CN106042240A - Forming die of unmanned aerial vehicle housing - Google Patents
Forming die of unmanned aerial vehicle housing Download PDFInfo
- Publication number
- CN106042240A CN106042240A CN201610668889.XA CN201610668889A CN106042240A CN 106042240 A CN106042240 A CN 106042240A CN 201610668889 A CN201610668889 A CN 201610668889A CN 106042240 A CN106042240 A CN 106042240A
- Authority
- CN
- China
- Prior art keywords
- outer layer
- unmanned plane
- bone
- shaped
- locating
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C39/00—Shaping by casting, i.e. introducing the moulding material into a mould or between confining surfaces without significant moulding pressure; Apparatus therefor
- B29C39/22—Component parts, details or accessories; Auxiliary operations
- B29C39/26—Moulds or cores
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C33/00—Moulds or cores; Details thereof or accessories therefor
- B29C33/12—Moulds or cores; Details thereof or accessories therefor with incorporated means for positioning inserts, e.g. labels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C39/00—Shaping by casting, i.e. introducing the moulding material into a mould or between confining surfaces without significant moulding pressure; Apparatus therefor
- B29C39/02—Shaping by casting, i.e. introducing the moulding material into a mould or between confining surfaces without significant moulding pressure; Apparatus therefor for making articles of definite length, i.e. discrete articles
- B29C39/10—Shaping by casting, i.e. introducing the moulding material into a mould or between confining surfaces without significant moulding pressure; Apparatus therefor for making articles of definite length, i.e. discrete articles incorporating preformed parts or layers, e.g. casting around inserts or for coating articles
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Moulds For Moulding Plastics Or The Like (AREA)
Abstract
The invention provides a forming die of an unmanned aerial vehicle housing. The forming die comprises an upper die part and a lower die part, wherein a cavity is defined by the inner wall surface of the upper die part and the inner wall surface of the lower die part; a keel locating part is arranged in the cavity, and is used for mounting an internal keel of the unmanned aerial vehicle housing; an outer layer locating part for locating an upper outer layer is arranged on the inner wall surface of the upper die part; an outer layer locating part for locating a lower outer layer is arranged on the inner wall surface of the lower die part; the upper outer layer and the lower outer layer form a thin-skin outer layer of the unmanned aerial vehicle housing; the space, except the space that the keel locating part, the outer layer locating parts, the internal keel and the thin-skin outer layer occupy in the cavity, forms a middle layer cavity; and the middle layer cavity is used for forming a light middle layer. With the adoption of the forming die of the unmanned aerial vehicle housing, the unmanned aerial vehicle housing is formed by moulding the thin-skin outer layer, the light middle layer and the internal keel integrally .
Description
Technical field
The present invention relates to unmanned plane field, specifically refer to the mould of a kind of unmanned plane shell.
Background technology
In recent years, unmanned plane is come by more with its simple structure, the easily feature such as manipulation and higher security performance
The most attention.Unmanned plane of the prior art, including fuselage and wing arm, and its fuselage and wing arm are separately molding, use
Time need to be installed on fuselage wing arm；Simultaneously its internal keel bracket be all outside after casing forming by securing member or its
His mode installs, and such design not only makes unmanned plane installation procedure in use the most complicated, meanwhile, after installation
The appearance of unmanned plane there will be various installation vestige, as securing member etc. affects the installation vestige of the outward appearance of unmanned plane, thus lead
The appearance causing unmanned plane is poor.
Summary of the invention
In order to solve the problems referred to above, the present invention proposes the mould of a kind of unmanned plane shell, it is intended to molding is a kind of by thin
Outer cortex, lightweight middle level and interior furring channels integrated unmanned plane shell.
The present invention is achieved through the following technical solutions:
The present invention proposes the mould of a kind of unmanned plane shell, including upper die and lower die, the internal face of described upper mold and lower mold
Internal face surround die cavity；
Being provided with Os Draconis location division in described die cavity, described Os Draconis location division is for installing the interior furring channels of unmanned plane shell；
The internal face of described upper mold is provided with the outer layer location division for positioning upper outer layer；The internal face of described lower mold is provided with use
The outer layer location division of lower outer layer in location；Described upper outer layer and the thin skin outer layer of lower outer layer composition unmanned plane shell；
Removing the space beyond Os Draconis location division, outer layer location division, interior furring channels and thin skin outer layer in described die cavity is middle stratotype
Chamber, described middle level die cavity is used for forming lightweight middle level.
