CN106965921A - Fixed-wing and the integral unmanned aerial vehicle of many rotors - Google Patents
Fixed-wing and the integral unmanned aerial vehicle of many rotors Download PDFInfo
- Publication number
- CN106965921A CN106965921A CN201710320860.7A CN201710320860A CN106965921A CN 106965921 A CN106965921 A CN 106965921A CN 201710320860 A CN201710320860 A CN 201710320860A CN 106965921 A CN106965921 A CN 106965921A
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- wing
- fixed
- many
- aerial vehicle
- unmanned aerial
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- 238000000465 moulding Methods 0.000 claims description 15
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 12
- 229910052799 carbon Inorganic materials 0.000 claims description 12
- 239000000835 fiber Substances 0.000 claims description 6
- 229910000838 Al alloy Inorganic materials 0.000 claims description 3
- 230000005611 electricity Effects 0.000 claims description 2
- 230000009187 flying Effects 0.000 abstract description 8
- 238000010586 diagram Methods 0.000 description 3
- 239000007787 solid Substances 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 238000006467 substitution reaction Methods 0.000 description 2
- 239000002131 composite material Substances 0.000 description 1
- 239000006260 foam Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C37/00—Convertible aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/25—Fixed-wing aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/10—Wings
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/13—Propulsion using external fans or propellers
- B64U50/14—Propulsion using external fans or propellers ducted or shrouded
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of fixed-wing and the integral unmanned aerial vehicle of many rotors, with fixed-wing offline mode and many rotor flying patterns, it includes unmanned aerial vehicle body, many propeller aircrafts, fixed-wing empennage, fixed-wing wing and fixed-wing propeller.The detachably connected many 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 two 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 according to operating personnel's actual demand neatly assembly and disassembly turn into multi-rotor unmanned aerial vehicle or fixed-wing unmanned plane.
Description
Technical field
The invention belongs to unmanned air vehicle technique field, and in particular to a kind of fixed-wing and the integral unmanned aerial vehicle of many rotors.
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 the lift of multiple rotors generations to balance the gravity of aircraft itself generation, 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.
Fixed-wing unmanned plane relies primarily on the thrust of propeller or turbogenerator generation as power, and its lift is main
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 is long
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.
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 many rotors, above-mentioned technology is overcome to be stranded
It is difficult.
The content of the invention
There is provided a kind of fixed-wing and the integral unmanned aerial vehicle of many rotors for situation of the invention for prior art.
The present invention uses following technical scheme, the fixed-wing and the integral unmanned aerial vehicle of many rotors, with fixed-wing flight
Pattern and many rotor flying patterns, it includes unmanned aerial vehicle body, many propeller aircrafts, fixed-wing empennage, fixed-wing wing and consolidated
Determine wing propeller, wherein：
The detachably connected many propeller aircrafts of unmanned aerial vehicle body, the removably unmanned aerial vehicle body or connection 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 two 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.
According to above-mentioned technical proposal, many propeller aircrafts are provided with many propeller aircraft supports, many rotor spirals
Oar support is fixedly installed in many propeller aircraft mounting holes, and many propeller aircraft supports are provided with many propeller aircraft connecting rods,
Many propeller aircraft connecting rods are fixedly connected on many propeller aircraft supports, and many propeller aircraft connecting rods are able to revolve more
Wing propeller bracket rotates for pivot.
According to above-mentioned technical proposal, the two ends end of many propeller aircraft connecting rods is respectively equipped with many propeller aircraft electricity
Machine and motor contact, many propeller aircraft motors positioned at both sides are fixedly connected on many rotor spiral shells by motor contact respectively
Oar connecting rod is revolved, many propeller aircraft motors electrically connect many propeller aircrafts and drive it to rotate.
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 two 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 include 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 is 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 many propeller aircraft motors, motor contact and many 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, many propeller aircraft connecting rods are made of fibrous carbon pipe disposal molding, described
Many 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 by the invention is with the integral unmanned aerial vehicle of many rotors, its advantage, with fixed-wing flight
Pattern and many rotor flying patterns, as needed neatly assembly and disassembly turn into multi-rotor unmanned aerial vehicle or fixed-wing nobody
Machine.
Brief description of the drawings
Fig. 1 is the structural representation of the unmanned aerial vehicle body of the preferred embodiment of the present invention.
Fig. 2 is the structural representation of many propeller aircrafts of the preferred embodiment of the present invention.
Fig. 3 is combination diagram of the unmanned aerial vehicle body with many propeller aircrafts of the preferred embodiment of the present invention.
Fig. 4 is the support bracket fastened structural representation of fixed-wing empennage of the preferred embodiment of the present invention.
