CN207242001U - A kind of small drone wing Quick assembling-disassembling structure - Google Patents
A kind of small drone wing Quick assembling-disassembling structure Download PDFInfo
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- CN207242001U CN207242001U CN201720936770.6U CN201720936770U CN207242001U CN 207242001 U CN207242001 U CN 207242001U CN 201720936770 U CN201720936770 U CN 201720936770U CN 207242001 U CN207242001 U CN 207242001U
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- fuselage
- auxiliary girder
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Abstract
A kind of small drone wing Quick assembling-disassembling structure, including fuselage, fuselage girder, fuselage auxiliary girder, wing, wing girder, wing auxiliary girder, screw, rubber pad, aluminum component, it is characterized in that：The fuselage does exterior skin by composite material, is internally provided with reinforcing rib, which includes fuselage girder, fuselage auxiliary girder, and is respectively run through using a carbon pipe；The wing equally does exterior skin by composite material, is internally provided with reinforcing rib, and wing includes wing girder, wing auxiliary girder, and the wing girder is run through by a carbon pipe, and wing auxiliary girder uses the carbon pipe of one section of 200mm；Aluminum component is bonded with the wing girder, wing auxiliary girder, for fixing screws, screw is used for tightening extruding rubber pad.The structure easy disassembly, it is easy to carry, it is light-weight, built-up time is drastically reduce the area, unmanned plane is rapidly entered working status.
Description
Technical field
The present invention relates to the technical field of structures of unmanned plane, and in particular to a kind of quick peace speed of small drone wing is torn open
Unload structure.
Background technology
At present, unmanned plane be it is a kind of by radio robot or itself programme-control its fly it is unpiloted
Flight equipment, it comes across earliest in the 1920s, the target drone as training used at that time, and the purposes of unmanned plane is very wide
General and cost is relatively low, during use, even if running into surprisingly casualties situation will not occurs.The survival ability of unmanned plane
By force, mobility is good, easy to use, there is extremely important effect in modern war, or even also possesses in civil field wide
Prospect.
Due to the light weight of small drone, it can case take away at any time, so needing the quick attaching of fuselage energy and fractionation, together
It is also to take into account wing to have enough installation strengths, otherwise accident occurs in unmanned plane, causes the loss of economy.
Utility model content
Technical problem to be solved in the utility model is to overcome the defects of existing, there is provided a kind of small drone wing
Structure quickly is disconnected, its technical solution is as follows.
A kind of the quick of small drone wing disconnects structure, including wing, wing girder, wing auxiliary girder, fuselage, fuselage
Girder, fuselage auxiliary girder, pin, spring, it is characterized in that：The fuselage does exterior skin by composite material, is internally provided with reinforcing rib,
The fuselage includes fuselage girder, fuselage auxiliary girder, and is respectively run through using a carbon pipe；The wing is equally done outer by composite material
Covering, is internally provided with reinforcing rib, and wing includes wing girder, wing auxiliary girder, and wing girder is run through by a carbon pipe, wing auxiliary girder
Using the carbon pipe of one section of 200mm；The fuselage girder, fuselage auxiliary girder are equipped with the hole for being used for fixing the pin；The pin
Upper sheathed spring；Connected between the fuselage and wing by above-mentioned carbon pipe.
Preferably：The carbon pipe outside diameter of the fuselage girder is 14mm, internal diameter 12mm, and the carbon pipe outside diameter of wing girder is
12mm, internal diameter 10mm, fuselage auxiliary girder outside diameter are 8mm, and internal diameter 6mm, wing auxiliary girder outside diameter is 6mm, internal diameter 4mm, due to different machines
The wing thickness of type is different, so the length scale of pin and spring depends on the circumstances, its length 60mm here, and pin diameter
For 3mm length 85mm, band baffle ring on pin, for doing spring retainer.
Preferably：The hole that a diameter of 3mm is equipped with fuselage girder carbon pipe, apart from fuselage edge 30mm away from
From；Wing girder will be plugged in fuselage, so wing girder will stretch out wing 100mm, equally on the girder that wing stretches out
The position for the top 70mm that distance is stretched out sets the hole of an a diameter of 3mm, so can just be combined together, use pin lock
Tightly.
Beneficial effect：Its easy disassembly, it is easy to carry, built-up time is drastically reduce the area, unmanned plane is rapidly entered work
Make state.Pin is added while fuselage is designed and sheathed spring and the baffle ring for limit spring on pin, from
And loose one's grip and can set back automatically after pin is extracted.So when assembly and disassembly, only pin need to be extracted, it is not necessary to borrow
Help other instruments.
Brief description of the drawings
Fig. 1 is the structure diagram that the utility model wing and fuselage disconnect.
