CN207045716U - A kind of five-pointed star type multi-rotor aerocraft - Google Patents
A kind of five-pointed star type multi-rotor aerocraft Download PDFInfo
- Publication number
- CN207045716U CN207045716U CN201720827144.3U CN201720827144U CN207045716U CN 207045716 U CN207045716 U CN 207045716U CN 201720827144 U CN201720827144 U CN 201720827144U CN 207045716 U CN207045716 U CN 207045716U
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- pointed star
- star type
- lower house
- rotor aerocraft
- upper shell
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Abstract
The utility model discloses a kind of five-pointed star type multi-rotor aerocraft, including five-pointed star type fuselage, five-pointed star type fuselage is connected through a screw thread by upper shell and lower house and formed, threaded rod is provided with upper shell and lower house, the winged control plate of regular pentagon is provided between upper shell and lower house, and the connecting pole for being threaded hole for flying to set on five angles that control plate passes through upper and lower surface is connected with shaft, and power set are provided with five angles of upper casing external surface；The utility model solves the problems, such as existing MAV stability difference and purposes is single, by the way that upper-lower casing is designed into five-pointed star type becomes the multi-rotor aerocraft of the cantilever of five axle five, it is effectively improved the stability of aircraft, the design of five-pointed star type can be put as handicraft, and all electronic equipments all wrap up in abdomen within housing, realize compact-sized, aircraft small volume itself, relatively light, its is simple to operate and flexible.
Description
Technical field
The utility model belongs to aeromodelling aerocraft technical field, is related to a kind of five-pointed star type multi-rotor aerocraft.
Background technology
Multi-rotor aerocraft is also referred to as Multi-axis aircraft, is a kind of rotor craft having more than two rotor shafts, more rotations
The mobility of rotor aircraft is torsion by changing different rotors and rotating speed to realize.At present, common multi-rotor unmanned aerial vehicle
Model plane are the rotor MAVs of four axle four, are only capable of using as aeromodelling aerocraft, and purposes is more single, and stability has one
Fixed limitation.
As can be seen here, it is highly desirable to design a kind of multi-rotor aerocraft model plane, can both improves aircraft flight stability,
Put in not flight but also as handicraft, increase the purposes of minute vehicle.
Utility model content
The purpose of this utility model is to provide a kind of five-pointed star type multi-rotor aerocraft, and it is steady to solve existing MAV
The problem of qualitative poor.
The utility model is the technical scheme adopted is that a kind of five-pointed star type multi-rotor aerocraft, including five-pointed star type machine
Body, five-pointed star type fuselage are connected through a screw thread by upper shell and lower house and formed, and water is connected between upper shell and lower house
The flat winged control plate in regular pentagon set；Fly to be provided with flight control system on the upper surface of control plate, fly the lower surface of control plate
Battery container is connected between center and lower house center, power set are provided with five angles of upper casing external surface.
The characteristics of the utility model, also resides in：
Each power set include motor, propeller and motor assembly；
Motor assembly include slurry set, be arranged on slurry set top slurry cap and be arranged on slurry set bottom slurry folder, motor and
Slurry folder connection, propeller are arranged at slurry and put and be located at slurry cap between slurry folder；Upper casing is fixed in motor lower end by mounting seat
On any angle of external surface.
Each power set are also associated with arc blade protective cover, and blade protective cover is connected to cylinder by two connecting rods
On the fastener of shape, fastener is connected in the neck set in mounting seat, and the inner surface of fastener is close to the appearance of motor
Face, and the height of fastener will be less than motor.
V-groove a is provided with the outer surface of five cantilevers of upper shell, coloured ribbon lamp a is provided with each V-groove a,
Multiple heat emission hole a are provided with around each V-groove a；The inner surface of five cantilevers of upper shell is respectively connected with threaded rod a,
Upper shell is connected by all threaded rod a with flying control plate upper surface.
V-groove b is provided with the outer surface of five cantilevers of lower house, coloured ribbon lamp b is embedded with each V-groove b, under
The inner surface of five cantilevers of housing is respectively connected with threaded rod b；Lower house is connected by all threaded rod b with flying control plate lower surface
Connect.
Camera of taking photo by plane is connected with the adjacent cantilever of lower casing external surface any two.
Base buckle is provided with five cantilevers of lower house, lower house passes through all base buckles and pentagonal prism shape bottom
Seat clamping.
Battery container is cylindric in being vertically arranged, and the top of battery container is connected with flying control plate, the bottom of battery container
The circular hole clamping set with lower house center, the bottom of battery container is provided with battery fixed card buckle, set on cell casing side wall
It is equipped with heat emission hole b.
