CN208007266U - A kind of click-on design between unmanned plane parts - Google Patents
A kind of click-on design between unmanned plane parts Download PDFInfo
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- CN208007266U CN208007266U CN201820413304.4U CN201820413304U CN208007266U CN 208007266 U CN208007266 U CN 208007266U CN 201820413304 U CN201820413304 U CN 201820413304U CN 208007266 U CN208007266 U CN 208007266U
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Abstract
The utility model provides a kind of click-on design between unmanned plane parts, suitable for parts are fixed in the agent structure of unmanned plane, the ontology with a plate is buckled, runs through on ontology and offers at least one set of holding hole, parts correspondence is held in holding hole；And the external end edge of ontology has extended outward to form an at least clamping part, agent structure is provided with docking section corresponding to clamping part, clamping part correspondence is fastened in docking section, and then by buckling the clamping with parts and the snapping of buckle and agent structure, realize parts installing, fixing on the body construction so that its is easy to assembly, quick.
Description
Technical field
The present invention relates to aircraft fields, and in particular to a kind of click-on design between unmanned plane parts.
Background technology
Unmanned plane, refer to be not loaded with operating personnel 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, light-weight, expense is low, operation is flexible and pacifies
The features such as property is high entirely.
Currently, the fuselage of unmanned plane is the three-dimensional structure that multiple component is constituted, more than two plane figures are constituted
Each parts between need to be locked in together by a large amount of screw, and then need during assembling using corresponding
Tool operates, and installation is complicated with dismounting so that connects the repair of each component of unmanned plane and replaces cumbersome.Therefore such as
What is realized the simplification assembled between each parts, rapid becomes nowadays urgent problem to be solved.
Invention content
For this purpose, the technical problem to be solved in the present invention be to overcome the unmanned plane of the prior art due to fuselage more planes it
Between each parts by the sealed connection of screw, technological deficiency complicated, that assembling is inconvenient is in turn resulted in, to provide
A kind of easy to assembly, quick click-on design between unmanned plane parts.
The present invention provides a kind of click-on designs between unmanned plane parts thus, suitable for being fixed on parts
In the agent structure of unmanned plane, which has the ontology of a plate, runs through on ontology and offers at least one set of holding hole,
Parts correspondence is held in holding hole；And the external end edge of ontology has extended outward to form an at least clamping part, agent structure
Clamping part is provided with docking section, clamping part correspondence is fastened in docking section, and then by buckling the clamping with parts
And buckle and the snapping of agent structure, realize parts installing, fixing on the body construction so that its is easy to assembly,
Quickly.
Further, each group of holding hole includes at least a holding hole respectively, and each parts correspond to each clamping
Hole is respectively arranged with holding section, and holding section is held in holding hole.
Further, two groups of holding holes are offered on ontology, the quantity of holding hole is respectively two in each group, and two
Group holding hole parallel interval setting；Parts are corresponding with two groups, and each parts correspond respectively to each group of holding hole and are provided with
Two holding sections, two holding sections correspond respectively to be held in two holding holes, by the way that two groups of holding holes and right are arranged
The holding section answered, and then realize two groups of parts installing, fixing on the body construction.
Further, one group of holding hole is offered on ontology, and the quantity of holding hole is one, every one zero in the group
Part is correspondingly arranged there are one holding section, and holding section is held in holding hole.
Further, the external end edge of ontology is extended outward to form there are one clamping part, and the external end edge of clamping part is recessed inwardly
It is formed with dashpot, the opening direction of dashpot is identical as the fastening of clamping part locking direction, and then is fastened when clamping part corresponds to
When in docking section, for clamping part by the crimp of docking section, dashpot provides sufficient deformation space for the deformation, to
It is fastened so that the outer wall of clamping part is squeezed with docking section elasticity.
Further, two opposite outboard end edge of clamping part are recessed inwardly respectively is formed with limiting slot；Docking section is docking
The inner wall of hole or docking groove, docking section is smaller than the outer wall spacing of clamping part, and between more than or equal to two limiting slots
Spacing, pass through and limiting slot be set so that when clamping part and docking section are clipped to limiting slot, effect of the clamping part due to limiting slot
And can not give up the throne, and then ensure that the snap lock between clamping part and docking section.
Further, the external end edge of ontology is extended outward to form there are two the clamping part that is oppositely arranged, two clamping parts
Extending direction is opposite；Agent structure includes spaced two parts, and is correspondingly arranged on docking section in each section respectively,
Clamping part snaps onto in corresponding docking section, to connect two parts of agent structure, i.e., when agent structure has two parts, and ontology
Realize the function of two-way clamping.
