CN205906206U - Wing connecting device , wing and aircraft - Google Patents
Wing connecting device , wing and aircraft Download PDFInfo
- Publication number
- CN205906206U CN205906206U CN201620778134.0U CN201620778134U CN205906206U CN 205906206 U CN205906206 U CN 205906206U CN 201620778134 U CN201620778134 U CN 201620778134U CN 205906206 U CN205906206 U CN 205906206U
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- Prior art keywords
- wing
- column spinner
- wing portion
- attachment means
- joint unit
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- 238000003780 insertion Methods 0.000 claims abstract description 16
- 230000037431 insertion Effects 0.000 claims abstract description 16
- 239000003302 ferromagnetic material Substances 0.000 claims description 3
- 230000013011 mating Effects 0.000 claims 1
- 238000009434 installation Methods 0.000 abstract 1
- 230000000694 effects Effects 0.000 description 8
- 238000000034 method Methods 0.000 description 4
- 238000004806 packaging method and process Methods 0.000 description 4
- 239000000463 material Substances 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 2
- NOQGZXFMHARMLW-UHFFFAOYSA-N Daminozide Chemical group CN(C)NC(=O)CCC(O)=O NOQGZXFMHARMLW-UHFFFAOYSA-N 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000284 extract Substances 0.000 description 1
- 238000003032 molecular docking Methods 0.000 description 1
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Abstract
The utility model discloses a wing connecting device, wing and aircraft belongs to aircraft installation technical field, and wherein this wing connecting device includes: first joint unit, interior clamping in first wing portion is including hollow column spinner and flexible piece, the column spinner is used for around its axis rotatoryly, has on the column spinner side rather than the parallel groove of axis, the stiff end of flexible piece is connected with first wing portion, and the expansion end that stretches out and draws back piece is connected with one side bottom surface of column spinner or is located the inslot, the second joint unit, the external second wing portion that is located for can be with first joint unit cooperation so that first wing portion and second wing portion be connected, including the arch of the pole that can insert column spinner hollow structure and ability insertion groove piece, the one end of pole is connected with second wing portion, and protruding piece link bit is on the pole and be close to the position of the pole other end. The utility model has the advantages of the security is high, the durability is high.
Description
Technical field
The utility model is related to aircraft mounting technique field and in particular to a kind of wing attachment means, wing and aircraft.
Background technology
At present, most of aircrafts are completed by assembling, and such as unmanned plane is typically by being completed
A kind of aircraft, is a kind of new industry, has wide market prospects.For save space, the unmanned plane of fixed-wing generally will
Wing merotomizes and is assembled, and a kind of modal point-score is that wing is divided into one section of inner wing and two sections of outer wings.
Between the inside and outside wing, the method for assembling is also had nothing in common with each other, and a kind of method being usually used is grafting, e.g. by outer wing
On bar inject inner wing on hole in, then with one lock lever lock is lived, this method has individual shortcoming, when unmanned plane stall is reclaimed,
Fuselage and ground will occur sharp impacts, thus lock can afford huge impulsive force, and plug assembly will produce can not be extensive
Multiple damage.For example also have a kind of inserting mode again without lock, but a cushion rubber is added on bar, frictionally is outer to fix
The wing, but this mode is very dangerous, is just likely to come off when outer wing is subject to larger load.
Utility model content
Therefore, when the utility model embodiment technical problem to be solved is that in prior art, stall is reclaimed, wing connects
Device can damage, wing can come off when being subject to compared with big load, and the wing attachment means security of prior art is low, durability
Low.
For this reason, a kind of wing attachment means of the utility model embodiment, comprising:
First joint unit, embeds and is located at the first wing portion, the column spinner including hollow and telescopic block；Column spinner be used for around
Its axis rotates, and column spinner side has the groove with its diameter parallel；The fixing end of telescopic block is connected with the first wing portion, stretches
The expansion end of contracting block is connected with the side bottom surface of column spinner or is located in groove；
Second joint unit, external is located at the second wing portion, for can be with the first joint unit cooperation so that the first wing
Portion and the second wing portion connect, including the protruding block of the bar that can insert column spinner hollow structure and energy insertion groove；One end of bar with
Second wing portion connects, and protruding block connects the position being located on bar and near the bar other end.
Preferably, described telescopic block includes slide block and spring, and one end of spring is connected with the first wing portion, spring another
End is connected with slide block.
