CN206537486U - A kind of unmanned plane wing splicing construction - Google Patents
A kind of unmanned plane wing splicing construction Download PDFInfo
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- CN206537486U CN206537486U CN201621289805.3U CN201621289805U CN206537486U CN 206537486 U CN206537486 U CN 206537486U CN 201621289805 U CN201621289805 U CN 201621289805U CN 206537486 U CN206537486 U CN 206537486U
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- fuselage
- intubation
- unmanned plane
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Abstract
The utility model is related to a kind of unmanned plane wing splicing construction.It includes fuselage, port wing and starboard wing, in addition to multiple assembly components for being used to being assembled in port wing and starboard wing into the fuselage left and right sides respectively.By setting assembly component in the stitching portion of left and right wing and fuselage, and the mode coordinated using intubation and socket gap makes fuselage and wing mutually splice, it will splice the fuselage being integrated using the binding part and buckle on assembly component and wing carry out secondary fixation.The utility model unmanned plane wing splicing construction, intubation and jack that mutual gap coordinates are set in the inside of wing and fuselage, binding part is recycled by wing and the secondary fixation of fuselage, used tubing not only improves the integrally-built intensity of light-duty unmanned plane, and two frees degree of wing and fuselage can be limited, it is simple in construction together with the stretching by binding part can be tightly secured in wing with fuselage, ingenious in design, assembly is convenient.
Description
Technical field
The utility model is related to unmanned air vehicle technique field, more particularly to a kind of unmanned plane wing splicing construction.
Background technology
Light-duty unmanned plane refer to low-latitude flying, take-off weight below 7kg unmanned plane.In light-duty unmanned plane commercial field
In, unmanned plane structure accomplish it is portable, it is easy splicing, it is solid and reliable be huge advantage, the dismounting connecting method of wherein wing can be carried
High Consumer's Experience, reduces unmanned plane and stores volume, be particularly important in individual combat.
The connecting method of domestic existing light-duty unmanned plane is usually to be cooperated with metalwork at present, is screwed；
Or be fastened using fastener, and the splicing intensity of fastener and metalwork will reach the stability that unmanned plane during flying needs, zero
The quality of part can be than larger, and the volume of part is also than larger.This is all bad for light-duty unmanned plane total quality and internal structure
Gesture.In addition, screw fix structure and fastener manner it is complicated, high processing costs, operating method is not easy.
The content of the invention
The purpose of this utility model is to provide a kind of unmanned plane wing splicing construction.
The utility model solve the technical scheme that is used of above-mentioned technical problem for：A kind of unmanned plane wing splicing construction,
It includes fuselage and can be in the port wing and starboard wing of specular, in addition to multiple is used for the port wing and right machine
The wing is assembled in the assembly component of the fuselage left and right sides respectively.
In a preferred embodiment, the assembly component includes：In banding and the binding part of Bending Deformation can be produced；Can
It is formed with the buckle held together for the binding part winding hoop, the side wall of the buckle for limiting the binding element falling
Stopper slot；And it is detachably connectable on the binding part, the leash for pulling it and making it produce Bending Deformation.
In a preferred embodiment, the left and right sides of the fuselage is respectively symmetrically formed with left mounting surface and right mounting surface,
It is formed with that be formed with the left Mosaic face can be inconsistent with the left mounting surface and be close to, the starboard wing can on the port wing
With the right mounting surface is inconsistent and the right Mosaic face be close to.
In a preferred embodiment, shape is corresponded to respectively on the left Mosaic face of the port wing and the left mounting surface of the fuselage
Into have it is multiple can mutually in the left intubation and left jack of male-female engagement grafting, the right Mosaic face of the starboard wing and the fuselage
Be correspondingly formed respectively on right mounting surface it is multiple can mutually in male-female engagement grafting right intubation and right jack；It is described left to be intubated
Being fully inserted into the left jack can be such that the left side of the port wing and fuselage closely splices, and the right intubation is fully-inserted described right slotting
Hole can be such that the right side of the starboard wing and fuselage closely splices.