Wherein：1 is fuselage girder, and 2 be fuselage auxiliary girder, and 3 be fuselage, and 4 be pin, and 5 be spring, and 6 be wing girder, and 7 are
Wing, 8 be wing auxiliary girder.
Embodiment
Unmanned plane includes fuselage, both sides wing group, tail supporting rod, empennage group.Wing group includes two wings, respectively in fuselage
The both sides of front end, empennage group is in the end of tail supporting rod.The light weight of small drone, so most of multiple using glass fibre etc.
Condensation material makes, and wing is also in this way, because wing desired strength is higher, and reinforced structure has been added in inside, has strengthened knot
Structure includes piece auxiliary girder of reinforcing rib and a girder, and the Quick assembling-disassembling structure that we do, is exactly on girder.
The composition of wing is to do exterior skin by composite material, and reinforcing rib is done in inside, in order to save cost, so in wing
Portion's primary structure beam runs through wing using one whole carbon pipe, and the carbon pipe outside diameter of fuselage girder is 14mm, internal diameter 12mm, wing girder
Carbon pipe outside diameter be 12mm, internal diameter 10mm, fuselage auxiliary girder outside diameter is 8mm, internal diameter 6mm, and wing auxiliary girder outside diameter is 6mm, internal diameter
4mm, could so realize grafting.
Because the no locking device of connection after grafting, the locking mode of spring is added using pin, in fuselage
The hole of an a diameter of 3mm is made a call on girder carbon pipe, apart from the distance of fuselage edge 30mm.The girder of wing will be plugged on fuselage
In, so wing girder will stretch out wing 100mm, equally the position on the top 70 that distance is stretched out is beaten on the girder that wing stretches out
The hole of one a diameter of 3mm, the locking of ability realization pin so after grafting.
Embodiment 1：
The girder of wing is generally made at the peak of airfoil lift face, and auxiliary girder is made in the probably 50%-70%'s away from leading edge
, it is necessary to depend on the circumstances within the scope of one.The girder of same fuselage and auxiliary girder position, be with the girder of wing and the position of auxiliary girder
Corresponding ability grafting is entered.So the carbon pipe of the carbon pipe of outside diameter 14mm and outside diameter 8mm is made into the required length of fuselage.Machine
The carbon pipe of body girder needs to make a call to an a diameter of 3mm hole, apart from the distance of fuselage and the edge 30mm of wing plugging direction.In carbon
The direction of Guan Shangkong, main wing carbon is wanted when pipe and fuselage shaping, be towards the leading edge of a wing.
A pin is done while fuselage is designed, a baffle ring is done on pin, for doing the spacing of spring, so
Loose one's grip and can set back automatically after pin is extracted.Pin is directly made in fuselage interior, together with carbon pipe and fuselage jointly into
Type.
The same with fuselage, wing girder and auxiliary girder are also that carbon pipe is directly made in the inside, and wing girder is with outside diameter 12mm's
Carbon pipe, it is exposed in airfoil outer so the girder of wing will grow 100mm due to wanting grafting into the girder of fuselage, for
Fuselage grafting.The carbon pipe of wing auxiliary girder outside diameter 8mm, since the shape of wing has different patterns, institute on different types
Shape with this wing illustrated is trapezoidal, and (right side in Fig. 1) air-foil is narrower more laterally, thus wing auxiliary girder without
Method makes whole, can only make one section, is made in herein using the carbon pipe of total length 200mm, half inside wing, half dew
Outside.
After wing is finished, equally a diameter is made a call in the position on the top 70 that distance is stretched out on the girder that wing stretches out
For the hole of 3mm, pay attention to the direction of perforate, towards the leading edge of wing, so after grafting could realization locked with pin, so
Waited when mounted after finishing, only need to can complete to connect to inserting, the mesh for reaching locking in hole is then directly inserted in a pin
, prevent wing from deviating from.
It is noted here that when carrying out wing punching, hole position, which coordinates, has to accurately, and otherwise hole position is inaccurate, screw
Insert not enter.
Many details are elaborated in the above description in order to fully understand the utility model.But above description
Only it is the preferred embodiment of the utility model, the utility model can be with much next different from other manner described here
Implement, therefore the utility model is from the limitation of specific implementation disclosed above.Any those skilled in the art exist at the same time
Do not depart under technical solutions of the utility model ambit, it is all new to this practicality using the methods and technical content of the disclosure above
Type technical solution makes many possible changes and modifications, or is revised as the equivalent embodiment of equivalent variations.It is every without departing from this
The content of utility model technical solution, any is simply repaiied according to the technical essence of the utility model to made for any of the above embodiments
Change, equivalent variations and modification, in the range of still falling within technical solutions of the utility model protection.