Preferably, the expansion end of described telescopic block can make the first joint unit and the second joint unit phase when being located in groove
It is connected.
Preferably, described first joint unit also includes rotational stopper；
Rotational stopper connects on the side bottom surface being located at described column spinner and against telescopic block.
Preferably, also include:
First location hole, embeds the first wing portion of being located at；
First alignment pin, external is located at the second wing portion, for matching with the first location hole to insert the first location hole.
Preferably, the other end end face of described bar is coated with ferromagnetic material；
The side of described column spinner is provided with magnet, and magnet is used for being automatically drawn into the bar of insertion column spinner hollow structure.
Preferably, described column spinner includes two sections rotating against, and is embedded with can ejecting in first paragraph column spinner
Two alignment pins, are embedded with the second location hole in second segment column spinner, the when ejecting insertion the second location hole for the second alignment pin
Groove on one section of column spinner is connected with the groove on second segment column spinner.
A kind of wing of the utility model embodiment, comprising: the first wing portion, the second wing portion and above-mentioned wing connect
Device；
First wing portion is connected with the second wing portion by wing attachment means.
A kind of aircraft of the utility model embodiment, including above-mentioned wing.
The technical scheme of the utility model embodiment, has the advantage that
1. the wing attachment means that the utility model embodiment provides, by arranging the column spinner of the first joint unit and stretching
Contracting block and the protruding block of the second joint unit being matched therewith, are dexterously constituted the device of lock, are had using telescopic block
A certain amount of contractility, thereby may be ensured that to be flown in the first, second wing portion being connected by first, second joint unit
Will not fall off in journey, improve the security of wing attachment means.And when the system stall loading this wing attachment means is returned
Time receiving, because telescopic block can make protruding block move in the groove of column spinner, thus the second wing portion can be with respect to the first wing
Portion produces displacement in the horizontal direction, in conjunction with the cushioning effect of telescopic block, in hard material such as colliding surfaces, can substantially reduce
The damage of system, improves durability.
2. the wing attachment means that the utility model embodiment provides, by arranging magnet, using the suction of magnet,
Automatically bar can be sucked, and the length that bar is inhaled into can be limited, thus substantially reducing loaded down with trivial details calibration step during manual-alignment
Suddenly, further increase packaging efficiency, also reduce assembling error rate and scrappage.
3. the wing attachment means that the utility model embodiment provides, by arranging two sections of column spinners, because two sections rotate
Groove on post is staggeredly placed at the beginning, and misalignment, so can be by when bar inserts the hollow structure of one section of column spinner
The bottom surface of another section of column spinner props up, and anti-stopping bar inserts too much and misses default assembling position, leads to assemble unsuccessfully, especially
It is applied to Machine automated production, improve packaging efficiency.
Brief description
In order to be illustrated more clearly that the technical scheme in the utility model specific embodiment, below will be to specific embodiment party
Formula description in required use accompanying drawing be briefly described it should be apparent that, drawings in the following description are the utility model
Some embodiments, for those of ordinary skill in the art, on the premise of not paying creative work, can also root
Obtain other accompanying drawings according to these accompanying drawings.
Fig. 1 is the structural representation of a specific example of wing attachment means in the utility model embodiment 1；
Fig. 2 is the structural representation of a specific example of telescopic block in the utility model embodiment 1；
Fig. 3 is the structural representation of a specific example of the first joint unit in the utility model embodiment 1；
Fig. 4 is the structural representation of a specific example of wing attachment means in the utility model embodiment 2；
Fig. 5 is the structural representation of a specific example in the second wing portion in the utility model embodiment 2；
Fig. 6 is the structural representation of a specific example of column spinner in the utility model embodiment 2.
Reference: 1- first joint unit, 11- column spinner, 110- groove, 113- magnet, 114- second alignment pin, 115-
Second location hole, 12- telescopic block, 121- slide block, 122- spring, 13- rotational stopper, 2- second joint unit, 21- bar, 22-
Protruding block, 3- first location hole, 4- first alignment pin, 10- wing attachment means, 20- the first wing portion, 30- the second wing portion,
A- first paragraph column spinner, b- second segment column spinner.
Specific embodiment
Below in conjunction with accompanying drawing, the technical solution of the utility model is clearly and completely described it is clear that described
Embodiment is a part of embodiment of the utility model, rather than whole embodiments.Based on the embodiment in the utility model, this
The every other embodiment that field those of ordinary skill is obtained under the premise of not making creative work, broadly falls into this practicality
Novel protected scope.