Fig. 5 is the unmanned aerial vehicle body and the support bracket fastened combination diagram of fixed-wing empennage of the preferred embodiment of the present invention.
Fig. 6 is the overall structure diagram of the preferred embodiment of the present invention.
Fig. 7 is the function structure chart of the preferred embodiment of the present invention.
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 many propeller aircraft mounting holes of 15-；20- is more
Propeller aircraft 20；The many propeller aircraft supports of 21-；The many propeller aircraft connecting rods 22 of 22-；The many 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
The invention discloses a kind of fixed-wing and the integral unmanned aerial vehicle of many rotors, with reference to preferred embodiment, to this hair
Bright embodiment is further described.
Referring to Fig. 6 and Fig. 7 of accompanying drawing, the integral unmanned aerial vehicle of the fixed-wing and many rotors have fixed-wing offline mode and
Many rotor flying patterns, including unmanned aerial vehicle body 10, many propeller aircrafts 20, fixed-wing empennage 30, fixed-wing wing 40 and solid
Determine wing propeller 50, the detachably connected many 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 many propeller aircrafts 20, fixed-wing of the present invention is changed into multi-rotor unmanned aerial vehicle with the integral unmanned aerial vehicle of many rotors.Work as institute
Unmanned aerial vehicle body 10 is stated while when the wing empennage 30 that is connected, fixed-wing wing 40 and fixed-wing propeller 50, the present invention is fixed
The wing is changed into fixed-wing unmanned plane with the integral unmanned aerial vehicle of many rotors, and assembly and disassembly are simple and easy to do, contribute to operating personnel's root
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 many rotor flyings simultaneously
Pattern, the unmanned aerial vehicle body 10 has some mounting holes and fixing hole simultaneously.Preferably, the two of the unmanned aerial vehicle body 10
Hold end that there is 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 and trailing flank that are shown in figure）Symmetrically there is the first mounting hole of fixed-wing wing 12 and solid
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, is not located at same side with above-mentioned fixed-wing wing first/second mounting hole）Symmetrically there is propeller aircraft more than two groups to pacify
Fill hole 15.
Further, the unmanned aerial vehicle body 10 is made of the fiber carbon plate disposal molding of high intensity, lightweight, anti-
Excellent performance is fallen, is easy to assembly and disassembly.
Referring to Fig. 2 of accompanying drawing, many propeller aircrafts 20 are shown.Preferably, many propeller aircrafts 20 are provided with many rotations
Wing propeller bracket 21, many propeller aircraft supports 21 are fixedly installed in many propeller aircrafts positioned at unmanned aerial vehicle body 10
Mounting hole 15.Wherein, many propeller aircraft supports 21 are provided with many propeller aircraft connecting rods 22, and many propeller aircrafts connect
Bar 22 is fixedly connected on many propeller aircraft supports 21 so that many propeller aircraft connecting rods 22 are with many 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 many propeller aircrafts 20 is shown.Preferably, institute
The two ends end for stating many propeller aircraft connecting rods 22 is respectively equipped with many propeller aircraft motors 23 and motor contact 24, positioned at two
Many propeller aircraft motors 23 of side are fixedly connected on many propeller aircraft connecting rods 22 by motor contact 24 respectively.It is described many
Propeller aircraft motor 23 electrically connects many propeller aircrafts 20, and drives it to rotate, so as to produce in many rotor flying patterns
Under lift.Each many propeller aircraft motor 23 can simultaneously or selectively adjust turning for corresponding many propeller aircrafts 20
Speed, to control the UAV Attitude under many rotor flying patterns.
Further, the quantity of many propeller aircraft motors 23, motor contact 24 and many propeller aircrafts 20 is equal
For 4；Many propeller aircraft connecting rods 22 are made of the fibrous carbon pipe disposal molding of high intensity；Many 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 two 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 is wrapped
The first mounting rod and the second mounting rod are included, the mounting hole of fixed-wing wing first positioned at unmanned aerial vehicle body 10 is fixedly installed in 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, within the spirit and principles of the invention, that is made any repaiies
Change, equivalent substitution, improvement etc., should be included in protection scope of the present invention.