Further, two opposite outboard end edge of each clamping part are recessed inwardly respectively is formed with limiting slot；Docking section is
The inner wall of butt hole or docking groove, docking section is smaller than the outer wall spacing of corresponding clamping part, and more than or equal to corresponding card
The spacing between two limiting slots on buckle, by the way that limiting slot is arranged so that when clamping part is clipped to limiting slot with docking section,
Clamping part can not be given up the throne due to the effect of limiting slot, and then ensure that the snap lock between clamping part and docking section.
Further, the external end edge of each clamping part, which is recessed inwardly, is formed with dashpot, and the opening of each dashpot
Direction is identical as the fastening of corresponding clamping part locking direction, and then when clamping part correspondence is fastened in docking section, clamping part by
To the crimp of docking section, dashpot provides sufficient deformation space for the deformation so that the outer wall of clamping part with it is right
Socket part elasticity squeezes fastening.
Provided by the present invention for the click-on design between unmanned plane parts, due to buckling the ontology with a plate, this
Through at least one set of holding hole is offered on body, parts correspondence is held in holding hole；And the external end edge of ontology is to extension
It stretches and is formed with an at least clamping part, agent structure is provided with docking section corresponding to clamping part, and clamping part correspondence is fastened on docking section
In, and then by buckling the clamping with parts and the snapping of buckle and agent structure, parts are realized in agent structure
On install, fix so that its is easy to assembly, quick.
Description of the drawings
In order to illustrate more clearly of the technical solution of the specific embodiment of the invention, below according to the specific implementation of the present invention
Example and in conjunction with attached drawing, is described in further detail invention.
Fig. 1 is the schematic diagram that the present invention connects parts and agent structure for the click-on design between unmanned plane parts；
Fig. 2 is the schematic diagram of non-snapping between parts and agent structure in click-on design shown in Fig. 1；
Fig. 3 is the schematic diagram of click-on design and parts shown in Fig. 1；
Fig. 4 is schematic diagram of the present invention for the click-on design another embodiment between unmanned plane parts；
Fig. 5 is the assembling schematic diagram between click-on design shown in Fig. 4 and the double-deck parts；
The schematic diagram that Fig. 6 is the present invention for click-on design the third embodiment between unmanned plane parts.
It is each in figure that the reference numerals are as follows：
100- click-on designs；1- ontologies；11- holding holes；12- clamping parts；
13- dashpots；14- limiting slots；200- parts；The holding sections 201-；
300- agent structures；The docking sections 301-.
Specific implementation mode
Technical scheme of the present invention is clearly and completely described below in conjunction with attached drawing, it is clear that described implementation
Example is a part of the embodiment of the present invention, instead of all the embodiments.Based on the embodiments of the present invention, ordinary skill
The every other embodiment that personnel are obtained without making creative work, shall fall within the protection scope of the present invention.
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" is base
It in orientation or positional relationship shown in the drawings, is merely for convenience of description of the present invention and simplification of the description, rather than indicates or imply
Signified device or element must have a particular orientation, with specific azimuth configuration and operation, therefore should not be understood as to this
The limitation of invention.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " connection " should be done
It broadly understood, for example, it may be being fixedly connected, may be a detachable connection.When an element be expressed " connection " another
Element, it can be directly to another element or may exist one or more elements placed in the middle therebetween.For this
For the those of ordinary skill in field, the concrete meaning of above-mentioned term in the present invention can be understood with concrete condition.
As long as in addition, technical characteristic involved in invention described below different embodiments non-structure each other
It can be combined with each other at conflict.
Embodiment 1
A kind of click-on design 100 between unmanned plane parts as described in Fig. 1 to Fig. 3 is suitable for parts 200
It is fixed in the agent structure 300 of unmanned plane, which has the ontology 1 of a plate, runs through on ontology 1 and offers
At least one set of holding hole 11, the correspondence of parts 200 are held in holding hole 11；And the external end edge of ontology 1 extends outward to form
There are an at least clamping part 12, agent structure 300 that clamping part 12 is provided with docking section 301, the correspondence of clamping part 12 is fastened on
In docking section 301.
The above-mentioned click-on design 100 between unmanned plane parts, due to buckling the ontology 1 with a plate, on ontology 1
Through at least one set of holding hole 11 is offered, the correspondence of parts 200 is held in holding hole 11；And the external end edge of ontology 1 to
Outer extension is formed with an at least clamping part 12, and agent structure 300 is provided with docking section 301, clamping part 12 corresponding to clamping part 12
Correspondence is fastened in docking section 301, and then by buckling the clamping with parts 200 and the button of buckle and agent structure 300
It connects, realizes the installing, fixing in agent structure 300 of parts 200 so that its is easy to assembly, quick.