In description of the present utility model, " " center ", " on ", D score, " interior ", " outward " etc. refer to it should be noted that term
The orientation showing or position relationship are based on orientation shown in the drawings or position relationship, be for only for ease of description the utility model and
Simplify description, rather than the device of instruction or hint indication or element must have specific orientation, with specific azimuth configuration
And operation, therefore it is not intended that to restriction of the present utility model.Additionally, term " first ", " second " etc. are only used for describing mesh
, and it is not intended that indicating or hint relative importance.
In description of the present utility model, it should be noted that unless otherwise clearly defined and limited, term " peace
Dress ", " being connected ", " connection " should be interpreted broadly, for example, it may be being fixedly connected or being detachably connected, or integratedly
Connect；Can be to be joined directly together it is also possible to be indirectly connected to by intermediary, can also be the connection of two element internals.Right
For those of ordinary skill in the art, concrete meaning in the utility model for the above-mentioned term can be understood with concrete condition.
As long as additionally, involved technical characteristic in the utility model different embodiments disclosed below is each other
The conflict of not constituting just can be combined with each other.
Embodiment 1
The present embodiment provides a kind of wing attachment means, can be applicable to the assembling of aircraft wing, such as fixed-wing unmanned plane
The inside and outside wing assembling, as shown in figure 1, wing attachment means 10 include: the first joint unit 1 and the second joint unit 2.The
One joint unit 1 embeds the first wing portion 20 of being located at, and the first wing portion 20 can be for example inner wing or outer wing.First
Joint unit 1 includes column spinner 11 and the telescopic block 12 of hollow.Column spinner 11 is used for rotating about the axis thereof, as shown in figure 1, rotation
Post 11 is the cylindrical of hollow, and column spinner 11 can also be the circular cone of hollow, round platform, cuboid etc. according to actual needs.Circle
The column spinner 11 of cylinder shape has side and two bottom surfaces, and column spinner 11 can rotate around its center axis.On column spinner 11 side
There is the groove 110 with its diameter parallel, groove 110 can run through the wall of column spinner 11, thus the cross section of column spinner 11 forms one " c "
Shape.The fixing end of telescopic block 12 is connected with the first wing portion 20, positioned at the right side of column spinner 11, the expansion end of telescopic block 12 with
The side bottom surface of column spinner 11 connects, and now telescopic block 12 is in confined state, or the expansion end of telescopic block 12 is located at groove
In 110, now telescopic block 12 is in part release and stretches or discharge extended configuration completely.
As shown in figure 1, the second joint unit 2 is external is located at the second wing portion 30, for coordinating with the first joint unit 1
So that the first wing portion 20 and the second wing portion 30 connect, the second wing portion 30 is arranged according to the setting in the first wing portion 20,
Can be outer wing or inner wing.Second joint unit 2 includes inserting the bar 21 of column spinner 11 hollow structure and can insert
The protruding block 22 of groove 110.One end of bar 21 is connected with the second wing portion 30, and protruding block 22 connects on bar 21 and near bar 21
The position of the other end.Preferably, the first joint unit 1 and the second joint unit 2 are respectively positioned on the position near the leading edge of a wing.
When being not connected with original state, telescopic block 12 is tightly pressed against on the side bottom surface of column spinner 11, and telescopic block 12 is pressed in
Position on column spinner 11 side bottom surface be column spinner 11 on groove 110 carry out clockwise or counterclockwise 180 ° (can also
It is adjusted according to actual needs) position that reaches afterwards.Protruding block 22 is with respect to bar 21 central axis in space coordinates
With respect to column spinner 11 central axis, the position in space coordinates is identical with telescopic block 12, with the first joint unit 1 for position
Match with the external surface shape in the first wing portion 20 and the second wing portion 30 after the second joint unit 2 cooperation.When connecting, first
First the second wing portion 30 is rotated 180 ° around bar 21 central axis, so that protruding block 22 and groove 110 is alignd, then barre 21 inserts
Protruding block 22 is made to be fully inserted among column spinner 11, rotation the second wing portion 30 is rotated post 11 simultaneously and rotates, and rotates 180 °
Afterwards, the telescopic block 12 being originally pressed on column spinner 11 slips in groove 110, contacts with protruding block 22 and because the effect of contractility is stretched
Contracting block 12 pushes down protruding block 22, makes protruding block 22 cannot skid off groove 110 easily.The contractility of the telescopic block 12 after docking is one
Individual crucial index, this power must assure that the power of the disengaging producing more than maximum load on wing, and it can be by testing
Arrive.During dismounting, need to exert oneself to pull the second wing portion 20 to make telescopic block 12 return to beyond groove 110, then rotate the second wing
Portion 20, column spinner 11 rotates simultaneously, and telescopic block 12 is withstood by the side bottom surface of column spinner 11, extracts the second machine after rotatable 180 °
Alar part 20, the first joint unit 1 sets back.This dismountable structure, improve wing attachment means durability and can
Reusability, and substantially reduce production cost.