Further, described die cavity includes center cavity and some arm chambeies；Described center cavity is square and is positioned at described die cavity
Center, each arm chamber extends radially to far-end on a corner of described center cavity.
Further, described Os Draconis location division is installed on the internal face of described upper mold；Described Os Draconis location division includes position
In the shaped as frame bone locating piece of center cavity and be distributed in some motor bone locating pieces of close end position in each arm chamber；In described
Portion's Os Draconis include shaped as frame bone and some motor bones；Described shaped as frame bone locating piece is used for installing described shaped as frame bone；Described motor bone is fixed
Position block is used for installing described motor bone.
Further, described motor bone locating piece includes connecting portion and installation portion；The outer surface of described installation portion and motor
The inner surface laminating of bone；Described connecting portion is connected between installation portion and the internal face of upper mold, the outer surface of described connecting portion with
The outer surface profile of motor bone is similar.
Further, the cross section of described connecting portion is plum blossom-shaped, including some orthodromes and some small arc-shapeds；Described greatly
Circular arc and small arc-shaped spaced connection are arranged；The diameter of described orthodrome is more than the diameter of small arc-shaped.
Further, the internal face of described upper mold is fitted for the outer surface with described upper outer layer；The inwall of described lower mold
Fit for the outer surface with described lower outer layer in face.
Further, the outer layer location division of the lower outer layer in location includes some locating dowels and some locating convex blocks；Described locating convex block
Being positioned at center cavity, described locating dowel is distributed in the position near end, each arm chamber；The position of described lower outer layer correspondence locating dowel
Being provided with hole, location, described locating dowel is used for positioning hole, described location；The position of described lower outer layer correspondence locating convex block is provided with location
Groove, described locating convex block is used for positioning described detent.
Further, on location, the outer layer location division of outer layer is also described Os Draconis location division, and described Os Draconis location division was both used
Installation in described interior furring channels is also used for the location of upper outer layer；The position of described upper outer layer correspondence shaped as frame bone locating piece is provided with frame
Shape bone opening, described shaped as frame bone locating piece is used for positioning described shaped as frame bone opening；Described upper outer layer corresponding some motor bones location
The position of block offers motor bone opening respectively, and described motor bone locating piece is used for positioning described motor bone opening.
Further, the marginal distribution of the die joint of described upper mold has some stopper slots, corresponding stopper slot in described lower mold
Position be provided with some limited blocks, described stopper slot positions with limited block one_to_one corresponding.
Beneficial effects of the present invention:
The present invention is by being provided with thin skin outer layer and interior furring channels in the die cavity of mould, when by melted light material note
Enter in the die cavity of middle level, will be formed with thin skin outer layer, lightweight middle level and the unmanned plane shell of interior furring channels three in one molding, so
Afterwards thin skin outer layer and interior furring channels are disassembled from die cavity and can be obtained by integrated unmanned plane shell.
Accompanying drawing explanation
The Figure of description of the part constituting the application is used for providing a further understanding of the present invention, and the present invention shows
Meaning property embodiment and explanation thereof are used for explaining the present invention, are not intended that inappropriate limitation of the present invention.In the accompanying drawings:
Fig. 1 is the cross-sectional schematic of the mould of the unmanned plane shell of the present invention；
Fig. 2 is the first angle schematic perspective view of the mould of the unmanned plane shell of the present invention；
Fig. 3 is the second angle schematic perspective view of the mould of the unmanned plane shell of the present invention；
Fig. 4 is the structural representation of upper mold in Fig. 1；
Fig. 5 is the structural representation of lower mold in Fig. 1；
Fig. 6 is the structural representation of the unmanned plane shell of the mould formation of the present invention；
Fig. 7 is the structural representation of the interior furring channels of unmanned plane shell；
Fig. 8 is the structural representation of the upper outer layer of the thin skin outer layer of unmanned plane shell；
Fig. 9 is the structural representation of the lower outer layer of the thin skin outer layer of unmanned plane shell.