In a preferred embodiment, shape is corresponded to respectively on the left Mosaic face of the port wing and the left mounting surface of the fuselage
Into have it is multiple can mutually in the left jack and left intubation of male-female engagement grafting, the right Mosaic face of the starboard wing and the fuselage
Be correspondingly formed respectively on right mounting surface it is multiple can mutually in male-female engagement grafting right jack and right intubation；It is described left to be intubated
Being fully inserted into the left jack can be such that the left side of the port wing and fuselage closely splices, and the right intubation is fully-inserted described right slotting
Hole can be such that the right side of the starboard wing and fuselage closely splices.
In a preferred embodiment, the left and right sides of the fuselage upper surface is respectively formed with multiple for being tied up described in fixation
Determine separable insertion one in the first mounting groove of part, first mounting groove closed for the binding part to be connected into
The contiguous block of round；At the upper surface of the port wing and starboard wing and the position of the close left Mosaic face and right Mosaic face
It is formed with multiple second mounting grooves for being used to fix the buckle corresponding with first mounting groove.
In a preferred embodiment, the left and right sides of the fuselage upper surface is respectively formed with multiple for fixing the card
At second mounting groove of button, port wing and the starboard wing upper surface and the position of the close left Mosaic face and right Mosaic face
It is formed with multiple first mounting grooves corresponding with second mounting groove, first mounting groove and separates an embedded use
In the contiguous block that the binding part is connected into closed round.
In a preferred embodiment, the binding part may be selected from it is following in one or more combinations：Rubber band, elasticity
Rope, toughness rope, the binding part, which can be wound, to be arranged in the stopper slot of the buckle.
In a preferred embodiment, the fuselage, port wing and starboard wing are made by tubing, and its material may be selected from as follows
One or more of combinations in material：Compound carbon fibre material, metal material, inorganic material, the left intubation and right intubation
Cross sectional shape can be circular or polygon.
The beneficial effect of the utility model unmanned plane wing splicing construction is：Pass through the splicing in left and right wing and fuselage
Place sets assembly component, and the mode coordinated using intubation and socket gap, and wing and the assembled of fuselage can be made more to facilitate
Fast, it is precisely firm.The utility model unmanned plane wing splicing construction, sets mutual gap to coordinate in the inside of wing and fuselage
Intubation and jack, recycle binding part and buckle to be intertwined and connected, can by wing and the secondary fixation of fuselage, used pipe
Material not only improves the integrally-built intensity of light-duty unmanned plane, but also can limit two frees degree of wing and fuselage, by tying up
Determine together with the stretching of part can be tightly secured in wing with fuselage, simple in construction, ingenious in design, assembly is convenient.
Brief description of the drawings
Fig. 1 is the schematic perspective view of light-duty unmanned plane in an embodiment.
Fig. 2 is the enlarged diagram of assembly component in Fig. 1.
Fig. 3 is the top view after light-duty unmanned plane decomposition in an embodiment.
Fig. 4 is light-duty unmanned plane exploded schematic perspective view in an embodiment.
Fig. 5 is the enlarged diagram of part A in Fig. 4.
Embodiment
Further detailed is made to unmanned plane wing splicing construction of the present utility model below in conjunction with specific embodiment and accompanying drawing
Thin description.
Refer to Fig. 1, a kind of unmanned plane wing splicing construction, it includes fuselage 10 and can be in the left machine of specular
The wing 20 and starboard wing 30, in addition to multiple spellings for being used to being assembled in port wing 20 and starboard wing 30 into the left and right sides of fuselage 10 respectively
Arrangement 40.
Please referring also to Fig. 2 and Fig. 5, it is preferred that assembly component includes binding part 41, buckle 42 and leash 43；Tie up
Part 41 is determined in banding and bendable is converted into a round, its two ends doubling and after fixing, the binding part 41 of the round can wind hoop
Hold together on the lateral wall of buckle 42, the stopper slot 421 that limitation binding part 41 comes off, traction are additionally operable on the lateral wall of buckle 42
Band 43 is detachably connectable on binding part 41, pulls leash 43 that binding part 41 can be driven to produce Bending Deformation, release is led
Leader tape 43, binding part 41 can keep present situation or recover to original state.