Above-mentioned wing attachment means, by arranging the column spinner of the first joint unit and telescopic block and being matched therewith
The protruding block of the second joint unit, dexterously constitutes the device of lock, has a certain amount of contractility using telescopic block, thus can
Be will not fall off in flight course with the first, second wing portion ensureing to connect by first, second joint unit, improve machine
The security of wing attachment means.And when load this wing attachment means system stall reclaim when, due to telescopic block can make convex
Bittiness move in the groove of column spinner, thus the second wing portion can produce position in the horizontal direction with respect to the first wing portion
Move, in conjunction with the cushioning effect of telescopic block, in hard material such as colliding surfaces, the damage of system can be substantially reduced, improve resistance to
The property used.
Preferably, as shown in Fig. 2 telescopic block 12 includes slide block 121 and spring 122, one end of spring 122 and the first wing
Portion 20 connects, and the other end of spring 122 is connected with slide block 121, and the contractility of telescopic block 12 depends on the spring of spring 122
Pressure.The expansion end of telescopic block 12 can make the first joint unit 1 and the second joint unit 2 company of matching when being located in groove 110
Connect.It is further preferred that slide block 121 be sized to be slightly smaller than protruding block 22, so can prevent dismounting when protruding block 22 skid off groove
110, thus block to rotate.The impact caused to the rotation of column spinner 11 in order to reduce slide block 121, slide block 121 is general
Require surface very smooth, preferably use the material that hardness is high, skin-friction force is little.It will be understood by those of skill in the art that
Telescopic block is not limited to the concrete structure of above-mentioned slide block and spring, and the device that other are capable of extension and contraction control is all possible.
Preferably, as shown in figure 3, the first joint unit 1 also includes rotational stopper 13.Rotational stopper 13 connection is located at
On the side bottom surface of column spinner 11 and against telescopic block 12.Due to the effect of rotational stopper 13, in first, second wing portion group
During dress, the second wing portion that can only limit at the beginning is rotated in one direction, thus avoid during appearance assembling around great circle and
Assemble the situation making a mistake, particularly when being assembled using automation equipments such as robots, and then improve assembling effect
Rate.
Embodiment 2
The present embodiment provides a kind of wing attachment means, as shown in figure 4, except including wing attachment means in embodiment 1
Feature beyond, also include: the first location hole 3 and the first alignment pin 4.First location hole 3 embeds the first wing portion 20 of being located at.The
One alignment pin 4 is external to be located at the second wing portion 30, for matching with the first location hole 3 to insert the first location hole 3.
When the effect of the first location hole 3 and the first alignment pin 4 is mainly docked in first, second wing portion, auxiliary is fixed
Position, is further ensured that the first wing portion 20 and the external surface shape in the second wing portion 30 match.And the first location hole 3 and
The cooperation of one alignment pin 4 is also prevented from first, second wing portion in flight course and rotates against, and improves stability.
When connecting, first the second wing portion 30 is rotated 180 ° around bar 21 central axis, make protruding block 22 and groove 110 right
Together, then barre 21 inserts the first wing portion 20, and insertion depth is h1, so that protruding block 22 is fully inserted among column spinner 11, rotation
The second wing portion 30 of turning is rotated post 11 simultaneously and rotates, and rotates the end in end face to the first alignment pin 4 and the first wing portion 20
When face flushes (probably rotating to 150 ° about), adjust the end face of the first alignment pin 4 and the end contact in the first wing portion 20, continue
To after 180 °, the first alignment pin 4 be aligned inserts the first location hole 3 for continuous rotation, and the telescopic block 12 being originally pressed on column spinner 11 is sliding
Enter in groove 110, contact with protruding block 22 and because the effect telescopic block 12 of contractility pushes down protruding block 22, make the protruding block 22 cannot
Skid off groove 110 easily.
