CN209008843U - Spliced unmanned aerial vehicle fuselage - Google Patents
Spliced unmanned aerial vehicle fuselage Download PDFInfo
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- CN209008843U CN209008843U CN201821826491.5U CN201821826491U CN209008843U CN 209008843 U CN209008843 U CN 209008843U CN 201821826491 U CN201821826491 U CN 201821826491U CN 209008843 U CN209008843 U CN 209008843U
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- cantilever
- card slot
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- aerial vehicle
- unmanned aerial
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Abstract
The utility model provides a kind of spliced unmanned aerial vehicle fuselage, including central plate and is uniformly distributed the several groups power plant module being mounted on the outside of central plate, power plant module includes motor mounting plate and two cantilever slabs, wherein motor mounting plate is installed with power supply machine；Motor mounting plate is connected between spaced two cantilever slabs, and cantilever slab and central plate are clamped so that power plant module uses splicing structure, and due between power plant module and central plate using clamping, it is comprehensive so that its structure is simple, it is easy to assembly, quick.
Description
Technical field
The utility model relates to aircraft fields, and in particular to a kind of spliced unmanned aerial vehicle fuselage.
Background technique
Unmanned plane, refer to be not loaded with operator can be with autonomous flight or the aircraft of remote driving, to be widely used in
It takes photo by plane, detect, searching and rescuing, the every field such as resource exploration, agricultural, having that small in size, light-weight, expense is low, flexible operation and peace
The features such as Quan Xinggao.
Currently, the fuselage of unmanned plane is the three-dimensional structure that multiple component is constituted, more than two plane figures are constituted
Each components between need to be locked in together by a large amount of screw, and then need during assembling using corresponding
Tool operates, and installation and removal are complicated, so that the maintenance and replacement of each component of connection unmanned plane are more troublesome.Therefore such as
What is realized the simplification assembled between each components, rapid becomes nowadays urgent problem to be solved.
Utility model content
For this purpose, the technical problem to be solved by the present invention is to overcome the unmanned plane of the prior art more putting down due to fuselage
Each components between face in turn result in the technological deficiency that structure is complicated, assembling is inconvenient by the sealed connection of screw, thus
The spliced unmanned aerial vehicle fuselage that a kind of structure is simple, easy to assembly is provided.
The utility model provides a kind of spliced unmanned aerial vehicle fuselage thus, including during central plate and being uniformly distributed is mounted on
Several groups power plant module on the outside of core, power plant module include motor mounting plate and two cantilever slabs, wherein motor mounting plate with
Power supply machine installation；Motor mounting plate is connected between spaced two cantilever slabs, and cantilever slab and central plate are clamped, and then are made
It obtains power plant module and uses splicing structure, and since, using clamping, synthesis is so that its structure is simple between power plant module and central plate
It is single, it is easy to assembly, quick.
Further, one end clamping of cantilever slab on the central plate, offers the first cantilever card on the other end of cantilever slab
Slot corresponds to the first cantilever card slot on motor mounting plate and has protruded out protrusion, and protrusion correspondence is held in the first cantilever card slot, in turn
Realize the clamping between motor mounting plate and cantilever slab.
Further, the second cantilever card slot is also provided on cantilever slab, power plant module further includes cantilever snaps, cantilever snaps
Fixing groove is offered corresponding to the second cantilever card slot, cantilever snaps are connected between two cantilever slabs, and pass through fixing groove and the
Two cantilever card slots are clamped between cantilever slab, so that motor mounting plate can be realized by cantilever snaps clamping cantilever slab
The fastening installation of motor mounting plate in all directions.
Further, power plant module further includes at least one support plate, and one end of support plate is connected to motor mounting plate
Outside, interference fit is connected with blade protection board on the other end of support plate, so by blade protection board play to human body,
The protective effect of unmanned plane propeller and motor.