Specifically, each group of holding hole 11 includes at least a holding hole 11 respectively, each parts 200 correspond to each
Holding hole 11 is respectively arranged with holding section 201, and holding section 201 is held in holding hole 11.
As optional embodiment, offer one group of holding hole 11 on ontology 1, and in the group holding hole 11 quantity
It it is two, each parts 200 are correspondingly arranged there are two holding section 201, and holding section 201 is held in corresponding holding hole 11.
As the embodiment of deformation, as shown in Figure 4 and Figure 5, two groups of holding holes 11 are offered on ontology 1, in each group
The quantity of holding hole 11 is respectively two, and two groups of 11 parallel interval of holding hole settings；Parts 200 are corresponding with two groups, often
One parts 200 correspond respectively to each group of setting of holding hole 11, and there are two holding sections 201, and two difference of holding sections 201 are one by one
Correspondence is held in two holding holes 11, by the way that two groups of holding holes 11 and corresponding holding section 201 is arranged, and then realizes two
Group the installing, fixing in agent structure 300 of parts 200.
The embodiment that 11 quantity of holding hole is 2 in each group of holding hole 11 is listed in the present embodiment, such as Fig. 6 institutes
Show, quantity can also be used for 1 set-up mode, it is, of course, also possible to using the setting side for opening up 3,4 etc. holding holes 11
Formula is not repeated here herein；Likewise, it is one group and two groups of parts 200 to be listed in the present embodiment by parts 200
Embodiment, due to the holding hole 11 on ontology 1 be also provided with it is multigroup, such as 3 groups, 4 groups, 5 groups etc., equally can be with
It realizes the installation connection between multigroup parts 200 and ontology 1, is no longer enumerated herein.
In order to realize the connection between ontology 1 and agent structure 300, as optional embodiment, as shown in Fig. 2, working as
When agent structure 300 is only structure as a whole, the external end edge of ontology 1 is extended outward to form there are one clamping part 12, and ontology 1 passes through
Snapping between clamping part 12 and docking section 301 links together.
As the embodiment of deformation, when agent structure 300 includes spaced two parts, as shown in figure 5, ontology
1 external end edge is extended outward to form there are two the clamping part 12 being oppositely arranged, and the extending direction of two clamping parts 12 is opposite；Simultaneously
Docking section 301 is correspondingly arranged in each section of agent structure 300 respectively, clamping part 12 snaps onto corresponding docking section 301
In, to connect two parts of agent structure 300, i.e., when agent structure 300 has two parts, the correspondence of both sides clamping part 12 is fastened on
When in two-part docking section 301, to realize two-way snapping.
In order to ensure the stability and convenience of snapping between ontology 1 and agent structure 300, as shown in Figure 2 and Figure 5,
The external end edge of clamping part 12, which is recessed inwardly, is formed with dashpot 13, and the opening direction of dashpot 13 is locked with the fastening of clamping part 12
Direction is identical, and then when the correspondence of clamping part 12 is fastened in docking section 301, clamping part 12 is become by the extruding of docking section 301
Shape, dashpot 13 provide sufficient deformation space for the deformation, so that the outer wall of clamping part 12 is squeezed with 301 elasticity of docking section
Clinching is tight.
Meanwhile as the embodiment of deformation, engaging portion 12 can also use width to be gradually reduced along locking direction is fastened
Size design, while docking section 301 correspond to using width be less than 12 maximum width of engaging portion size design, such as Fig. 6 institutes
Show, and then again may be by the characteristic of 12 own material of engaging portion, to realize the elasticity fastening in fastened orientation.
In addition to this, during clamping part 12 and 301 snap lock of docking section, in order to avoid clamping part 12 is given up the throne,
Two opposite outboard end edge of each clamping part 12 are recessed inwardly respectively is formed with limiting slot 14, as shown in Figure 3 and Figure 4；Docking section
301 be butt hole or docking groove, and the inner wall of docking section 301 is smaller than the outer wall spacing of corresponding clamping part 12, and is more than
Equal to the spacing between two limiting slots 14 on corresponding clamping part 12, pass through and limiting slot 14 be set so that clamping part 12 with it is right
When socket part 301 is clipped to limiting slot 14, clamping part 12 can not be given up the throne due to the effect of limiting slot 14, and then ensure that clamping part
Snap lock between 12 and docking section 301.