The beneficial effects of the utility model are：
(1) multi-rotor aerocraft of the present utility model is in the multi-rotor aerocraft of five-pointed star type, the as cantilever of five axle five, can
To realize the VTOL of the parallel and helicopter of fixed-wing, for four-axle aircraft, its power is bigger, and stability is more
Good and outward appearance is also very novel, and parlor or bedroom can be placed in as handicraft in not flight；
(2) multi-rotor aerocraft of the present utility model have compact-sized, compact and it is in light weight the characteristics of, it is all
Electronic equipment is all arranged within the housing of the multi-rotor aerocraft, and all jacks are all distributed in the shell of the multi-rotor aerocraft
On external wall；Meanwhile the flying method of the multi-rotor aerocraft is simple, without too big take-off venue, it is not required that complicated
Operating technology can be achieved with indoor flight, and its is simple to operate and flexible, can investigate, take photo by plane in complex environment；
(3) multi-rotor aerocraft of the present utility model, using threaded connection between its upper and lower casing, belong to detachable
Connection, easy access；In the winged control plate for being internally provided with regular pentagon of the multi-rotor aerocraft, this flies control plate can be with upper lower casing
Body is stably connected with；Meanwhile the battery container upper surface of cylinder is fixed on to the lower surface for flying control plate, and by under the battery container
Surface is fixed in the circular hole that lower house center opens up, and the steadily of centre of gravity of whole multi-rotor aerocraft is so can guarantee that, in battery
The lower surface of housing sets buckle to can be used to self-contained battery, prevents battery from being dropped suddenly in flight way, in the side of battery container
Heat emission hole is set on wall, can power supply source and electronic equipment dissipating heat；
(4) multi-rotor aerocraft of the present utility model is also equipped with pentagonal prism shape base, and pentagonal prism shape base is with clamping
Form is fixed on the central axis of each cantilever of lower casing external surface, conveniently adds aircraft lands again while dismounting
Stability；
(5) multi-rotor aerocraft of the present utility model, arc blade protective cover is set on power set, by more than spiral shell
The outside back-up ring of rotation oar diameter plays a part of protecting propeller, adds the security performance of flight, and will not change of flight device
Aeroperformance；Blade protective cover realizes the tight fit with motor, an end of buckle by the open cylinders buckle of setting
The upper surface of five motor mounts of upper shell is close in face, and the overall height of buckle is set lower than motor, and can play prevents leaf
Slurry protective cover is tumbled the effect to come off；
(6) multi-rotor aerocraft of the present utility model, it is respectively arranged with five cantilevers of upper and lower two housings several
V-groove is additionally provided with cylindrical hole to place coloured ribbon lamp between the V-groove on upper shell, is radiated to fuselage；
(7) multi-rotor aerocraft of the present utility model, clamping shape is passed through on any two cantilever of lower casing external surface
Formula is respectively symmetrically fixed with camera of taking photo by plane, and relative to the unmanned plane of taking photo by plane of single camera, the double of the five-pointed star type aircraft take the photograph
As head is for the space that is greatly improved of finding a view of taking photo by plane, and two cameras are to be fixed on lower house using plug clamping form
On, convenient dismounting.
Brief description of the drawings
Fig. 1 is a kind of stereogram of five-pointed star type multi-rotor aerocraft of the utility model；
Fig. 2 is a kind of top view of five-pointed star type multi-rotor aerocraft of the utility model；
Fig. 3 is a kind of structural representation of five-pointed star type multi-rotor aerocraft internally-powered device of the utility model；
Fig. 4 is a kind of upper shell inner surface structure schematic diagram of five-pointed star type multi-rotor aerocraft of the utility model；
Fig. 5 is a kind of lower house inner surface structure schematic diagram of five-pointed star type multi-rotor aerocraft of the utility model；
Fig. 6 is a kind of upward view of five-pointed star type multi-rotor aerocraft of the utility model；
Fig. 7 is a kind of lower house of five-pointed star type multi-rotor aerocraft of the utility model and pentagonal prism shape base connection status
Schematic diagram.
In figure, 1. upper shells, 2. lower houses, 3. winged control plates, 4. battery containers, 5. connecting poles, 6. threaded rod a, 7. motors,
8. propeller, 9. motor assemblies, 10. blade protective covers, 11. fasteners, 12. coloured ribbon lamp a, 13. heat emission hole a, 14. pentagonal prism shapes
Base, 15. cameras, 16. base buckles, 17. heat emission hole b, 18. mounting seats, 19. necks, 20.V type grooves a, 21.V type groove b,
22. threaded rod b, 23. coloured ribbon lamp b.
Embodiment
The utility model is described in detail with reference to the accompanying drawings and detailed description.