Wherein, above-mentioned accompanying drawing includes the following drawings labelling:
1-upper mold, 2-lower mold, 3-die cavity, 4-hand-hole, 5-interior furring channels, 6-lightweight middle level, 7-thin skin outer layer, 11-Os Draconis are fixed
Position portion, 12-stopper slot, 21-locating dowel, 22-limited block, 23-locating convex block, 31-center cavity, 32-arm chamber, 51-shaped as frame bone,
52-motor bone, the upper outer layer of 71-, outer layer under 72-, 111-shaped as frame bone locating piece, 112-motor bone locating piece, 711-shaped as frame bone is opened
Mouthful, 712-motor bone opening, 721-positions hole, 722-detent, 1121-installation portion, 1122-connecting portion, 1123-great circle
Arc, 1124-small arc-shaped.
Detailed description of the invention
For clearer, complete explanation technical scheme, the invention will be further described below in conjunction with the accompanying drawings.
Please also refer to Fig. 1-Fig. 3, the mould of the unmanned plane shell that the detailed description of the invention of the present invention provides includes
Upper mold 1 and lower mold 2.Wherein, refer to Fig. 1, when upper mold 1 and the 2-in-1 mould of lower mold, the internal face of described upper mold 1 is interior with lower mold 2
Wall surrounds die cavity 3.In the present embodiment, refer to Fig. 1, described mould also includes hand-hole 4, described hand-hole 4
Run through described upper mold 1 and communicate with described die cavity 3.
Concrete, please also refer to Fig. 4, Fig. 5, in the present embodiment, described upper mold 1 and lower mold 2 are all square.
Please also refer to Fig. 4, Fig. 5, described die cavity 3 is in butterfly-like and include center cavity 31 and 4 arm chambeies 32；Described center
Chamber 31 is square and is positioned at the center of described die cavity 3, each arm chamber 32 on a corner of described center cavity 31 to far
End extends radially.
The designing points 1 of the present invention is, refer to Fig. 4, is provided with Os Draconis location division 11, described Os Draconis in described die cavity 3
Location division 11 is for installing the interior furring channels 5 of described unmanned plane shell.
Concrete, refer to Fig. 4, in described die cavity 3 is located in described Os Draconis location division 11 and be installed in the interior of described upper mold 1
On wall.Described Os Draconis location division 11 includes the shaped as frame bone locating piece 111 being positioned at upper mold 1 center and is distributed in described shaped as frame bone calmly
Four motor bone locating pieces 112 of block 111 periphery, position.Concrete, described shaped as frame bone locating piece 111 is positioned at center cavity 31, institute
State the position that motor bone locating piece 112 is distributed in the close end in each arm chamber 32.Refer to Fig. 6, described interior furring channels 5 includes
Shaped as frame bone 51 and four motor bones 52；Described shaped as frame bone locating piece 111 is used for installing described shaped as frame bone 51；Described motor bone positions
Block 112 is used for installing described motor bone 52.Wherein, described shaped as frame bone 51 is the circuit part for installing unmanned plane, described
Motor bone 52 is the motor for installing unmanned plane.
In the present embodiment, refer to Fig. 4, described motor bone locating piece 112 includes connecting portion 1122 and installation portion
1121；The inner surface laminating of the outer surface of described installation portion 1121 and motor bone 52；Described connecting portion 1122 is connected to installation portion
Between 1121 and the internal face of upper mold 1, the outer surface of described connecting portion 1122 is similar to the outer surface profile of motor bone 52.So
Design so that the location of described motor bone 52 is more accurate, after also making described motor bone 52 install and connecting portion simultaneously
The excess smoothness of 1122.
Further, refer to Fig. 4, the cross section of described connecting portion 1122 is plum blossom-shaped, including some orthodromes 1123
And some small arc-shapeds 1124；Described orthodrome 1123 and small arc-shaped 1124 spaced connection are arranged；Described orthodrome 1123
Diameter is more than the diameter of small arc-shaped 1124, and described orthodrome 1123 diameter is suitable with the diameter of motor.
