CN110481773A - A kind of split type unmanned plane of VTOL - Google Patents
A kind of split type unmanned plane of VTOL Download PDFInfo
- Publication number
- CN110481773A CN110481773A CN201810462895.9A CN201810462895A CN110481773A CN 110481773 A CN110481773 A CN 110481773A CN 201810462895 A CN201810462895 A CN 201810462895A CN 110481773 A CN110481773 A CN 110481773A
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- China
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- fuselage
- vtol
- wing
- unmanned plane
- rotor
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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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C37/00—Convertible aircraft
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of split type unmanned planes of VTOL, including fuselage, port wing, starboard wing, left VTOL mechanism and right VTOL mechanism；Fuselage is bilateral symmetry；Port wing, starboard wing are parallel with fuselage to be connected；It includes vertically arranged plate structure that left and right vertical, which plays descending mechanism, and the bottom level of plate structure connects rod-like structure, and the front-end and back-end of rod-like structure install two attachment devices, install rotor in two attachment devices；At least one of two attachment devices use Bendable ink attachment device, and rotor can be made parallel or vertical with fuselage.When unmanned plane takes off, rotor is parallel with fuselage, and fuselage rises in parallel, 90 ° of rotor wing rotation, vertical with fuselage after reaching certain height, carries out cruising flight.Under the premise of not changing fuselage state, VTOL function is realized.Also, rotor part can be removed according to demand, realize the conversion between vertical take-off and landing drone and fixed-wing unmanned plane.
Description
Technical field
The present invention relates to air vehicle technique field, more particularly to it is a kind of can VTOL split type unmanned plane.
Background technique
The fuselage of traditional unmanned plane is fixedly connected with wing, and the span adds winglet or tail close to there is one meter or so
The wing is perpendicular to fuselage, so that unmanned plane is not in flat state, it is a three-dimensional structure, it is therefore desirable to design special packet
Unmanned plane is placed in vanning, these unmanned plane packing cases are bulky, it usually needs more than two people is carried, is needed vehicle or aviation
Can be carried out transport, and be also required in transportational process to wing carry out it is particular fixed, to avoid vibration cause unmanned aerial vehicle body with
Wing dislocation, leads to stress damage, adds additional the weight of packing case, so that unmanned plane is inconvenient to the shortcomings that carrying and carrying
It is especially prominent.
Applicant once provided in the Chinese invention patent application of Publication No. CN107628223A " a kind of split type
Unmanned plane ", although and vertical take-off and landing drone, this unmanned plane need to change the position of itself to realize cruising flight.
When taking off, unmanned plane is vertical, reaches certain height, and unmanned plane adjusts position, and 90 degree of rotation becomes parallel, hence into cruise
State of flight.Since this transformation of this unmanned plane needs global adaptation, algorithm is complicated and needs powerful power, can just make
It obtains unmanned plane to smoothly turn to, influence is caused for the cost of this unmanned plane, popularization and application and hinders.
Summary of the invention
In view of the above-mentioned problems, the present invention provides a kind of split type unmanned plane of VTOL, it is therefore an objective to not change fuselage state
And realize VTOL function.
To achieve the above object, the invention provides the following technical scheme:
A kind of split type unmanned plane of VTOL, including fuselage, port wing, starboard wing, left VTOL mechanism and the right side
VTOL mechanism；The fuselage is located at middle, is bilateral symmetry；The port wing is located at the left side of fuselage, with machine
Body connects in parallel；The starboard wing is located at the right side of fuselage, parallel with fuselage to connect；The left VTOL mechanism is located at fuselage
It is vertical with fuselage and port wing to connect between port wing；The right VTOL mechanism between fuselage and starboard wing, with
Fuselage and starboard wing vertically connect；The left VTOL mechanism, right VTOL mechanism include a vertically arranged plate
Structure, the bottom level of the plate structure are connected with a rod-like structure, and the front-end and back-end of the rod-like structure are installed respectively
There are two attachment device, rotor is separately installed in former and later two described attachment devices；In former and later two described attachment devices
At least one uses Bendable ink attachment device, and the Bendable ink attachment device can carry out 90 ° of rotations, keeps rotor and fuselage flat
Row keeps rotor vertical with fuselage.