Further, it there are two support plates, and is arranged in a mutually vertical manner respectively with motor mounting plate, two support plates are in certain
Angle setting；The arc-shaped plate of blade protection board, and correspondence is connected on the free end of two support plates, ensure that blade is protected
Stress equalization of the backplate on power plant module, to ensure that the stability of flight.
Further, holding section has been protruded out on one end of cantilever slab, is corresponded to holding section on central plate and is offered several
Card hole, holding section corresponds and is held in card hole, and then realizes the clamping between cantilever slab and central plate.
Further, central plate is octagon, and opens up that there are two card holes on symmetrical four edges respectively；Power mould
Block has four groups, and is arranged in a one-to-one correspondence on four edges, and two cantilever slabs correspondence in each group of power plant module is connected to card hole
In.
Further, spliced unmanned aerial vehicle fuselage further includes center connecting plate, and center connecting plate is parallel to each other with central plate
Interval is arranged, and cantilever slab is corresponded on center connecting plate and offers connection card slot；Correspond to connection card slot on cantilever slab to be provided with
Third cantilever card slot, cantilever slab and center connecting plate realize cantilever by third cantilever card slot and connection card slot clamping
The position of plate and center connecting plate is fixed, to ensure that central plate can not move in vertical direction, ensure that the steady of flight
It is qualitative.
Further, spliced unmanned aerial vehicle fuselage further includes fixed card buckle, and fixed card buckle is arranged in a mutually vertical manner with central plate,
It is spaced apart in fixed card buckle and is equipped with the first card slot and the second card slot, central plate is connected in the first card slot, center connecting plate clamping
In the second card slot, the stabilization connected between central plate and center connecting plate is further strengthened by the way that fixed card buckle is arranged
Property.
Further, center connecting plate is octagon, and opens up that there are two connection cards on symmetrical four edges respectively
Slot；Power plant module has four groups, and is arranged in a one-to-one correspondence on four edges, the corresponding card of two cantilever slabs in each group of power plant module
It connects in connection card slot.
Spliced unmanned aerial vehicle fuselage provided by the utility model, since several groups power plant module is uniformly distributed the center of being mounted on
On the outside of plate, and then it ensure that the stress equalization in flight course；Simultaneously as power plant module includes that motor mounting plate and two are outstanding
Arm plate, wherein motor mounting plate is installed with power supply machine；Motor mounting plate is connected between spaced two cantilever slabs, into
And make power plant module using splicing structure, and since cantilever slab and central plate are clamped, i.e., between power plant module and central plate
It is comprehensive so that its structure is simple using clamping, it is easy to assembly, quick.
Detailed description of the invention
In order to illustrate more clearly of the technical solution of specific embodiment of the present invention, below according to the utility model
Specific embodiment and in conjunction with attached drawing, is described in further detail utility model.
Fig. 1 is the schematic diagram of the utility model spliced unmanned aerial vehicle fuselage；
Fig. 2 is the stereogram exploded view of spliced unmanned aerial vehicle fuselage shown in Fig. 1；
Fig. 3 is the enlarged diagram of power plant module in spliced unmanned aerial vehicle fuselage shown in Fig. 1；
Fig. 4 is the stereogram exploded view of power plant module shown in Fig. 4；
Fig. 5 is the assembling enlarged diagram between the central plate and center connecting plate of spliced unmanned aerial vehicle fuselage shown in Fig. 1；
Fig. 6 is the stereogram exploded view of central plate and center connecting plate shown in Fig. 5.
It is each in figure that the reference numerals are as follows:
1- central plate；11- card hole；2- power plant module；21- motor mounting plate；
211- protrusion；212- installs card slot；22- cantilever slab；221- the first cantilever card slot；
222- the second cantilever card slot；The holding section 223-；224- third cantilever card slot；
23- cantilever snaps；231- fixing groove；232- fixation hole；24- support plate；
241- first supports card slot；242- fixed part；243- second supports card slot；
25- blade protection board；251- blade protects card slot；3- center connecting plate；
31- connection card slot；4- fixed card buckle；The first card slot of 41-；The second card slot of 42-.
