CN107600414A - A kind of unmanned plane that can be taken off and quickly be assembled without instrument in case - Google Patents
A kind of unmanned plane that can be taken off and quickly be assembled without instrument in case Download PDFInfo
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- CN107600414A CN107600414A CN201710815565.9A CN201710815565A CN107600414A CN 107600414 A CN107600414 A CN 107600414A CN 201710815565 A CN201710815565 A CN 201710815565A CN 107600414 A CN107600414 A CN 107600414A
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Abstract
The invention discloses a kind of unmanned plane that can be taken off and quickly be assembled without instrument in case, including fuselage main body, outer wing and the central wing for being removably mounted on fuselage main body upper end, the central wing side is detachably connected by tail supporting rod and outer wing, the tail supporting rod rear and front end is provided with rotary wings, and the fuselage main body end is provided with rear-mounted propeller.This unmanned plane forms fixed-wing by central wing and outer wing, and four rotors are formed by tail supporting rod and the rotary wings of its end, this unmanned plane improves airplane efficiency and speed using fixed-wing, reduces energy consumption, VTOL is realized using four rotors, uav belly is landed and mitigates unmanned plane weight.Meanwhile this unmanned plane is realized and quickly loaded and unloaded without instrument, and assembling is completed within 2 minutes, and it can complete to assemble and take off directly in packing case, this unmanned plane can give full play to its advantage at emergent aspect, be widely used in the multiple fields such as civilian, military.
Description
Technical field
The present invention relates to vehicle technology field, more particularly, to a kind of nothing that can be taken off and quickly be assembled without instrument in case
It is man-machine.
Background technology
With the development of aeronautical technology, unmanned air vehicle technique is increasingly mature, civilian unmanned plane usually as toy, model plane,
It is also used for taking photo by plane simultaneously and goods delivers the fields such as transport, has broad application prospects.At present, fixed-wing unmanned plane and four rotations
Wing unmanned plane is two kinds of more conventional unmanned plane structures；Wherein, there is big power waste, high energy consumption, fly in four rotor wing unmanned aerial vehicles
The deficiencies of line efficiency is low, flying speed is slow and course continuation mileage is short；The stability of equilibrium of fixed-wing unmanned plane is poor, it is difficult to remains low
Speed flight and hovering, especially can not VTOL, to taking off and the ground environment requirement of landing place is high.
Also, unmanned plane is most to have the problems such as dismounting is difficult, it is difficult to without instrument assembly or disassembly, it is difficult to pack, it is impossible to
Adapt to the requirement of quick despatch.Though part unmanned plane can realize dismounting, it might even be possible to be placed on some packing cases after dismounting
In, the requirement but faced without suitable departure location or to departure location is of a relatively high.
The content of the invention
In view of the above-mentioned problems, the invention provides a kind of unmanned plane that can be taken off and quickly be assembled without instrument in case, it was both
With fixed-wing, it may have four rotors, improve flight efficiency height and stability of equilibrium is high, VTOL can be completed, and be easy to
Dismounting, can also complete landing on packing case.
The present invention is that technical scheme is used by solving its technical problem：
A kind of unmanned plane that can be taken off and quickly be assembled without instrument in case, including fuselage main body, outer wing and removably
Central wing in fuselage main body, the central wing side are detachably connected by tail supporting rod and outer wing, the tail supporting rod
Rear and front end is provided with rotary wings, and the fuselage main body end is provided with rear-mounted propeller.
As an improvement of entering for such scheme, support tube is equipped with the central wing, tail supporting rod and outer wing, it is described outer
The wing, central wing and tail supporting rod are locked by the first locking device.
As an improvement of entering for such scheme, first locking device includes fixed grab and can be with the fixed grab
The turn buckle of clamping fixed, the fixed grab and turn buckle are selected one and are arranged on outer wing, on another centrally disposed wing, the
One locking device is fixed outer wing and central wing, and tail supporting rod is clamped under the cooperation clamping of fixed grab and turn buckle
Between outer wing and central wing.
As an improvement of entering for such scheme, first locking device is arranged at the back of the body of outer wing, central wing and tail supporting rod
Face.
As an improvement of entering for such scheme, described central wing one end is connected by gripping mechanism with the fuselage body,
The central wing other end is connected by the second locking device with the fuselage body.