The designing points 2 of the present invention is, refer to Fig. 4, and the internal face of described upper mold 1 is provided with for positioning upper outer layer
The outer layer location division of 71；The internal face of described lower mold 2 is provided with the outer layer location division for positioning lower outer layer 72.
In the present embodiment, refer to Fig. 7 and Fig. 8, described upper outer layer 71 and lower outer layer 72 form unmanned plane shell
Thin skin outer layer 7.The internal face of described upper mold 1 is fitted for the outer surface with described upper outer layer 71；The internal face of described lower mold 2 is used
Fit in the outer surface with described lower outer layer 72.
In the present embodiment, described lower outer layer 72 is positioned in described lower mold 2 by following method.Refer to figure
5, the outer layer location division of the lower outer layer 72 in location includes 4 locating dowels 21 and 4 locating convex blocks 23；Please become with reference to Fig. 8, described lower outside
The position of the corresponding locating dowel 21 of layer 72 is provided with hole 721, location, and described locating dowel 21 is used for positioning hole, described location 721.Refer to
Fig. 8, the position of the corresponding locating convex block 23 of described lower outer layer 72 is provided with detent 722, and described locating convex block 23 is used for positioning institute
State detent 722.So that described lower outer layer 72 is positioned in described lower mold 2.
Concrete, refer to Fig. 5,4 locating convex blocks 23 lay respectively in described center cavity 31.Described locating dowel 21 is distributed
Position in the close end in each arm chamber 32.
In the present embodiment, refer to Fig. 7, on location, the outer layer location division of outer layer 71 is also described Os Draconis location division
11, described Os Draconis location division 11 had both been also used for the location of outer layer 71 for the installation of described interior furring channels 5；Described upper outer layer 71
The position of corresponding shaped as frame bone locating piece 111 is provided with shaped as frame bone opening 711, and described shaped as frame bone locating piece 111 is used for positioning described frame
Shape bone opening 711；The position of the corresponding some motor bone locating pieces 112 of described upper outer layer 71 offers motor bone opening 712 respectively,
Described motor bone locating piece 112 is used for positioning described motor bone opening 712.Thus upper outer layer 71 is positioned the inwall of upper mold 1
On face.
Therefore, described outer layer location division specifically includes and is respectively equipped with 4 locating dowels 21 and 4 on the internal face being positioned at lower mold 2
Individual locating convex block 23, and it is positioned at the shaped as frame bone locating piece 111 of upper mold 1 and 4 motor bone locating pieces 112.
In the present embodiment, Os Draconis location division 11, outer layer location division, interior furring channels 5 and thin skin are removed in described die cavity 3
Space beyond outer layer 7 is middle level die cavity, and described middle level die cavity is used for forming lightweight middle level 6.
As can be seen here, the present invention is by being provided with thin skin outer layer 7 and interior furring channels 5 in the die cavity 3 of mould, when molten
After the light material melted injects in the die cavity of middle level from described hand-hole 4, will be formed with thin skin outer layer 7, lightweight middle level 6 and
The unmanned plane shell of interior furring channels 5 three in one molding, then disassembles thin skin outer layer 7 and interior furring channels 5 from die cavity 3
Can be obtained by integrated unmanned plane shell.
What the mould of the present invention formed out is one-body molded by thin skin outer layer 7, lightweight middle level 6 and interior furring channels 5
Unmanned plane shell, the single layer structure gone out with mould molding of the prior art is significantly improved, and it is so that by stratiform
The product of structure composition decreases the most numerous and diverse installation process, also makes the connection between layer structure the tightest simultaneously
Close, firm.
What the mould of the present invention formed out is one-body molded by thin skin outer layer 7, lightweight middle level 6 and interior furring channels 5
Unmanned plane shell.Wherein, lightweight middle level 6 light weight buoyancy is good, simultaneously the volume fraction maximum buoyancy of lightweight middle level 6 part
Good, the unmanned plane shell that therefore mould in this case is formed is conducive to unmanned plane the most floating, and ensure that unmanned plane
Operation is freely on the water.The design of thin skin outer layer 7, is not given only the bonding strength of described unmanned plane shell, makes institute simultaneously yet
State the specious of unmanned plane shell.The design of interior furring channels so that unmanned plane shell has had for installing other circuit parts
Or the position of motor.