Specific embodiment
The technical solution of the utility model is clearly and completely described below in conjunction with attached drawing, it is clear that described
Embodiment is the utility model a part of the embodiment, instead of all the embodiments.Based on the embodiments of the present invention, originally
Field those of ordinary skill every other embodiment obtained without making creative work belongs to practical
Novel protected range.
In the description of the present invention, it should be noted that the orientation or positional relationship of the instructions such as term "inner", "outside"
To be based on the orientation or positional relationship shown in the drawings, it is merely for convenience of describing the present invention and simplifying the description, without referring to
Show or imply that signified device or element must have a particular orientation, be constructed and operated in a specific orientation, therefore cannot manage
Solution is limitations of the present invention.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " connection "
It shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection.When an element is expressed " connection " separately
One element, it can be directly to another element or there may be one or more elements placed in the middle therebetween.It is right
For those skilled in the art, the concrete meaning of above-mentioned term in the present invention can be understood with concrete condition.
In addition, as long as technical characteristic involved in the utility model different embodiments disclosed below is each other
Not constituting conflict can be combined with each other.
A kind of embodiment of spliced unmanned aerial vehicle fuselage as described in Figure 1, including central plate 1 and being uniformly distributed are mounted on
The several groups power plant module 2 in 1 outside of central plate, as shown in figure 4, power plant module 2 includes motor mounting plate 21 and two cantilever slabs
22, wherein motor mounting plate 21 is installed with power supply machine；Motor mounting plate 21 be connected to spaced two cantilever slabs 22 it
Between, cantilever slab 22 and central plate 1 are clamped.
Above-mentioned spliced unmanned aerial vehicle fuselage is mounted on 1 outside of central plate since several groups power plant module 2 is uniformly distributed, into
And it ensure that the stress equalization in flight course；Simultaneously as power plant module 2 includes motor mounting plate 21 and two cantilever slabs
22, wherein motor mounting plate 21 is installed with power supply machine；Motor mounting plate 21 be connected to spaced two cantilever slabs 22 it
Between so that power plant module 2 uses splicing structure, and since cantilever slab 22 and central plate 1 are clamped, i.e., power plant module 2 with
It is comprehensive so that its structure is simple using clamping between central plate 1, it is easy to assembly, quick.
As optional embodiment, as depicted in figs. 1 and 2, central plate 1 is octagon, and symmetrical four edges
It is upper to be opened up respectively there are two card hole 11；Power plant module 2 has four groups, and is arranged in a one-to-one correspondence on four edges, each group of power mould
Two cantilever slabs 22 correspondence in block 2 is connected in card hole 11.
Specifically, as shown in Figures 1 to 4, cantilever slab 22 is arranged in a mutually vertical manner with the central plate 1, the one of cantilever slab 22
End corresponds to card hole 11 and has protruded out holding section 223, and holding section 223 corresponds and is held in card hole 11, and then realizes cantilever
Clamping between plate 22 and central plate 1；The first cantilever card slot 221 and the second cantilever card slot are offered on the other end of cantilever slab 22
222。
Correspond to the first cantilever card slot 221 on motor mounting plate 21 and protruded out protrusion 211, protrusion 211 is corresponding to be held in the
In one cantilever card slot 221, and then realize the clamping between motor mounting plate 21 and cantilever slab 22.
Power plant module 2 further includes cantilever snaps 23, and cantilever snaps 23 correspond to the second cantilever card slot 222 and offer fixing groove
231, cantilever snaps 23 are connected between two cantilever slabs 22, and are clamped on by fixing groove 231 and the second cantilever card slot 222 outstanding
Between arm plate 22, so that motor mounting plate 21 can realize motor installation by 23 clamping cantilever slab 22 of cantilever snaps
The fastening installation of plate 21 in all directions.