As shown in figure 5, insertion depth is h1Length h equal to bar 212Deduct length h of the first alignment pin 43, protruding block 22
Length should be less than insertion depth h1, convex when the end face in end face and the first wing portion 20 of the first alignment pin 4 to ensure
Bittiness 22 are fully inserted in groove 110, and then ensure that telescopic block 12 can smoothly discharge stretching, extension.
Preferably, the other end end face of bar 21 is coated with ferromagnetic material.The side of column spinner 11 is provided with magnet
113, magnet 113 is used for being automatically drawn into the bar 21 of insertion column spinner 11 hollow structure.It is further preferred that magnet 113 can position
It is arranged at above-mentioned insertion depth h1Bar 21 by the suction of magnet, can be sucked, and can limit bar 21 quilt by place automatically
The length sucking, thus substantially reducing loaded down with trivial details calibration steps during manual-alignment, further increasing packaging efficiency, also reducing
Assembling error rate and scrappage.
Preferably, as shown in fig. 6, column spinner 11 includes two sections rotating against, two sections coaxial against connection, with magnet
113 present positions are line of demarcation (can also be not provided with magnet 113), are divided into first paragraph column spinner a and second segment column spinner b.The
It is embedded with the second alignment pin 114 that can eject in one section of column spinner a, in second segment column spinner b, be embedded with the second location hole 115,
Groove on first paragraph column spinner a when ejecting insertion the second location hole 115 for the second alignment pin 114 and second segment column spinner b
Groove be connected.
When connecting, first the second wing portion 30 is rotated 180 ° around bar 21 central axis, make protruding block 22 and second segment
The groove alignment of column spinner b, then barre 21 insertion the first wing portion 20, insertion depth is h1(i.e. at magnet 113 present position),
Protruding block 22 is made to be fully inserted among column spinner 11, rotation the second wing portion 30 drives second segment column spinner b to rotate, now simultaneously
First paragraph column spinner a does not turn, and (probably rotates to 150 ° of left sides when rotation is aligned to the second alignment pin 114 with the second location hole 115
Right) when, the second alignment pin 114 ejects insertion the second location hole 115, on the groove on first paragraph column spinner a and second segment column spinner b
Groove be connected, the now end face in the end face of the first alignment pin 4 and the first wing portion 20, continue rotation to after 180 °, the
One alignment pin 4 be aligned insertion the first location hole 3, the telescopic block 12 being originally pressed on column spinner 11 slips in the groove being connected, and
Protruding block 22 contacts and because the effect telescopic block 12 of contractility pushes down protruding block 22, makes protruding block 22 cannot skid off groove easily.
Above-mentioned wing attachment means, by arranging two sections of column spinners, because the groove on two sections of column spinners is staggered at the beginning
Place, and misalignment, so can be supported by the bottom surface of another section of column spinner when bar inserts the hollow structure of one section of column spinner
Live, anti-stopping bar inserts too much and misses default assembling position, leads to assemble unsuccessfully, is particularly well-suited to Machine automated life
Produce, improve packaging efficiency.
Embodiment 3
The present embodiment provides a kind of wing, comprising: the first wing portion 20, the second wing portion 30 and above-described embodiment 1 or 2
Wing attachment means 10.First wing portion 20 is connected with the second wing portion 30 by wing attachment means 10.This wing has peace
The advantage of Quan Xinggao, durability height etc..
Embodiment 4
The present embodiment provides a kind of aircraft, for example, can be unmanned plane, including the wing of above-described embodiment 3.This aircraft has
Have the advantages that safe, durability is high etc..
Obviously, above-described embodiment is only intended to clearly illustrate example, and the not restriction to embodiment.Right
For those of ordinary skill in the art, can also make on the basis of the above description other multi-forms change or
Change.There is no need to be exhaustive to all of embodiment.And the obvious change thus extended out or
Change among the protection domain created still in the utility model.