As an improvement of entering for such scheme, the gripping mechanism includes fixing groove and can be clamped in the fixing groove
Withstanding tight block, the fixing groove and withstanding tight block are selected on a centrally disposed wing, and another is arranged in fuselage main body, second lock
Tight device includes cupboard button device and the slot mechanism that can be locked with cupboard button device, and the cupboard button device and slot mechanism select one
In central wing, another is arranged in fuselage main body.
As an improvement of entering for such scheme, in addition to empennage, the empennage both-side ends by an attachment means with
Corresponding tail supporting rod end is detachably connected.
As an improvement of entering for such scheme, the empennage includes left and right empennage, and the left and right empennage rotationally connects
Connect and locked by the 3rd locking device, the empennage is in inverted V-shape during locking.
As an improvement of entering for such scheme, the 3rd locking device includes clamping element and can matched somebody with somebody with clamping element
The spinner component of clamping is closed, clamping element and the spinner component is selected one and is arranged on port tailplane, and another is arranged on starboard tailplane
On.
As an improvement of entering for such scheme, the 3rd locking device is arranged at the front of empennage.
The beneficial effects of the invention are as follows：
This unmanned plane forms fixed-wing by central wing and outer wing, and forms four by tail supporting rod and the rotary wings of its end
Rotor, this unmanned plane improve airplane efficiency and speed using fixed-wing, reduce energy consumption, VTOL is realized using four rotors,
Uav belly is landed and mitigate unmanned plane weight.
Meanwhile this unmanned plane is realized and quickly loaded and unloaded without instrument by being detachably connected between each part, operating personnel can be with
Each part of unmanned plane after the completion of dismounting is placed in packing case, in order to store and carry, also, due to this unmanned plane
Four rotors are taken off characteristic and the convenience without instrument handling, and this unmanned plane is completed to assemble directly in packing case, and directly wrapped
Taken off in vanning, greatly facilitate the use of unmanned plane, whole assembling and take-off process are from opening the box to assembling
Into just being completed within 2 minutes.This unmanned plane can give full play to its advantage due to its agility and reliability, at emergent aspect,
Tool is of great significance, and therefore, the applicable field of this unmanned plane is quite varied, includes the multiple fields such as civilian, military.
Brief description of the drawings
Technical scheme in order to illustrate the embodiments of the present invention more clearly, make required in being described below to embodiment
Accompanying drawing is briefly described.Obviously, described accompanying drawing is the part of the embodiment of the present invention, rather than is all implemented
Example, on the premise of not paying creative work, other that can also be obtained according to these accompanying drawings are set those skilled in the art
Meter scheme and accompanying drawing：
Fig. 1 is the structural representation one of present pre-ferred embodiments；
Fig. 2 is the structural representation two of present pre-ferred embodiments；
Fig. 3 is the top view of present pre-ferred embodiments；
Fig. 4 is the exploded view of present pre-ferred embodiments；
Fig. 5 is structural representation when empennage folds in present pre-ferred embodiments.
Embodiment
Carried out below with reference to the design of embodiment and accompanying drawing to the present invention, concrete structure and caused technique effect clear
Chu, it is fully described by, to be completely understood by the purpose of the present invention, feature and effect.Obviously, described embodiment is this hair
Bright part of the embodiment, rather than whole embodiments, based on embodiments of the invention, those skilled in the art is not paying
The other embodiment obtained on the premise of creative work, belongs to the scope of protection of the invention.
Referring to figs. 1 to Fig. 5, a kind of unmanned plane that can be taken off and quickly be assembled without instrument in case, including it is fuselage main body 1, outer
The wing 4 and the central wing 2 being removably mounted in fuselage main body 1, it is preferred that the central wing 2 is arranged on fuselage main body 1
Upper end, the side of central wing 2 are detachably connected by tail supporting rod 3 and outer wing 4, and the rear and front end of tail supporting rod 3 is provided with
Rotary wings 5, the end of fuselage main body 1 are provided with rear-mounted propeller 6, meanwhile, this unmanned plane also includes empennage 8, the empennage 8
Both-side ends are detachably connected by an attachment means 9 with the corresponding end of tail supporting rod 3.This unmanned plane, pass through the He of central wing 2
Outer wing 4 forms fixed-wing, also, forms four rotors by the rotary wings 5 of tail supporting rod 3 and its end, four of four rotor
Rotary wings 5 are evenly distributed in two fixed-wing front and back, so as to form the unmanned plane of mixed layout.In addition, fuselage main body 1 with
It is detachable between empennage 8 and tail supporting rod 3 between central wing 2, tail supporting rod 3 and outer wing 4 between central wing 2, in order to store
And carrying.