Meanwhile power plant module 2 further includes at least one support plate 24, one end of support plate 24 is connected to motor mounting plate 21
Outside, support plate 24 is corresponded on motor mounting plate 21 and is also provided with installation card slot 212, support plate 24 corresponds to installation card slot
212 offer the first support card slot 241, and the first support card slot 241 and installation card slot 212 staggeredly engage, to connect support plate 24
With motor mounting plate 21；Cantilever snaps 23 correspond to support plate 24 and are also provided with fixation hole 232, and support plate 24 corresponds to fixation hole
232 have protruded out fixed part 242, and fixed part 242 is plugged in fixation hole 232, to connect support plate 24 and cantilever snaps 23.
The other end interference fit of support plate 24 is connected with blade protection board 25, and the is offered on the other end of support plate 24
Two support card slots 243, blade protection board 25 correspond to the second support card slot 243 and offer blade protection card slot 251, blade protection
Card slot 251 and the second support card slot 243 staggeredly engage, and to connect support plate 24 and blade protection board 25, and then are protected by blade
Backplate 25 plays the protective effect to human body, unmanned plane propeller and motor.In the present embodiment, support plate 24 has two
It is a, and be arranged in a mutually vertical manner respectively with motor mounting plate 21, two settings in a certain angle of support plate 24；Blade protection board 25 is in
The plate of arc, and correspondence is connected on the free end of two support plates 24, ensure that blade protection board 25 on power plant module 2
Stress equalization, to ensure that the stability of flight.
In order to enable central plate 1 can not move in vertical direction, guarantee the stability of flight, such as Fig. 2, Fig. 5 and Fig. 6 institute
Show, spliced unmanned aerial vehicle fuselage further includes the center connecting plate 3 of octagon, between center connecting plate 3 and central plate 1 are parallel to each other
Card slot 31 is connected there are two opening up respectively every setting, and on symmetrical four edges；Four groups of power plant modules 2 are arranged in a one-to-one correspondence
Correspond to connection card slot 31 on the four edges, on two cantilever slabs 22 in each group of power plant module 2 and is provided with third cantilever card
Slot 224, cantilever slab 22 and center connecting plate 3 are clamped by third cantilever card slot 224 and connection card slot 31, and then realize cantilever
Plate 22 and the position of center connecting plate 3 are fixed, that is, ensure that central plate 1 can not move in vertical direction.
In the present embodiment, in order to further strengthen the stabilization connected between central plate 1 and center connecting plate 3
Property, as shown in Figure 2, Figure 5 and Figure 6, spliced unmanned aerial vehicle fuselage further includes fixed card buckle 4, and fixed card buckle 4 and central plate 1 are mutual
It is vertically arranged, is spaced apart in fixed card buckle 4 and is equipped with the first card slot 41 and the second card slot 42, central plate 1 is connected to the first card slot 41
In, center connecting plate 3 is connected in the second card slot 42, further strengthens central plate 1 and center by the way that fixed card buckle 4 is arranged
The stability connected between connecting plate 3.
Obviously, the above embodiments are merely examples for clarifying the description, and does not limit the embodiments.It is right
For those of ordinary skill in the art, can also make on the basis of the above description it is other it is various forms of variation or
It changes.There is no necessity and possibility to exhaust all the enbodiments.And it is extended from this it is obvious variation or
It changes still within the protection scope of the invention.
Claims (10)
1. a kind of spliced unmanned aerial vehicle fuselage, which is characterized in that including central plate (1) and be uniformly distributed and be mounted on the central plate
(1) the several groups power plant module (2) on the outside of, the power plant module (2) include:
Motor mounting plate (21), is installed with power supply machine；
Two cantilever slabs (22), the motor mounting plate (21) are connected between spaced two cantilever slabs (22),
The cantilever slab (22) and the central plate (1) are clamped.
2. spliced unmanned aerial vehicle fuselage according to claim 1, which is characterized in that one end of the cantilever slab (22) is clamped
On the central plate (1), the first cantilever card slot (221), the motor peace are offered on the other end of the cantilever slab (22)
Correspond to the first cantilever card slot (221) in loading board (21) to have protruded out raised (211), protrusion (211) correspondence is held in
In the first cantilever card slot (221).
