting hole of fixed-wing wing 13；The fixed-wing empennage 30 uses the EPO composite foams of high intensity once
Property shaping be made；The fixed-wing empennage connecting rod 32 is made of the fibrous carbon pipe disposal molding of high intensity；The fixed-wing
Empennage connector 33 is made of the fiber carbon plate disposal molding of high intensity.
For a person skilled in the art, the technical scheme described in foregoing embodiments can still be repaiied
Change, or equivalent substitution is carried out to which part technical characteristic, all within the spirit and principles of the utility model, that is made is any
Modification, equivalent substitution, improvement etc., should be included in the scope of protection of the utility model.
Claims (10)
1. a kind of fixed-wing and more rotor one unmanned aerial vehicles, it is characterised in that there is fixed-wing offline mode and more rotors to fly
Row mode, it includes unmanned aerial vehicle body, more propeller aircrafts, fixed-wing empennage, fixed-wing wing and fixed-wing propeller, its
In：
The detachably connected more propeller aircrafts of unmanned aerial vehicle body, the unmanned aerial vehicle body or are removably connected simultaneously
Fixed-wing empennage, fixed-wing wing and fixed-wing propeller；
There is fixed-wing propeller fixing hole and fixed-wing empennage fixing hole respectively in the both ends end of the unmanned aerial vehicle body,
The relative two sides of the unmanned aerial vehicle body symmetrically there is the mounting hole of fixed-wing wing first and fixed-wing wing second to pacify
Hole is filled, symmetrically there is propeller aircraft mounting hole more than two groups in the side side of the unmanned aerial vehicle body.
2. fixed-wing according to claim 1 and more rotor one unmanned aerial vehicles, it is characterised in that more rotor spirals
Oar is provided with more propeller aircraft supports, and more propeller aircraft supports are fixedly installed in more propeller aircraft mounting holes, described
More propeller aircraft supports are provided with more propeller aircraft connecting rods, and more propeller aircraft connecting rods are fixedly connected on more rotor spirals
Oar support, more propeller aircraft connecting rods are able to rotate by pivot of more propeller aircraft supports.
3. fixed-wing according to claim 2 and more rotor one unmanned aerial vehicles, it is characterised in that more rotor spirals
The both ends end of oar connecting rod is respectively equipped with more propeller aircraft motors and motor contact, more propeller aircrafts electricity positioned at both sides
Machine is fixedly connected on more propeller aircraft connecting rods by motor contact respectively, and more propeller aircraft motor electrical connections revolves
Wing propeller and drive its rotation.
4. fixed-wing according to claim 1 and more rotor one unmanned aerial vehicles, it is characterised in that the fixed-wing empennage
Provided with fixed-wing empennage fixed support, the fixed-wing empennage fixed support includes fixed-wing empennage connecting rod and fixed-wing empennage connects
Fitting, the both ends of the fixed-wing empennage connecting rod are respectively fixedly connected with unmanned aerial vehicle body and fixed-wing empennage connector, described
The both sides of fixed-wing empennage connector are fixedly connected with fixed-wing empennage simultaneously.
5. fixed-wing according to claim 4 and more rotor one unmanned aerial vehicles, it is characterised in that the fixed-wing empennage
One end end of connecting rod is fixedly installed in the fixed-wing empennage fixing hole positioned at unmanned aerial vehicle body, the fixed-wing empennage connecting rod
Other end end is fixedly installed in fixed-wing empennage connector, and the fixed-wing wing includes the first mounting rod and the second installation
Bar, the mounting hole of fixed-wing wing first and the mounting hole of fixed-wing wing second, the fixed-wing propeller are fixedly installed in respectively
It is fixedly installed in fixed-wing propeller fixing hole.
6. the fixed-wing and more rotor one unmanned aerial vehicles, its feature according to any claim in claim 1-5 exist
In the unmanned aerial vehicle body is made of fiber carbon plate disposal molding.
7. fixed-wing according to claim 3 and more rotor one unmanned aerial vehicles, it is characterised in that more rotor spirals
The quantity of oar motor, motor contact and more propeller aircrafts is 4.
8. fixed-wing according to claim 5 and more rotor one unmanned aerial vehicles, it is characterised in that the fixed-wing wing
The aperture of first mounting hole is more than the aperture of the mounting hole of fixed-wing wing second.
9. fixed-wing and more rotor one unmanned aerial vehicles according to any claim in claim 2 or 3, its feature
It is, more propeller aircraft connecting rods are made of fibrous carbon pipe disposal molding, and more propeller aircraft supports use
Aluminium alloy disposal molding is made.
10. fixed-wing and more rotor one unmanned aerial vehicles according to any claim in claim 4 or 5, it is special
Sign is that the fixed-wing empennage connecting rod is made of fibrous carbon pipe disposal molding, and the fixed-wing empennage connector uses
Fiber carbon plate disposal molding is made.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720506574.5U CN206782050U (en) | 2017-05-09 | 2017-05-09 | Fixed-wing and more rotor one unmanned aerial vehicles |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720506574.5U CN206782050U (en) | 2017-05-09 | 2017-05-09 | Fixed-wing and more rotor one unmanned aerial vehicles |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206782050U true CN206782050U (en) | 2017-12-22 |
Family
ID=60711068
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720506574.5U Expired - Fee Related CN206782050U (en) | 2017-05-09 | 2017-05-09 | Fixed-wing and more rotor one unmanned aerial vehicles |
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| CN (1) | CN206782050U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106965921A (en) * | 2017-05-09 | 2017-07-21 | 嘉兴安行信息科技有限公司 | Fixed-wing and the integral unmanned aerial vehicle of many rotors |
-
2017
- 2017-05-09 CN CN201720506574.5U patent/CN206782050U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106965921A (en) * | 2017-05-09 | 2017-07-21 | 嘉兴安行信息科技有限公司 | Fixed-wing and the integral unmanned aerial vehicle of many rotors |
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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: 20171222 Termination date: 20190509 |
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| CF01 | Termination of patent right due to non-payment of annual fee |