Wherein, referring to Figures 1 and 2, support tube 21 is equipped with the central wing 2, tail supporting rod 3 and outer wing 4, it is described outer
The wing 4, central wing 2 and tail supporting rod 3 are locked by the first locking device 7.First locking device 7 be mainly used in by outer wing 4, in
The centre wing 2 and tail supporting rod 3 are locked, and prevent outer wing 4 and tail supporting rod 3 from situation about being separated with central wing 2 occurs, and realize Fast Installation.
The one of which embodiment of first locking device 7 is provided in the present embodiment：First locking device 7 include fixed grab and
Can be with the turn buckle of the fixed grab clamping fixed, it is preferred that first locking device 7 is arranged at outer wing 4, central wing 2
With the back side of tail supporting rod 3.The fixed grab and turn buckle are selected one and are arranged on outer wing 4, on another centrally disposed wing 2,
I.e. fixed grab and turn buckle are separately mounted on outer wing 4 and central wing 2, two kinds of facilities.First locking device 7 exists
Under the cooperation clamping of fixed grab and turn buckle, outer wing 4 and central wing 2 are fixed, and tail supporting rod 3 is clamped in outer wing 4 with
Between entreating the wing 2, so as to realize locking.When this part is dismantled, it is only necessary to separate fixed grab and turn buckle, you can realize outer wing
4th, the separation of central wing 2 and the three of tail supporting rod 3, it is very convenient.
Wherein, reference picture 1 and Fig. 4, described one end of central wing 2 is connected by gripping mechanism with the fuselage body 1, described
The other end of central wing 2 is connected by the second locking device 11 with the fuselage body 1.Preferably, the gripping mechanism includes solid
Determine groove and the withstanding tight block that can be clamped in the fixing groove, the fixing groove and withstanding tight block are selected on a centrally disposed wing 2, another
Individual to be arranged in fuselage main body 1, i.e., fixing groove and withstanding tight block are separately positioned in central wing 2 and fuselage main body 1, two kinds of setting sides
Formula.Second locking device 11 includes cupboard button device and the slot mechanism that can be locked with cupboard button device, the rotation
Buckle mechanism and slot mechanism are selected one and are arranged in central wing 2, and another is arranged in fuselage main body 1, similarly, cupboard button device and card
Groove mechanism is separately positioned in central wing 2 and fuselage main body 1, two kinds of set-up modes.This part is in dismounting, it is necessary to first solve
Cupboard button device and slot mechanism are opened, then fixing groove and withstanding tight block are separated, so as to realize the separation of central wing 2 and fuselage main body 1.
Second locking device 11 disclosed above is only one of locking mode, and it can also use other locking modes, as above
The forms such as the first locking device 7 stated.
Further, reference picture 1, Fig. 4 and Fig. 5, the empennage 8 include port tailplane 81 and starboard tailplane 82, the port tailplane 81
It is rotatably coupled with starboard tailplane 82, and is locked by the 3rd locking device 10, during locking, the empennage 8 is in inverted V-shape.It is excellent
Choosing, the 3rd locking device 10 includes clamping element and can coordinate the spinner component of clamping, the card with clamping element
Tight element and spinner component are selected one and are arranged on port tailplane 81, and another is arranged on starboard tailplane 82.The clamping element and rotation
Buckle assembly is separately positioned on port tailplane 81 and starboard tailplane 82, two kinds of set-up modes.3rd locking device disclosed above
10 be only one of locking mode, and it can also use the shape such as other locking modes, the first locking device 7 described above
Formula.Preferably, the 3rd locking device 10 is arranged at the front of empennage 8.This part first passes through attachment means 9 in dismounting
The connection between tail supporting rod 3 and empennage 8 is untied, then unties the 3rd locking device 10, port tailplane 81 and starboard tailplane 82 are rolled over
It is folded, structural representation when wherein Fig. 5 is 82 folded state of port tailplane 81 and starboard tailplane.
The first locking device 7, the second locking device 11 and the 3rd locking device 10 used in above-mentioned attachment structure,
The locking mode limited in only the present embodiment is not limited, as long as realizing locking function.