It is preferred that, binding part 41 may be selected from it is following in one or more combinations：Rubber band, elastic threads, toughness rope, this is tied up
Determine part 41 and can wind to be arranged in 421 in the stopper slot of buckle 42.
Please referring also to Fig. 3, left mounting surface 11 and right mounting surface 12 are respectively symmetrically formed with the left and right sides of fuselage 10,
It is formed with that be formed with the left Mosaic face 21 can be inconsistent with left mounting surface 11 and be close to, starboard wing 30 can be with the right side on port wing 20
Mounting surface 12 is inconsistent and the right Mosaic face 31 be close to.
It is preferred that, be correspondingly formed respectively on the left Mosaic face 21 of port wing 20 and the left mounting surface 11 of fuselage 10 it is multiple can
Mutually in the left intubation 22 and left jack 13, the right Mosaic face 31 of starboard wing 30 and the right mounting surface of fuselage 10 of male-female engagement grafting
Be correspondingly formed respectively on 12 it is multiple can mutually in male-female engagement grafting right intubation 32 and right jack 14；Left intubation 22 and a left side are inserted
Between hole 13 and gap is formed between right intubation 32 and right jack 14 to coordinate, when 22 fully-inserted left jack 13 of left intubation,
The left side of port wing 20 and fuselage 10 can be made closely to splice, when 32 fully-inserted right jack 14 of right intubation, starboard wing 30 can be made
Closely splice with the right side of fuselage 10, now, fuselage 10 is spliced into a unmanned plane with port wing 20 and starboard wing 30.
In another embodiment, the position of left intubation 22 and left jack 13 can mutually be exchanged, right intubation 32 and right jack 14
Position can mutually exchange.It has been correspondingly formed respectively on the left Mosaic face 21 of port wing 20 and the left mounting surface 11 of fuselage 10 multiple
Can be mutually in the left jack 13 and left intubation 22 of male-female engagement grafting, the right installation of the right Mosaic face 31 and fuselage 10 of starboard wing 30
Be correspondingly formed respectively on face 12 it is multiple can mutually in male-female engagement grafting right jack 14 and it is right intubation 32；Left jack 13 and a left side
Intubation 22 between, right jack 14 and it is right intubation 32 before formed gap coordinate, when it is left intubation 22 fully-inserted left jack 13 when, can
The left side of port wing 20 and fuselage 10 is closely spliced, when it is right intubation 32 fully-inserted right jack 14 when, can make starboard wing 30 with
The right side of fuselage 10 is closely spliced, now, and fuselage 10 is spliced into a unmanned plane with port wing 20 and starboard wing 30.
Please referring also to Fig. 4 and Fig. 5, the left and right sides of the upper surface of fuselage 10, which has been symmetrically formed, multiple to be used to fix binding portion
Embedded one is separated in first mounting groove 412 of part 41, the first mounting groove 412 is used to binding part 41 connecting into closed circle
The contiguous block 411 of shape, contiguous block 411 is used to connect and bind the two ends of part 41 to form it into closed round；Port wing 20
Multiple and the first mounting groove is formed with the upper surface of starboard wing 30 and the position of close left Mosaic face 21 and right Mosaic face 31
412 second mounting grooves 422 corresponding, for fixing buckle 41；When port wing 20 and starboard wing 30 are tight with fuselage 10 respectively
During close splicing, the binding part 41 of round is pulled to be allowed to produce Bending Deformation towards buckle direction, then binding part 41 is wound
In stopper slot 421 on the lateral wall of buckle 42, the stretching to binding part 41 is then discharged, the activity of part 41 is now bound
End is held together in the stopper slot 421 of buckle 42 by hoop.