Preferably, support leg is installed below the fuselage.
Preferably, the port wing, starboard wing rear movable aileron is installed.
Preferably, the port wing, starboard wing, left VTOL mechanism, right VTOL mechanism can it is tool-free manually with
The fuselage connection locking is dismantled from the fuselage.
Preferably, the port wing, starboard wing can without left VTOL mechanism, right VTOL mechanism and directly with
The streamlined transition in junction of the junction, starboard wing and fuselage of fuselage connection locking, port wing and fuselage.
Compared with prior art, the beneficial effects of the present invention are:
The split type unmanned plane of VTOL of the invention is assembled by five parts, and rotor is parallel with fuselage, is risen
When flying, fuselage rises in parallel, 90 ° of rotor wing rotation, vertical with fuselage after reaching certain height, carries out cruising flight.To
Under the premise of not changing fuselage state, VTOL function is realized.Also, rotor part can be removed according to demand,
Realize the conversion between vertical take-off and landing drone and fixed-wing unmanned plane.
Detailed description of the invention
Fig. 1 is overall structure figure of the invention.
Fig. 2 is decomposition chart of the invention.
Fig. 3 is local structural graph of the invention.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
As depicted in figs. 1 and 2, the split type unmanned plane of VTOL of the invention includes mainly five parts, is machine respectively
Body 1, port wing 2, starboard wing 3, left VTOL mechanism 4 and right VTOL mechanism 5.Wherein, fuselage 1 is located at middle,
For bilateral symmetry, the lower section of fuselage 1 is equipped with support leg 6, and port wing 2 is located at the left side of fuselage 1, parallel with fuselage 1 to connect
It connects；Starboard wing 3 is located at the right side of fuselage 1, connection parallel with fuselage 1；Left VTOL mechanism 4 be located at fuselage 1 and port wing 2 it
Between, with fuselage 1 and port wing 2 is vertical connect；Right VTOL mechanism 5 is between fuselage 1 and starboard wing 3, with fuselage 1 and the right side
Wing 3 vertically connects.Port wing 2, starboard wing 3 rear movable aileron 11 is installed.As shown in Fig. 2, fuselage 1 is left and right
End is respectively provided with connecting end surface；Port wing 2, starboard wing 3 end equally there is the consistent connecting end surface of shape, port wing 2 with
After the left end of fuselage 1 is connected by connecting end surface, starboard wing 3 is connected with the right end of fuselage 1 by connecting end surface, port wing
2 with 1 junction of fuselage, starboard wing 3 and the streamlined transition in 1 junction of fuselage.
As shown in Figures 2 and 3, left VTOL mechanism 4, right VTOL mechanism 5 include a vertically arranged plate
Structure 7, the bottom level of plate structure 7 are connected with a rod-like structure 8, and the front-end and back-end of rod-like structure 8 are separately installed with two
A attachment device 9 is separately installed with rotor 10 in former and later two attachment devices 9.In the present embodiment, rod-like structure 8 rear portion
Attachment device 9 is fixed attachment device, and the rotor 10 installed thereon is parallel with fuselage 1 always；And the company of 8 front of rod-like structure
Connection device 9 uses Bendable ink attachment device, and there are two stations for Bendable ink attachment device tool, can make rotation mounted thereto
The wing 10 rotates within the scope of 90 °, converts between rotor 10 is parallel with fuselage 1 and rotor 10 is vertical with fuselage 1.Unmanned plane takes off
When, it is parallel with fuselage 1 to control all rotors 10, provides vertical vector, and fuselage 1 rises in parallel；When unmanned plane reaches centainly
After height, control rotor 10 is vertical with fuselage 1 after being rotated by 90 °, and carries out cruising flight.To in the premise for not changing fuselage state
Under, realize VTOL function.In other optional schemes, the attachment device 9 of front, rear portion can also all be used reflexibie
Formula attachment device.