Reference picture 1, this unmanned plane realize the mixed layout of four rotors and fixed-wing so that this unmanned plane both possesses solid
Determine airplane efficiency and the speed that wing unmanned plane is possessed, and reduce the energy consumption of unmanned plane, be also equipped with four rotor wing unmanned aerial vehicle institutes
The ability such as the VTOL having and belly landing, also reduces the weight of the setting and unmanned plane of undercarriage in itself.
Reference picture 4, this unmanned function realize fast quick-detach, resolve into fuselage main body 1, central wing 2, tail supporting rod 3, outer wing 4,
Rotary wings 5 and the grade part of empennage 8, wherein empennage 8 can also be folded, due to the structure design of above-mentioned all parts, and
The convenience of the locking devices such as the first locking device 7, the second locking device 11 and the 3rd locking device 10 operation, operating personnel
This unmanned plane can be dismounted without instrument.Also, these above-mentioned parts can be placed on inside packing case after removal,
Realize and very easily store and carry.In addition, this unmanned plane is without tool assemble and four rotors by the way of taking off, because
This, after directly opening the box, operating personnel directly can be assembled UAV Components in packing case, operator
Without using instrument, the unmanned plane after being completed directly takes off member on packing case.Above-mentioned whole quick assembling and rising is flown over
Journey, from opening the box to being completed, just it can be completed within 2 minutes.Just because of the agility and reliability of this unmanned plane,
Its advantage can be given full play at emergent aspect, can be played a positive role in various emergency occasion, tool is of great significance.Cause
This, the applicable field of this unmanned plane is quite varied, includes the multiple fields such as civilian, military.
Described above-described embodiment is that the above of the present invention is further described, but this should not be interpreted as into this hair
The scope of bright above-mentioned theme is only limitted to above-described embodiment, all models that the present invention is belonged to based on the technology that the above is realized
Enclose.
Claims (10)
- A kind of 1. unmanned plane that can be taken off and quickly be assembled without instrument in case, it is characterised in that：Including fuselage main body (1), outer wing (4) and the central wing (2) that is removably mounted in fuselage main body (1), central wing (2) side passes through tail supporting rod (3) It is detachably connected with outer wing (4), tail supporting rod (3) rear and front end is provided with rotary wings (5), fuselage main body (1) end End is provided with rear-mounted propeller (6).
- A kind of 2. unmanned plane that can be taken off and quickly be assembled without instrument in case according to claim 1, it is characterised in that：Institute State and support tube (21) is equipped with central wing (2), tail supporting rod (3) and outer wing (4), the outer wing (4), central wing (2) and tail Strut (3) is locked by the first locking device (7).
- A kind of 3. unmanned plane that can be taken off and quickly be assembled without instrument in case according to claim 2, it is characterised in that：Institute Stating the first locking device (7) includes fixed grab and can be with the turn buckle of the fixed grab clamping fixed, the fixed grab With turn buckle one is selected to be arranged on outer wing (4), on another centrally disposed wing (2), the first locking device in fixed grab and It is under the cooperation clamping of turn buckle, outer wing (4) and central wing (2) is fixed, and tail supporting rod (3) is clamped in outer wing (4) and center Between the wing (2).
- 4. a kind of unmanned plane that can be taken off and quickly be assembled without instrument in case according to Claims 2 or 3, its feature exist In：First locking device (7) is arranged at the back side of outer wing (4), central wing (2) and tail supporting rod (3).
- A kind of 5. unmanned plane that can be taken off and quickly be assembled without instrument in case according to claim 1, it is characterised in that：Institute State central wing (2) one end to be connected with the fuselage body (1) by gripping mechanism, central wing (2) other end passes through second Locking device (11) is connected with the fuselage body (1).
- A kind of 6. unmanned plane that can be taken off and quickly be assembled without instrument in case according to claim 5, it is characterised in that：Institute Stating gripping mechanism includes fixing groove and the withstanding tight block that can be clamped in the fixing groove, and the fixing groove and withstanding tight block select a setting In central wing (2), another is arranged in fuselage main body (1), and second locking device (11) includes cupboard button device and can The slot mechanism locked with cupboard button device, the cupboard button device and slot mechanism are selected one and are arranged in central wing (2), another It is individual to be arranged in fuselage main body (1).
- A kind of 7. unmanned plane that can be taken off and quickly be assembled without instrument in case according to claim 1, it is characterised in that：Also Including empennage (8), empennage (8) both-side ends are detachable by an attachment means (9) and corresponding tail supporting rod (3) end Connection.