In another embodiment, the position of the first mounting groove 412 and the second mounting surface 422 can be exchanged, i.e. the first mounting groove
412 form in the upper surface of port wing 20 and starboard wing 30 and at the position of left Mosaic face 21 and right Mosaic face 31, and second
Mounting surface 422 forms the left and right sides in the upper surface of fuselage 10.The left and right sides of the upper surface of fuselage 10 has been symmetrically formed multiple use
In the second mounting groove 422 of fixed buckle 41, the upper surface of port wing 20 and starboard wing 30 and close left Mosaic face 21 and right spelling
It is formed with the position of junction 31 in multiple first mounting grooves 412 corresponding with the second mounting groove 422, the first mounting groove 412
Separable embedded one contiguous block 411 for binding part 41 to be connected into closed round, contiguous block 411 is used to connect and bind
The two ends of part 41 are to form it into closed round；When port wing 20 and starboard wing 30 closely splice with fuselage 10 respectively,
Pull the binding part 41 of round to be allowed to produce Bending Deformation towards buckle direction, then binding part 41 is wrapped in outside buckle 42
In stopper slot 421 on the wall of side, the stretching to binding part 41 is then discharged, the movable end for now binding part 41 is bound round
In the stopper slot 421 of buckle 42.
Fuselage 10, port wing 20 and starboard wing 30 are made by tubing, with its integrally formed left intubation 20 and right intubation
30 are made by tubing, and its material may be selected from one or more of combinations in following material：Compound carbon fibre material, metal material
（Such as aluminium, titanium）, inorganic material（Glass, ceramics etc.）；The cross sectional shape of left intubation 22 and right intubation 32 can be circular or polygon
Shape, this way can effectively prevent splicing mistake, can improve the integrally-built intensity of unmanned plane.
When actual assembled, because port wing and starboard wing are in specular, and joining method is identical, starboard wing
Splicing exemplified by illustrate, binding part explanation exemplified by rubber band.First, by the right Mosaic face of starboard wing towards fuselage right installation
Face is drawn close, and right intubation is mutually alignd one by one with right jack, promotes direction of the starboard wing along right jack to move, and make right intubation
Take advantage of a situation and insert right jack, stop when in the right fully-inserted right jack of intubation, now right Mosaic face is close to safely with right mounting surface
Together, starboard wing is integrated with fuselage splicing, the first peace for then inserting the contiguous block on the rubber band in round on wing
Tankage, the second mounting groove for then again inserting buckle on starboard wing, rubber band now is that can not bind round in buckle under normal conditions
On, then pull or pull rubber band and being allowed to produce Bending Deformation with pull rope, to its movable end close to buckle, then will
Rubber band hoop is held together at the stopper slot on buckle by way of winding, according to the rubber band of different length, can be wound by changing
The number of turns be allowed to and snap connection, until rubber band be in exceptionally straight state, now discharge the pulling to rubber band, it bounces back towards normality
During can be fully embedded in stopper slot, so far, assembly component is completed, and other several assembly components repeat above-mentioned
Step, due to binding the stretching action of part in assembly component, can make to lean in mutually conflict all the time between starboard wing and fuselage
Near state, makes splicing more stablize.
To sum up, the beneficial effect of the utility model unmanned plane wing splicing construction is：By in left and right wing and fuselage
Stitching portion assembly component, and the mode coordinated using intubation and socket gap are set, can make wing and fuselage it is assembled more
Plus it is convenient and swift, precisely firm.The utility model unmanned plane wing splicing construction, sets mutual in the inside of wing and fuselage
Being intertwined and connected for intubation and jack that gap coordinates, recycling binding part and buckle, can be made wing and the secondary fixation of fuselage
Tubing not only improves the integrally-built intensity of light-duty unmanned plane, but also can limit two frees degree of wing and fuselage,
Simple in construction together with stretching by binding part can be tightly secured in wing with fuselage, ingenious in design, assembly is convenient.
Although being to combine embodiments above to carry out to description of the present utility model, it is familiar with the art
Personnel many replacements, modifications and variations can be carried out according to above-mentioned content, are obvious.Therefore, it is all such
Substitute, improve and change and be included in the spirit and scope of appended claims.
Claims (8)
1. a kind of unmanned plane wing splicing construction, it includes fuselage and can be in the port wing and starboard wing of specular, and it is special
Levy and be, in addition to multiple be used to being assembled in the port wing and starboard wing into the fuselage left and right sides respectively assembled group
Part；
The assembly component includes：
In banding and the binding part of Bending Deformation can be produced；
It is available for the binding part to wind on the buckle that hoop holds together, the side wall of the buckle to be formed with for limiting the binding part
The stopper slot come off；And
It is detachably connectable to be bound described on part, for pulling it and making the leash of its generation Bending Deformation.