In the present embodiment, described light material is EPS expanded material, and described thin skin outer layer 7 and interior furring channels 5 are
Plastic material.The foaming buoyancy of EPS expanded material is good, and beneficially unmanned plane is the most floating and ensure that unmanned plane is made on the water
Industry is freely.Simultaneously all do not have plastics strong because of the ruggedness of EPS expanded material, plasticity, high temperature resistant and water proofing property the most again, the most described thin
Outer cortex 711 and interior furring channels 513 all use plastic material, so can not only ensure that described unmanned plane is the most floating
Also the service life making described unmanned plane while of characteristic is longer.
In the present embodiment, upper mold 1 and lower mold 2 are carried out positioning matched moulds by this case by following method.Refer to
Fig. 4, the marginal distribution of the die joint of described upper mold 1 has four stopper slots 12, refer to Fig. 5, corresponding stopper slot in described lower mold 2
The position of 12 is provided with four limited blocks 22；Refer to Fig. 2 or Fig. 3, described limited block 22 is fixed with described stopper slot 12 one_to_one corresponding
Position thus described upper mold 1 is positioned with lower mold 2.In other embodiments, it may be upper mold 1 be provided with four spacing
Block, lower mold 2 is provided with four stopper slots, or the number of limited block and stopper slot is not 4, as long as can cross upper mold 1 He
Lower mold 2 is positioned together accurately can.
Certainly, the present invention also can have other numerous embodiments, based on present embodiment, those of ordinary skill in the art
On the premise of not making any creative work, obtained other embodiments, broadly fallen into the scope that the present invention is protected.
Claims (9)
1. a mould for unmanned plane shell, including upper die and lower die, the internal face of described upper mold and the internal face of lower mold
Surround die cavity；It is characterized in that,
Being provided with Os Draconis location division in described die cavity, described Os Draconis location division is for installing the interior furring channels of unmanned plane shell；
The internal face of described upper mold is provided with the outer layer location division for positioning upper outer layer；The internal face of described lower mold is provided with use
The outer layer location division of lower outer layer in location；Described upper outer layer and the thin skin outer layer of lower outer layer composition unmanned plane shell；
Removing the space beyond Os Draconis location division, outer layer location division, interior furring channels and thin skin outer layer in described die cavity is middle stratotype
Chamber, described middle level die cavity is used for forming lightweight middle level.
The mould of unmanned plane shell the most according to claim 1, it is characterised in that described die cavity include center cavity and
Some arm chambeies；Described center cavity is square and is positioned at the center of described die cavity, and each arm chamber is from one of described center cavity
Extend radially to far-end on corner.
The mould of unmanned plane shell the most according to claim 2, it is characterised in that described Os Draconis location division is installed in
On the internal face of described upper mold；Described Os Draconis location division includes the shaped as frame bone locating piece being positioned at center cavity and is distributed in each arm chamber
Some motor bone locating pieces of close end position；Described interior furring channels includes shaped as frame bone and some motor bones；Described shaped as frame
Bone locating piece is used for installing described shaped as frame bone；Described motor bone locating piece is used for installing described motor bone.
The mould of unmanned plane shell the most according to claim 3, it is characterised in that described motor bone locating piece includes
Connecting portion and installation portion；The inner surface laminating of the outer surface of described installation portion and motor bone；Described connecting portion is connected to installation portion
And between the internal face of upper mold, the outer surface of described connecting portion is similar to the outer surface profile of motor bone.
The mould of unmanned plane shell the most according to claim 4, it is characterised in that the cross section of described connecting portion in
Plum blossom-shaped, including some orthodromes and some small arc-shapeds；Described orthodrome and small arc-shaped spaced connection are arranged；Described great circle
The diameter of arc is more than the diameter of small arc-shaped.
The mould of unmanned plane shell the most according to claim 1, it is characterised in that the internal face of described upper mold is used for
Fit with the outer surface of described upper outer layer；The internal face of described lower mold is fitted for the outer surface with described lower outer layer.