A kind of five-pointed star type multi-rotor aerocraft of the utility model, as shown in figure 1, including five-pointed star type fuselage, this five jiaos
Star-like fuselage is connected by screw thread by upper shell 1 and lower house 2 and formed；
As shown in Fig. 2 it is provided with power set on five angles of the outer surface of upper shell 1；Each power set include
Motor 7, propeller 8 and motor assembly 9, as shown in figure 3, motor assembly 9 includes slurry set 9-2, is arranged on the slurry on slurry set 9-2 tops
The cap 9-1 and slurry folder 9-3 for being arranged on slurry set 9-2 bottoms, motor 7 are connected with slurry folder 9-3, and propeller 8 is arranged on slurry set 9-2
And between slurry cap 9-1 and slurry folder 9-3；The lower end of motor 7 is fixed on any angle of the outer surface of upper shell 1 by mounting seat 18
On；Each power set are also associated with arc blade protective cover 10, and blade protective cover 10 is connected to cylinder by two connecting rods
On the fastener 11 of shape, the fastener 11 is connected in the neck 19 set in mounting seat 18, and the inner surface of fastener 11 is close to
Height in the outer surface of motor 7, and fastener 11 will be less than motor 7；It is provided with the outer surface of 1 five cantilevers of upper shell
V-groove a20, coloured ribbon lamp a12 is provided with each V-groove a20, multiple radiatings are provided with around each V-groove a20
Hole a13；As shown in figure 4, the inner surface of five cantilevers of upper shell 1 is respectively connected with threaded rod a6；
As shown in figure 5, V-groove b21 is provided with the outer surface of 2 five cantilevers of lower house, in each V-groove b21
Coloured ribbon lamp b23 is embedded with, the inner surface of 2 five cantilevers of lower house is respectively connected with threaded rod b22；As shown in fig. 6, outside lower house 2
Camera 15 of taking photo by plane is connected with the adjacent cantilever of surface any two；Base is provided with 2 five cantilevers of lower house
Buckle 16, lower house 2 can be used for branch by all base buckles 16 and the clamping of pentagonal prism shape base 14, pentagonal prism shape base 14
Support whole five-pointed star type multi-rotor aerocraft；
As shown in fig. 7, being provided with the winged control plate 3 in regular pentagon between upper shell 1 and lower house 2, fly the upper table of control plate
Face and lower surface are provided with connecting pole 5 with threaded hole, and fly the upper surface of control plate 3 by connecting pole 5 and threaded rod a6 with
Upper shell 1 is threadedly coupled, and the lower surface for flying control plate 3 is connected by connecting pole 5 and threaded rod b22 with lower house 2, is further improved
The stability connected between winged control plate 3 and upper shell 1 and lower house 2, meanwhile, fly to be provided with flight on the upper surface of control plate 3
Control system, the lower surface center for flying control plate 3 are connected with the top of the battery container 4 of cylinder, and the bottom of battery container 4 is with
The circular port clamping that the center of housing 2 opens up, and the bottom of battery container 4 is provided with the buckle of self-contained battery, battery container 4
Heat emission hole b17 is provided with side wall.
By the above-mentioned means, a kind of five-pointed star type multi-rotor aerocraft of the utility model is by by upper shell 1, lower house 2
Be designed to five-pointed star type, become the multi-rotor aerocraft of the cantilever of five axle five, it is possible to achieve fixed-wing it is parallel with going straight up to
The VTOL of machine, bigger relative to the power of four-axle aircraft, stability is relatively more preferable, and novel appearance, all electricity
Sub- equipment all wraps up in abdomen within five-pointed star type fuselage, and all jacks are all disposed within five-pointed star type fuselage outer surface, has knot
The characteristics of structure is compact.Five-pointed star type multi-rotor aerocraft itself small volume of the present utility model, lighter weight；In addition, not
Parlor or bedroom can be placed on during flight, is put as handicraft, can effectively solve existing MAV stability
The problem of poor and purposes is single, meanwhile, this flying method, it is not necessary to too big take-off venue, it is not required that complicated operation
Technology, indoor flight can be achieved with by aircraft control system, outgoing to be convenient for carrying, its is simple to operate and flexible, therefore, can be with
Investigate, take photo by plane in complex environment.
Claims (8)
- A kind of 1. five-pointed star type multi-rotor aerocraft, it is characterised in that including five-pointed star type fuselage, the five-pointed star type fuselage by Upper shell (1) and lower house (2) are connected through a screw thread composition, and level is connected between the upper shell (1) and lower house (2) The winged control plate (3) in regular pentagon set；Flight control system is provided with the upper surface of the winged control plate (3), it is described to fly Battery container (4) is connected between the lower surface center of control plate (3) and lower house (2) center, upper shell (1) outer surface Power set are provided with five angles.