Claims (10)
1. a kind of fixed-wing and the integral unmanned aerial vehicle of many rotors, it is characterised in that fly with fixed-wing offline mode and many rotors
Row mode, it includes unmanned aerial vehicle body, many propeller aircrafts, fixed-wing empennage, fixed-wing wing and fixed-wing propeller, its
In：
The detachably connected many propeller aircrafts of unmanned aerial vehicle body, the removably unmanned aerial vehicle body or connection 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 two 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 the integral unmanned aerial vehicle of many rotors, it is characterised in that many rotor spirals
Oar is provided with many propeller aircraft supports, and many propeller aircraft supports are fixedly installed in many propeller aircraft mounting holes, described
Many propeller aircraft supports are provided with many propeller aircraft connecting rods, and many propeller aircraft connecting rods are fixedly connected on many rotor spirals
Oar support, many propeller aircraft connecting rods are able to rotate by pivot of many propeller aircraft supports.
3. fixed-wing according to claim 2 and the integral unmanned aerial vehicle of many rotors, it is characterised in that many rotor spirals
The two ends end of oar connecting rod is respectively equipped with many propeller aircraft motors and motor contact, many propeller aircrafts electricity positioned at both sides
Machine is fixedly connected on many propeller aircraft connecting rods by motor contact respectively, and many propeller aircraft motor electrical connections revolves
Wing propeller and it is driven to rotate.
4. fixed-wing according to claim 1 and the integral unmanned aerial vehicle of many rotors, 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 two 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 the integral unmanned aerial vehicle of many rotors, 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 second and installed
Bar, is fixedly installed in the mounting hole of fixed-wing wing first and the mounting hole of fixed-wing wing second, the fixed-wing propeller respectively
It is fixedly installed in fixed-wing propeller fixing hole.
6. fixed-wing and the integral unmanned aerial vehicle of many rotors according to any claim in claim 1-5, its feature exist
In the unmanned aerial vehicle body is made of fiber carbon plate disposal molding.
7. fixed-wing according to claim 3 and the integral unmanned aerial vehicle of many rotors, it is characterised in that many rotor spirals
The quantity of oar motor, motor contact and many propeller aircrafts is 4.
8. fixed-wing according to claim 5 and the integral unmanned aerial vehicle of many rotors, 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 the integral unmanned aerial vehicle of many rotors, its feature according to any claim in claim 2 or 3
It is, many propeller aircraft connecting rods are made of fibrous carbon pipe disposal molding, many propeller aircraft supports are used
Aluminium alloy disposal molding is made.
10. fixed-wing and the integral unmanned aerial vehicle of many rotors according to any claim in claim 4 or 5, it is special
Levy and be, the fixed-wing empennage connecting rod is made of fibrous carbon pipe disposal molding, the fixed-wing empennage connector is used
Fiber carbon plate disposal molding is made.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710320860.7A CN106965921A (en) | 2017-05-09 | 2017-05-09 | Fixed-wing and the integral unmanned aerial vehicle of many rotors |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710320860.7A CN106965921A (en) | 2017-05-09 | 2017-05-09 | Fixed-wing and the integral unmanned aerial vehicle of many rotors |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106965921A true CN106965921A (en) | 2017-07-21 |
Family
ID=59331218
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710320860.7A Pending CN106965921A (en) | 2017-05-09 | 2017-05-09 | Fixed-wing and the integral unmanned aerial vehicle of many rotors |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106965921A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
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| WO2021078267A1 (en) * | 2019-10-23 | 2021-04-29 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle |
| CN112977797A (en) * | 2021-02-23 | 2021-06-18 | 四川大学 | High-strength light detachable fixed-wing scouting and hitting unmanned aerial vehicle |
| CN113682475A (en) * | 2021-08-27 | 2021-11-23 | 沈阳无距科技有限公司 | Modularization unmanned aerial vehicle |
| WO2025152968A1 (en) * | 2024-01-15 | 2025-07-24 | 深圳市旗客智能技术有限公司 | Two-in-one convertible unmanned aerial vehicle |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2021078267A1 (en) * | 2019-10-23 | 2021-04-29 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle |
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| US12187467B2 (en) * | 2019-10-23 | 2025-01-07 | Autel Robotics Co., Ltd. | Convertible unmanned aerial vehicle |
| CN112977797A (en) * | 2021-02-23 | 2021-06-18 | 四川大学 | High-strength light detachable fixed-wing scouting and hitting unmanned aerial vehicle |
| CN112977797B (en) * | 2021-02-23 | 2022-02-01 | 四川大学 | High-strength light detachable fixed-wing scouting and hitting unmanned aerial vehicle |
| CN113682475A (en) * | 2021-08-27 | 2021-11-23 | 沈阳无距科技有限公司 | Modularization unmanned aerial vehicle |
| WO2025152968A1 (en) * | 2024-01-15 | 2025-07-24 | 深圳市旗客智能技术有限公司 | Two-in-one convertible unmanned aerial vehicle |
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Application publication date: 20170721 |