- A kind of 8. unmanned plane that can be taken off and quickly be assembled without instrument in case according to claim 7, it is characterised in that：Institute Stating empennage (8) includes left and right empennage (81,82), and the left and right empennage (81,82) is rotatably coupled and by the 3rd locking Device (10) is locked, and the empennage (8) is in inverted V-shape during locking.
- A kind of 9. unmanned plane that can be taken off and quickly be assembled without instrument in case according to claim 8, it is characterised in that：Institute Stating the 3rd locking device (10) includes clamping element and can coordinate the spinner component of clamping, the clamping element with clamping element One is selected with spinner component to be arranged on port tailplane (81), another is arranged on starboard tailplane (82).
- 10. a kind of unmanned plane that can be taken off and quickly be assembled without instrument in case according to claim 7 or 8, its feature exist In：3rd locking device (10) is arranged at the front of empennage (8).
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710815565.9A CN107600414B (en) | 2017-09-11 | 2017-09-11 | Unmanned aerial vehicle capable of taking off in box and rapidly assembling without tools |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710815565.9A CN107600414B (en) | 2017-09-11 | 2017-09-11 | Unmanned aerial vehicle capable of taking off in box and rapidly assembling without tools |
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| Publication Number | Publication Date |
|---|---|
| CN107600414A true CN107600414A (en) | 2018-01-19 |
| CN107600414B CN107600414B (en) | 2024-03-15 |
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| CN201710815565.9A Active CN107600414B (en) | 2017-09-11 | 2017-09-11 | Unmanned aerial vehicle capable of taking off in box and rapidly assembling without tools |
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Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108341052A (en) * | 2018-02-13 | 2018-07-31 | 北京航空航天大学 | Composite rotor aircraft |
| CN108657414A (en) * | 2018-05-15 | 2018-10-16 | 北京航空航天大学 | A kind of attachment device and the connection method of unmanned plane central wing, outer wing and shoe |
| CN108860570A (en) * | 2018-05-15 | 2018-11-23 | 北京航空航天大学 | A kind of foldable, fast assembling-disassembling unmanned airplane empennage and the unmanned plane including the empennage |
| CN109649633A (en) * | 2018-12-31 | 2019-04-19 | 江西冠通用飞机有限公司 | A kind of fixed wing aircraft shell that wing frame eyelid retractor is easy to assembly and stable |
| CN110371286A (en) * | 2019-07-15 | 2019-10-25 | 珠海天晴航空航天科技有限公司 | A kind of manned vehicle |
| CN110466750A (en) * | 2019-08-19 | 2019-11-19 | 西北工业大学 | A kind of Portable vertical landing scouting monitoring unmanned plane |
| CN112429198A (en) * | 2020-11-27 | 2021-03-02 | 青岛航空技术研究院(中国科学院工程热物理研究所青岛研究中心) | Small unmanned aerial vehicle type V-shaped empennage sleeve plug-in multi-degree-of-freedom locking device |
| CN113386966A (en) * | 2021-07-23 | 2021-09-14 | 珠海天晴航空航天科技有限公司 | Unmanned aerial vehicle convenient to dismouting |
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| CN108657414A (en) * | 2018-05-15 | 2018-10-16 | 北京航空航天大学 | A kind of attachment device and the connection method of unmanned plane central wing, outer wing and shoe |
| CN108860570A (en) * | 2018-05-15 | 2018-11-23 | 北京航空航天大学 | A kind of foldable, fast assembling-disassembling unmanned airplane empennage and the unmanned plane including the empennage |
| CN109649633A (en) * | 2018-12-31 | 2019-04-19 | 江西冠通用飞机有限公司 | A kind of fixed wing aircraft shell that wing frame eyelid retractor is easy to assembly and stable |
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| CN110466750A (en) * | 2019-08-19 | 2019-11-19 | 西北工业大学 | A kind of Portable vertical landing scouting monitoring unmanned plane |
| CN112429198A (en) * | 2020-11-27 | 2021-03-02 | 青岛航空技术研究院(中国科学院工程热物理研究所青岛研究中心) | Small unmanned aerial vehicle type V-shaped empennage sleeve plug-in multi-degree-of-freedom locking device |
| CN113386966A (en) * | 2021-07-23 | 2021-09-14 | 珠海天晴航空航天科技有限公司 | Unmanned aerial vehicle convenient to dismouting |
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| Publication number | Publication date |
|---|---|
| CN107600414B (en) | 2024-03-15 |
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