- A kind of 2. five-pointed star type multi-rotor aerocraft as claimed in claim 1, it is characterised in that each power set bag Include motor (7), propeller (8) and motor assembly (9)；The motor assembly (9) includes slurry set (9-2), the slurry cap (9-1) for being arranged on slurry set top and is arranged on slurry set (9-2) The slurry folder (9-3) of bottom, the motor (7) are connected with slurry folder (9-3), and the propeller (8) is arranged on slurry set (9-2) and position Between slurry cap (9-1) and slurry folder (9-3)；Upper shell (1) outer surface is fixed in motor (7) lower end by mounting seat (18) Any angle on.
- 3. a kind of five-pointed star type multi-rotor aerocraft as claimed in claim 2, it is characterised in that each power set are also Arc blade protective cover (10) is connected with, the blade protective cover (10) is connected to the fastener of cylinder by two connecting rods (11) on, the fastener (11) is connected in the neck (19) set in mounting seat (18), the interior table of the fastener (11) The outer surface of motor (7) is close in face, and the height of the fastener (11) will be less than motor (7).
- A kind of 4. five-pointed star type multi-rotor aerocraft as claimed in claim 1, it is characterised in that the upper shell (1) five V-groove a (20) is provided with the outer surface of cantilever, coloured ribbon lamp a (12) is provided with each V-groove a (20), Multiple heat emission hole a (13) are provided with around each V-groove a (20)；The inner surface of five cantilevers of the upper shell (1) Threaded rod a (6) is respectively connected with, the upper shell (1) is connected by all threaded rod a (6) with flying control plate (3) upper surface.
- A kind of 5. five-pointed star type multi-rotor aerocraft as claimed in claim 1, it is characterised in that the lower house (2) five V-groove b (21) is provided with the outer surface of cantilever, coloured ribbon lamp b (23) is embedded with each V-groove b (21), it is described The inner surface of (2) five cantilevers of lower house is respectively connected with threaded rod b (22)；The lower house (2) passes through all threaded rod b (22) it is connected with flying control plate (3) lower surface.
- A kind of 6. five-pointed star type multi-rotor aerocraft as claimed in claim 5, it is characterised in that lower house (2) appearance Camera of taking photo by plane (15) is connected with the adjacent cantilever of face any two.
- A kind of 7. five-pointed star type multi-rotor aerocraft as claimed in claim 5, it is characterised in that the lower house (2) five Base buckle (16) is provided with cantilever, the lower house (2) passes through all base buckles (16) and pentagonal prism shape base (14) clamping.
- 8. a kind of five-pointed star type multi-rotor aerocraft as claimed in claim 1, it is characterised in that the battery container (4) is in What is be vertically arranged is cylindric, the top of the battery container (4) with fly control plate (3) be connected, the bottom of the battery container (4) and The circular hole clamping that lower house (2) center is set, the bottom of the battery container (4) is provided with battery fixed card buckle, the battery Heat emission hole b (17) is provided with housing (4) side wall.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720827144.3U CN207045716U (en) | 2017-07-10 | 2017-07-10 | A kind of five-pointed star type multi-rotor aerocraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720827144.3U CN207045716U (en) | 2017-07-10 | 2017-07-10 | A kind of five-pointed star type multi-rotor aerocraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207045716U true CN207045716U (en) | 2018-02-27 |
Family
ID=61495256
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720827144.3U Expired - Fee Related CN207045716U (en) | 2017-07-10 | 2017-07-10 | A kind of five-pointed star type multi-rotor aerocraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207045716U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108674644A (en) * | 2018-05-21 | 2018-10-19 | 西北工业大学明德学院 | A kind of multi-rotor aerocraft with slave |
| CN116221256A (en) * | 2023-03-20 | 2023-06-06 | 北京工业大学 | Single-degree-of-freedom symmetrical seven-rod closed-loop extensible unit and regular five-pointed star-regular five-pointed prism conversion mechanism based on same |
-
2017
- 2017-07-10 CN CN201720827144.3U patent/CN207045716U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108674644A (en) * | 2018-05-21 | 2018-10-19 | 西北工业大学明德学院 | A kind of multi-rotor aerocraft with slave |
| CN116221256A (en) * | 2023-03-20 | 2023-06-06 | 北京工业大学 | Single-degree-of-freedom symmetrical seven-rod closed-loop extensible unit and regular five-pointed star-regular five-pointed prism conversion mechanism based on same |
| CN116221256B (en) * | 2023-03-20 | 2024-06-11 | 北京工业大学 | Single-degree-of-freedom symmetrical seven-rod closed-loop extensible unit and regular five-pointed star-regular five-pointed prism conversion mechanism based on same |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180227 Termination date: 20190710 |