Claims (9)
1. a kind of wing attachment means are it is characterised in that include:
First joint unit (1), embeds and is located at the first wing portion (20), the column spinner (11) including hollow and telescopic block (12)；
Column spinner (11) is used for rotating about the axis thereof, and column spinner (11) side has the groove (110) with its diameter parallel；Telescopic block
(12) fixing end is connected with the first wing portion (20), and the expansion end of telescopic block (12) is connected with the side bottom surface of column spinner (11)
Connect or be located in groove (110)；
Second joint unit (2), external is located at the second wing portion (30), for can be with the first joint unit (1) cooperation so that the
One wing portion (20) and the second wing portion (30) connect, including the bar (21) that can insert column spinner (11) hollow structure with can insert
The protruding block (22) of groove (110)；One end of bar (21) is connected with the second wing portion (30), and protruding block (22) connects positioned at bar (21)
The position of upper and close bar (21) other end.
2. wing attachment means according to claim 1 are it is characterised in that described telescopic block (12) includes slide block (121)
With spring (122), one end of spring (122) is connected with the first wing portion (20), the other end of spring (122) and slide block (121)
Connect.
3. wing attachment means according to claim 1 are it is characterised in that the expansion end of described telescopic block (12) is located at
Groove (110) can make the first joint unit (1) in mating connection with the second joint unit (2) when interior.
4. wing attachment means according to claim 1 are it is characterised in that described first joint unit (1) also includes revolving
Turn confinement block (13)；
Rotational stopper (13) connects on the side bottom surface being located at described column spinner (11) and against telescopic block (12).
5. wing attachment means according to claim 1 are it is characterised in that also include:
First location hole (3), embeds the first wing portion (20) of being located at；
First alignment pin (4), external is located at the second wing portion (30), for matching with the first location hole (3) to insert first
Location hole (3).
6. wing attachment means according to claim 5 are it is characterised in that coat on the other end end face of described bar (21)
There is ferromagnetic material；
The side of described column spinner (11) is provided with magnet (113), and magnet (113) is used for being automatically drawn in insertion column spinner (11)
The bar (21) of hollow structure.
7. wing attachment means according to claim 5 are it is characterised in that described column spinner (11) includes rotating against
Two sections, be embedded with the second alignment pin (114) that can eject in first paragraph column spinner, be embedded with second in second segment column spinner fixed
Position hole (115), the groove and the on first paragraph column spinner when ejecting insertion the second location hole (115) for the second alignment pin (114)
Groove on two sections of column spinners is connected.
8. a kind of wing is it is characterised in that include: the first wing portion (20), the second wing portion (30) and such as claim 1-7 are appointed
Wing attachment means (10) described in one；
First wing portion (20) is connected with the second wing portion (30) by wing attachment means (10).
9. a kind of aircraft is it is characterised in that include wing as claimed in claim 8.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620778134.0U CN205906206U (en) | 2016-07-23 | 2016-07-23 | Wing connecting device , wing and aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620778134.0U CN205906206U (en) | 2016-07-23 | 2016-07-23 | Wing connecting device , wing and aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205906206U true CN205906206U (en) | 2017-01-25 |
Family
ID=57805753
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620778134.0U Expired - Fee Related CN205906206U (en) | 2016-07-23 | 2016-07-23 | Wing connecting device , wing and aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205906206U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106114816A (en) * | 2016-07-23 | 2016-11-16 | 北京耐威智能科技有限公司 | A kind of wing attachment means, wing and aircraft |
| CN108031129A (en) * | 2017-12-18 | 2018-05-15 | 深圳市中航电科技有限公司 | Easy-to-mount fuselage docks connected structure with wing |
| CN110077573A (en) * | 2019-06-13 | 2019-08-02 | 天津天航智远科技有限公司 | A kind of rotary fixing structure of unmanned plane main wing and outer wing |
-
2016
- 2016-07-23 CN CN201620778134.0U patent/CN205906206U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106114816A (en) * | 2016-07-23 | 2016-11-16 | 北京耐威智能科技有限公司 | A kind of wing attachment means, wing and aircraft |
| CN106114816B (en) * | 2016-07-23 | 2018-06-15 | 北京耐威智能科技有限公司 | A kind of wing attachment device, wing and aircraft |
| CN108031129A (en) * | 2017-12-18 | 2018-05-15 | 深圳市中航电科技有限公司 | Easy-to-mount fuselage docks connected structure with wing |
| CN108031129B (en) * | 2017-12-18 | 2024-01-02 | 深圳市中航电科技有限公司 | Butt joint grafting structure of fuselage and wing convenient to dismouting |
| CN110077573A (en) * | 2019-06-13 | 2019-08-02 | 天津天航智远科技有限公司 | A kind of rotary fixing structure of unmanned plane main wing and outer wing |
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