2. unmanned plane wing splicing construction according to claim 1, it is characterised in that the left and right sides difference of the fuselage
It has been symmetrically formed to be formed with left mounting surface and right mounting surface, the port wing and can be inconsistent with the left mounting surface and be close to
The right Mosaic face can be inconsistent with the right mounting surface and be close to is formed with left Mosaic face, the starboard wing.
3. unmanned plane wing splicing construction according to claim 2, it is characterised in that the left Mosaic face of the port wing and
Be correspondingly formed respectively on the left mounting surface of the fuselage it is multiple can mutually in male-female engagement grafting left intubation and left jack, institute
State be correspondingly formed respectively on the right Mosaic face of starboard wing and the right mounting surface of the fuselage it is multiple can mutually in male-female engagement insert
The right intubation connect and right jack；The left fully-inserted left jack of intubation can make the left side of the port wing and fuselage close
Splicing, the right fully-inserted right jack of intubation can be such that the right side of the starboard wing and fuselage closely splices.
4. unmanned plane wing splicing construction according to claim 2, it is characterised in that the left Mosaic face of the port wing and
Be correspondingly formed respectively on the left mounting surface of the fuselage it is multiple can mutually in male-female engagement grafting left jack and left intubation, institute
State be correspondingly formed respectively on the right Mosaic face of starboard wing and the right mounting surface of the fuselage it is multiple can mutually in male-female engagement insert
The right jack connect and right intubation；The left fully-inserted left jack of intubation can make the left side of the port wing and fuselage close
Splicing, the right fully-inserted right jack of intubation can be such that the right side of the starboard wing and fuselage closely splices.
5. the unmanned plane wing splicing construction according to any one of claim 3 to 4, it is characterised in that the fuselage upper table
The left and right sides in face is respectively formed with can in multiple the first mounting grooves for being used to fix the binding part, first mounting groove
Embedded one of separation is used for the contiguous block that the binding part is connected into closed round；The upper table of the port wing and starboard wing
Face and be formed with the position of the left Mosaic face and right Mosaic face it is multiple with first mounting groove is corresponding is used for
Second mounting groove of the fixed buckle.
6. the unmanned plane wing splicing construction according to any one of claim 3 to 4, it is characterised in that the fuselage upper table
The left and right sides in face is respectively formed with multiple the second mounting grooves for being used to fix the buckle, port wing and the starboard wing upper table
Face and it is formed with multiple corresponding with second mounting groove first at the position of the left Mosaic face and right Mosaic face
Embedded one connection for being used to connecting into the binding part into closed round is separated in mounting groove, first mounting groove
Block.
7. unmanned plane wing splicing construction according to claim 1, it is characterised in that the binding part may be selected from following
In one or more combinations：Rubber band, elastic threads, toughness rope, the binding part, which can be wound, is arranged on the spacing of the buckle
In groove.
8. the unmanned plane wing splicing construction according to any one of claim 4, it is characterised in that the fuselage, port wing
It is made with starboard wing by tubing, its material may be selected from one or more of combinations in following material：Compound carbon fibre material, gold
Belong to material, inorganic material, the cross sectional shape of the left intubation and right intubation can be circular or polygon.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621289805.3U CN206537486U (en) | 2016-11-28 | 2016-11-28 | A kind of unmanned plane wing splicing construction |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621289805.3U CN206537486U (en) | 2016-11-28 | 2016-11-28 | A kind of unmanned plane wing splicing construction |
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| Publication Number | Publication Date |
|---|---|
| CN206537486U true CN206537486U (en) | 2017-10-03 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201621289805.3U Active CN206537486U (en) | 2016-11-28 | 2016-11-28 | A kind of unmanned plane wing splicing construction |
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| CN (1) | CN206537486U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109250067A (en) * | 2018-08-27 | 2019-01-22 | 上海歌尔泰克机器人有限公司 | Quick Release wing and unmanned vehicle |
-
2016
- 2016-11-28 CN CN201621289805.3U patent/CN206537486U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109250067A (en) * | 2018-08-27 | 2019-01-22 | 上海歌尔泰克机器人有限公司 | Quick Release wing and unmanned vehicle |
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