3. spliced unmanned aerial vehicle fuselage according to claim 2, which is characterized in that be also provided on the cantilever slab (22)
Second cantilever card slot (222), the power plant module (2) further include cantilever snaps (23), and the cantilever snaps (23) correspond to institute
It states the second cantilever card slot (222) to offer fixing groove (231), the cantilever snaps (23) are connected to two cantilever slabs (22)
Between, and be clamped between the cantilever slab (22) by the fixing groove (231) and the second cantilever card slot (222).
4. spliced unmanned aerial vehicle fuselage according to claim 2, which is characterized in that the power plant module (2) further include to
A few support plate (24), one end of the support plate (24) is connected to the outside of the motor mounting plate (21), the support
Interference fit is connected with blade protection board (25) on the other end of plate (24).
5. spliced unmanned aerial vehicle fuselage according to claim 4, which is characterized in that there are two the support plates (24), and
It is arranged in a mutually vertical manner respectively with the motor mounting plate (21), two support plate (24) settings in a certain angle；The paddle
The arc-shaped plate of leaf protection board (25), and correspondence is connected on the free end of two support plates (24).
6. the spliced unmanned aerial vehicle fuselage according to any one of claim 2-5, which is characterized in that the cantilever slab (22)
One end on protruded out holding section (223), on the central plate (1) correspond to the holding section (223) offer several cards
Hole (11), the holding section (223) correspond and are held in the card hole (11).
7. spliced unmanned aerial vehicle fuselage according to claim 6, which is characterized in that the central plate (1) is octagon,
And there are two being opened up respectively on symmetrical four edges the card hole (11)；The power plant module (2) has four groups, and corresponds
It is arranged on the four edges, two cantilever slabs (22) correspondence in each group of power plant module (2) is connected to the card hole (11)
In.
8. spliced unmanned aerial vehicle fuselage according to any one of claims 1-5, which is characterized in that it is described it is spliced nobody
Machine fuselage further includes center connecting plate (3), and the center connecting plate (3) and the central plate (1) are parallel to each other and are spaced setting, institute
It states and offers connection card slot (31) corresponding to the cantilever slab (22) on center connecting plate (3)；It is corresponding on the cantilever slab (22)
The connection card slot (31) is provided with third cantilever card slot (224), the cantilever slab (22) and the center connecting plate (3) are logical
Cross the third cantilever card slot (224) and the connection card slot (31) clamping.
9. spliced unmanned aerial vehicle fuselage according to claim 8, which is characterized in that the spliced unmanned aerial vehicle fuselage also wraps
Include fixed card buckle (4), the fixed card buckle (4) is arranged in a mutually vertical manner with the central plate (1), on the fixed card buckle (4) between
It separates and is equipped with the first card slot (41) and the second card slot (42), the central plate (1) is connected in first card slot (41), described
Center connecting plate (3) is connected in second card slot (42).
10. spliced unmanned aerial vehicle fuselage according to claim 8, which is characterized in that the center connecting plate (3) is positive eight
Side shape, and open up that there are two the connection card slots (31) on symmetrical four edges respectively；The power plant module (2) has four groups,
And be arranged in a one-to-one correspondence on the four edges, two cantilever slabs (22) correspondence in each group of power plant module (2) is connected to institute
It states in connection card slot (31).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821826491.5U CN209008843U (en) | 2018-11-07 | 2018-11-07 | Spliced unmanned aerial vehicle fuselage |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821826491.5U CN209008843U (en) | 2018-11-07 | 2018-11-07 | Spliced unmanned aerial vehicle fuselage |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209008843U true CN209008843U (en) | 2019-06-21 |
Family
ID=66841599
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821826491.5U Active CN209008843U (en) | 2018-11-07 | 2018-11-07 | Spliced unmanned aerial vehicle fuselage |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209008843U (en) |
-
2018
- 2018-11-07 CN CN201821826491.5U patent/CN209008843U/en active Active
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