The mould of unmanned plane shell the most according to claim 6, it is characterised in that the outer layer location of the lower outer layer in location
Portion includes some locating dowels and some locating convex blocks；Described locating convex block is positioned at center cavity, and described locating dowel is distributed in each arm
Chamber is near the position of end；The position of described lower outer layer correspondence locating dowel is provided with hole, location, and described locating dowel is used for positioning described
Hole, location；The position of described lower outer layer correspondence locating convex block is provided with detent, and described locating convex block is used for positioning described location
Groove.
The mould of unmanned plane shell the most according to claim 6, it is characterised in that on location the outer layer location of outer layer
Portion is also described Os Draconis location division, and described Os Draconis location division was both also used for determining of outer layer for the installation of described interior furring channels
Position；The position of described upper outer layer correspondence shaped as frame bone locating piece is provided with shaped as frame bone opening, and described shaped as frame bone locating piece is used for positioning institute
State shaped as frame bone opening；The position of the corresponding some motor bone locating pieces of described upper outer layer offers motor bone opening, described electricity respectively
Machine bone locating piece is used for positioning described motor bone opening.
The mould of unmanned plane shell the most according to claim 1, it is characterised in that the limit of the die joint of described upper mold
Fate is furnished with some stopper slots, and in described lower mold, the position of corresponding stopper slot is provided with some limited blocks, and described stopper slot is with spacing
Block one_to_one corresponding positions.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610668889.XA CN106042240A (en) | 2016-08-16 | 2016-08-16 | Forming die of unmanned aerial vehicle housing |
| PCT/CN2017/070782 WO2018032723A1 (en) | 2016-08-16 | 2017-01-10 | Unmanned aerial vehicle, tool for molding housing of unmanned aerial vehicle, and molding process |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610668889.XA CN106042240A (en) | 2016-08-16 | 2016-08-16 | Forming die of unmanned aerial vehicle housing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106042240A true CN106042240A (en) | 2016-10-26 |
Family
ID=57480996
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610668889.XA Pending CN106042240A (en) | 2016-08-16 | 2016-08-16 | Forming die of unmanned aerial vehicle housing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106042240A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018032723A1 (en) * | 2016-08-16 | 2018-02-22 | 前海星航（深圳）科技有限公司 | Unmanned aerial vehicle, tool for molding housing of unmanned aerial vehicle, and molding process |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101653990A (en) * | 2009-09-25 | 2010-02-24 | 北京航空航天大学 | Integrative solidifying and molding method of minitype unmanned aerial vehicle body and vertical fin and solidifying mold thereof |
| CN105270612A (en) * | 2015-10-23 | 2016-01-27 | 精功（绍兴）复合材料技术研发有限公司 | Unmanned aerial vehicle body |
| US20160122017A1 (en) * | 2014-10-29 | 2016-05-05 | Identified Technologies Corporation | Structure and Manufacturing Process for Unmanned Aerial Vehicle |
| CN206335761U (en) * | 2016-08-16 | 2017-07-18 | 前海星航（深圳）科技有限公司 | A kind of mould of unmanned plane shell |
-
2016
- 2016-08-16 CN CN201610668889.XA patent/CN106042240A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101653990A (en) * | 2009-09-25 | 2010-02-24 | 北京航空航天大学 | Integrative solidifying and molding method of minitype unmanned aerial vehicle body and vertical fin and solidifying mold thereof |
| US20160122017A1 (en) * | 2014-10-29 | 2016-05-05 | Identified Technologies Corporation | Structure and Manufacturing Process for Unmanned Aerial Vehicle |
| CN105270612A (en) * | 2015-10-23 | 2016-01-27 | 精功（绍兴）复合材料技术研发有限公司 | Unmanned aerial vehicle body |
| CN206335761U (en) * | 2016-08-16 | 2017-07-18 | 前海星航（深圳）科技有限公司 | A kind of mould of unmanned plane shell |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018032723A1 (en) * | 2016-08-16 | 2018-02-22 | 前海星航（深圳）科技有限公司 | Unmanned aerial vehicle, tool for molding housing of unmanned aerial vehicle, and molding process |
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