In the present embodiment, click-on design 100 use light material, such as cork wood, acrylic board, carbon fiber board,
Engineering plastics etc., and then when parts 200 are layer structure, realizing the layer structure of single layer or multilayer in unmanned plane
Installation in agent structure 300 simultaneously, also makes the weight of complete machine mitigate significantly, to save material, improve aircraft
Power performance.
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 (9)
1. a kind of click-on design (100) between unmanned plane parts is suitable for the parts (200) being fixed on nobody
In the agent structure (300) of machine, which is characterized in that the click-on design (100) has the ontology (1) of a plate, the ontology
(1) through at least one set of holding hole (11) is offered on, parts (200) correspondence is held in the holding hole (11)；
And the external end edge of the ontology (1) has extended outward to form an at least clamping part (12), and the agent structure (300) corresponds to
The clamping part (12) is provided with docking section (301), and clamping part (12) correspondence is fastened in the docking section (301).
2. the click-on design (100) according to claim 1 between unmanned plane parts, which is characterized in that each group
The holding hole (11) includes at least a holding hole (11) respectively, and each parts (200) correspond to each institute
It states holding hole (11) and is respectively arranged with holding section (201), the holding section (201) is held in the holding hole (11).
3. the click-on design (100) according to claim 2 between unmanned plane parts, which is characterized in that described
The quantity of holding hole (11) described in offering two groups on body (1), holding hole (11) described in each group is respectively two, and two
Group holding hole (11) the parallel interval setting；The parts (200) are corresponding with two groups, each parts (200) point
Not Dui Yingyu holding hole (11) setting described in each group there are two holding section (201), two holding sections (201) are respectively one by one
Correspondence is held in two holding holes (11).
4. the click-on design (100) according to claim 2 between unmanned plane parts, which is characterized in that described
Holding hole (11) described in offering one group on body (1), and the quantity of holding hole (11) is one, each described zero in the group
Part (200) is correspondingly arranged there are one holding section (201), and the holding section (201) is held in the holding hole (11).
5. the click-on design (100) being used between unmanned plane parts according to any one of claim 1 or 4, feature
It is, the external end edge of the ontology (1) extends outward to form that there are one the clamping part (12), the outer ends of the clamping part (12)
Edge, which is recessed inwardly, is formed with dashpot (13), and the opening direction of the dashpot (13) is locked with the fastening of the clamping part (12)
Direction is identical, and clamping part (12) correspondence is fastened in the docking section (301).
6. the click-on design (100) according to claim 5 between unmanned plane parts, which is characterized in that the card
Two opposite outboard end edge of buckle (12) are recessed inwardly respectively is formed with limiting slot (14)；The docking section (301) is butt hole
Or docking groove, the inner wall of the docking section (301) is smaller than the outer wall spacing of the clamping part (12), and is more than or equal to
Spacing between two limiting slots (14).
7. the click-on design (100) being used between unmanned plane parts according to any one of claim 1 or 4, feature
It is, the external end edge of the ontology (1) extends outward to form that there are two the clamping part (12) being oppositely arranged, two clamping parts
(12) extending direction is opposite；The agent structure (300) includes spaced two parts, and right respectively in each section
It should be provided with the docking section (301), the clamping part (12) snaps onto in the corresponding docking section (301), to connect
State two parts of agent structure (300).
8. the click-on design (100) according to claim 7 between unmanned plane parts, which is characterized in that Mei Yisuo
It states two opposite outboard end edge of clamping part (12) and is recessed inwardly respectively and be formed with limiting slot (14)；The docking section (301) is pair
Hole or docking groove are connect, the inner wall of the docking section (301) is smaller than the outer wall spacing of the corresponding clamping part (12), and
More than or equal to the spacing between two limiting slots (14) on the correspondence clamping part (12).
9. the click-on design (100) according to claim 7 between unmanned plane parts, which is characterized in that Mei Yisuo
The external end edge for stating clamping part (12) is recessed inwardly and is formed with dashpot (13), and the opening direction of each dashpot (13)
It is identical as the fastening of the correspondence clamping part (12) locking direction.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820413304.4U CN208007266U (en) | 2018-03-27 | 2018-03-27 | A kind of click-on design between unmanned plane parts |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820413304.4U CN208007266U (en) | 2018-03-27 | 2018-03-27 | A kind of click-on design between unmanned plane parts |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208007266U true CN208007266U (en) | 2018-10-26 |
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ID=63889269
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820413304.4U Active CN208007266U (en) | 2018-03-27 | 2018-03-27 | A kind of click-on design between unmanned plane parts |
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| CN (1) | CN208007266U (en) |
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- 2018-03-27 CN CN201820413304.4U patent/CN208007266U/en active Active
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