Claims (3)
1. a kind of small drone wing Quick assembling-disassembling structure, including fuselage, fuselage girder, fuselage auxiliary girder, wing, wing master
Beam, wing auxiliary girder, screw, rubber pad, aluminum component, it is characterized in that：The fuselage does exterior skin by composite material, is internally provided with adding
Strengthening tendons, which includes fuselage girder, fuselage auxiliary girder, and is respectively run through using a carbon pipe；The wing is equally by composite wood
Material does exterior skin, is internally provided with reinforcing rib, and wing includes wing girder, wing auxiliary girder, and the wing girder is passed through by a carbon pipe
Wear, wing auxiliary girder uses the carbon pipe of one section of 200mm；Aluminum component is bonded with the wing girder, wing auxiliary girder, for fixing spiral shell
Nail, screw are used for tightening extruding rubber pad.
2. a kind of small drone wing Quick assembling-disassembling structure according to claim 1, it is characterized in that：The fuselage girder
Carbon pipe outside diameter be 14mm, internal diameter 12mm, the carbon pipe outside diameter of wing girder is 12mm, internal diameter 10mm, and fuselage auxiliary girder outside diameter is
10mm, internal diameter 8mm, wing auxiliary girder outside diameter are 8mm internal diameters 6mm；The aluminum component outside diameter of wing girder bonding is 8mm, and wing auxiliary girder glues
The aluminum component outside diameter connect is 6mm, and the aluminum component length that wing girder and wing auxiliary girder are bonded is 10mm, is not equipped with its aluminum component center
M3 threaded holes；Rubber pad outside diameter is 8mm on wing girder, and rubber pad outside diameter is 6mm on wing auxiliary girder, and thickness is respectively 1mm,
Its rubber pad center is respectively equipped with the hole of a diameter of 3mm.
3. a kind of small drone wing Quick assembling-disassembling structure according to claim 1, it is characterized in that：The wing girder
Wing 100mm is stretched out respectively with wing auxiliary girder, while stretches out the carbon tube top end viscous of wing in wing girder and wing auxiliary girder
Aluminum component is connect, the aluminum component will be flushed with carbon tube top end；Screw covers the rubber pad that top external diameter is 8mm and 6mm respectively, is tightened in wing
On the aluminum component of girder and wing auxiliary girder, make rubber pad crimp.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720936770.6U CN207242001U (en) | 2017-07-28 | 2017-07-28 | A kind of small drone wing Quick assembling-disassembling structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720936770.6U CN207242001U (en) | 2017-07-28 | 2017-07-28 | A kind of small drone wing Quick assembling-disassembling structure |
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| Publication Number | Publication Date |
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| CN207242001U true CN207242001U (en) | 2018-04-17 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201720936770.6U Active CN207242001U (en) | 2017-07-28 | 2017-07-28 | A kind of small drone wing Quick assembling-disassembling structure |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108438200A (en) * | 2018-05-11 | 2018-08-24 | 南京航天猎鹰飞行器技术有限公司 | A kind of fixed-wing unmanned plane of fast demountable wing |
| CN108910016A (en) * | 2018-07-23 | 2018-11-30 | 上海歌尔泰克机器人有限公司 | Quick Release wing and unmanned vehicle |
| 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 |
| CN109733590A (en) * | 2019-03-22 | 2019-05-10 | 天津天航智远科技有限公司 | A kind of connection structure between unmanned plane main wing and outer wing |
| CN110435895A (en) * | 2019-07-05 | 2019-11-12 | 嘉兴安行信息科技有限公司 | A kind of replaceable unmanned plane load storehouse |
-
2017
- 2017-07-28 CN CN201720936770.6U patent/CN207242001U/en active Active
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108438200A (en) * | 2018-05-11 | 2018-08-24 | 南京航天猎鹰飞行器技术有限公司 | A kind of fixed-wing unmanned plane of fast demountable wing |
| CN108910016A (en) * | 2018-07-23 | 2018-11-30 | 上海歌尔泰克机器人有限公司 | Quick Release wing and unmanned vehicle |
| 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 |
| CN109250067B (en) * | 2018-08-27 | 2022-04-05 | 上海歌尔泰克机器人有限公司 | Quick detach wing and unmanned vehicles |
| CN109733590A (en) * | 2019-03-22 | 2019-05-10 | 天津天航智远科技有限公司 | A kind of connection structure between unmanned plane main wing and outer wing |
| CN110435895A (en) * | 2019-07-05 | 2019-11-12 | 嘉兴安行信息科技有限公司 | A kind of replaceable unmanned plane load storehouse |
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