The adoptable assembly method of the present invention is, fuselage 1, port wing 2, starboard wing 3 connecting end surface on be respectively set
Having can mutually matched docking apparatus；It is inserted after the docking apparatus of port wing 2 to be passed through to the plate structure 7 of left VTOL mechanism 4
Enter fuselage 1 and it is corresponding to the docking apparatus of fuselage 1 cooperate, by the docking apparatus of starboard wing 3 pass through right VTOL mechanism 5 plate
It is inserted into fuselage 1 after shape structure 7 and corresponding to the docking apparatus of fuselage 1 cooperates.Port wing 2, starboard wing are made using plugging mode
3, left VTOL mechanism 4, right VTOL mechanism 5 tool-free manually quickly can connect with fuselage 1 and lock or from fuselage 1
Upper disassembly.A kind of above-mentioned assembly method for patching fixed structure only and being the present invention and enumerated, can also use other fixed structures instead.
Also, left VTOL mechanism 4, right VTOL mechanism 5 can be removed according to demand, and by port wing 2, starboard wing 3
It directly is connect locking with fuselage 1, the present invention is converted to fixed-wing unmanned plane from vertical take-off and landing drone.
It can understand the above description of the embodiments is intended to facilitate those skilled in the art and apply this specially
Benefit.Person skilled in the art obviously easily can make various modifications to these embodiments, and described herein
General Principle is applied in other embodiments without having to go through creative labor.Therefore, the present invention is not limited to implementations here
Example, those skilled in the art's announcement according to the present invention, improvement and modification made without departing from the scope of the present invention all should be
Within protection scope of the present invention.
Claims (5)
1. a kind of split type unmanned plane of VTOL, it is characterised in that: including fuselage, port wing, starboard wing, left VTOL machine
Structure and right VTOL mechanism；The fuselage is located at middle, is bilateral symmetry；The port wing is located at a left side for fuselage
Side, it is parallel with fuselage to connect；The starboard wing is located at the right side of fuselage, parallel with fuselage to connect；The left VTOL mechanism
It is vertical with fuselage and port wing to connect between fuselage and port wing；The right VTOL mechanism is located at fuselage and right machine
It is vertical with fuselage and starboard wing to connect between the wing；The left VTOL mechanism, right VTOL mechanism include a vertical cloth
The plate structure set, the bottom level of the plate structure are connected with a rod-like structure, the front-end and back-end of the rod-like structure
Two attachment devices are separately installed with, are separately installed with rotor in former and later two described attachment devices；Former and later two described connections
At least one of device uses Bendable ink attachment device, and the Bendable ink attachment device can carry out 90 ° of rotations, make rotor
It is parallel with fuselage or keep rotor vertical with fuselage.
2. the split type unmanned plane of a kind of VTOL according to claim 1, it is characterised in that: pacify the lower section of the fuselage
Equipped with support leg.
3. the split type unmanned plane of a kind of VTOL according to claim 1, it is characterised in that: the port wing, right machine
The rear of the wing is equipped with movable aileron.
4. the split type unmanned plane of a kind of VTOL according to claim 1, it is characterised in that: the port wing, right machine
The wing, left VTOL mechanism, right VTOL mechanism tool-free can manually connect locking with the fuselage or from the fuselages
Upper disassembly.
5. the split type unmanned plane of a kind of VTOL according to claim 1, it is characterised in that: the port wing, right machine
The wing can directly connect locking without left VTOL mechanism, right VTOL mechanism with fuselage, the company of port wing and fuselage
Connect the streamlined transition in junction of place, starboard wing and fuselage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810462895.9A CN110481773A (en) | 2018-05-15 | 2018-05-15 | A kind of split type unmanned plane of VTOL |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810462895.9A CN110481773A (en) | 2018-05-15 | 2018-05-15 | A kind of split type unmanned plane of VTOL |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110481773A true CN110481773A (en) | 2019-11-22 |
Family
ID=68544899
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810462895.9A Pending CN110481773A (en) | 2018-05-15 | 2018-05-15 | A kind of split type unmanned plane of VTOL |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110481773A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113022848A (en) * | 2021-04-18 | 2021-06-25 | 上海尚实能源科技有限公司 | Wing passenger plane |
-
2018
- 2018-05-15 CN CN201810462895.9A patent/CN110481773A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113022848A (en) * | 2021-04-18 | 2021-06-25 | 上海尚实能源科技有限公司 | Wing passenger plane |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20191122 |