CN206511106U - A kind of VTOL composite wing Vertical Dynamic device for quickly disassembling - Google Patents
A kind of VTOL composite wing Vertical Dynamic device for quickly disassembling Download PDFInfo
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- CN206511106U CN206511106U CN201720165667.6U CN201720165667U CN206511106U CN 206511106 U CN206511106 U CN 206511106U CN 201720165667 U CN201720165667 U CN 201720165667U CN 206511106 U CN206511106 U CN 206511106U
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- pipe clamp
- fixture block
- wing
- main body
- travelling pipe
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Abstract
The utility model provides a kind of VTOL composite wing Vertical Dynamic device for quickly disassembling, it is characterised in that：Including wing, wing fixed block is installed with below wing；With travelling pipe clamp, the pipe clamp that moves about includes travelling pipe clamp main body, upper fixture block, lower fixture block；The bolt of a piece transverse direction through the top of upper fixture block and travelling pipe clamp main body and be connected upper fixture block and travelling pipe clamp main body, upper fixture block and travelling pipe clamp main body respectively the both sides of contact wing fixed block and wing fixed block is securely folded between fixture block and travelling pipe clamp main body；Travelling pipe clamp main body lower end is connected with lower fixture block, rotor connecting rod pass through and be fixed on the cambered surface of travelling pipe clamp main body lower end and circle that the cambered surface of lower fixture block upper end is surrounded in.The utility model makes the attachment structure between connecting rod and fixed-wing between the rotor and rotor drive mechanism of composite wing unmanned plane can be with fast assembling-disassembling.
Description
Technical field
The utility model belongs to a kind of unmanned plane structure, more particularly to a kind of mounting structure of unmanned plane wing.
Background technology
At present, unmanned plane is mainly two kinds of forms of rotor wing unmanned aerial vehicle and fixed-wing unmanned plane, and rotor wing unmanned aerial vehicle is similar to go straight up to
Machine, using rotor parallel to the ground or almost parallel as flying power, be able to can be hovered with VTOL, motor-driven during flight
Flexibly, but cruise when its speed and voyage be restricted, fixed-wing unmanned plane cruise when obtain at high speed and high voyage,
But it is clear that VTOL or can not hover in the air.
Composite wing is an innovation vehicle technology, combines the VTOL ability and fixed wing aircraft of rotor craft
Efficiency, speed and voyage advantage.The compound rotor aircraft with fixed-wing rotor passes through comprehensive fixed wing aircraft and four
Rotor craft obtains the VTOL performance advantage of uniqueness, while keeping the flight of fixed wing aircraft platform to large extent
Performance, particularly duration performance and speed ability.Composite wing aircraft has longer than helicopter and multi-rotor aerocraft continue
ETS estimated time of sailing, and landing flying field is more much smaller than fixed wing aircraft.It enables fixed wing aircraft to be used in minimum place.
The way of realization of current composite wing unmanned plane is mainly, and the fixed-wing of fuselage and both sides is connected as a single entity, solid at two
Determine to be respectively mounted rotor connecting rod in the middle part of the wing, rotor and rotor drive mechanism are installed in the two ends of rotor connecting rod.
But, because the two ends of rotor connecting rod have rotor and rotor drive mechanism, and rotor connecting rod is to install
In the middle part of fixed-wing, cause the connection of rotor connecting rod and fixed-wing pretty troublesome, cylinder block strength may be influenceed, if fixed
Non-dismountable to install, whole unmanned plane just occupies volume very much, and transports very inconvenient.
Utility model content
The utility model provides a kind of VTOL composite wing Vertical Dynamic device for quickly disassembling, and the purpose is to solve prior art
The shortcoming of presence, makes the connection knot between the connecting rod and fixed-wing between the rotor and rotor drive mechanism of composite wing unmanned plane
Structure can be with fast assembling-disassembling.
The utility model solves the technical scheme that its technical problem used：
A kind of VTOL composite wing Vertical Dynamic device for quickly disassembling, it is characterised in that：Including wing, it is installed with below wing
Wing fixed block；With travelling pipe clamp, the pipe clamp that moves about includes travelling pipe clamp main body, upper fixture block, lower fixture block；The bolt of a piece transverse direction
Fixture block and travelling pipe clamp main body, upper fixture block and travelling pipe clamp main body on being connected through the top of upper fixture block and travelling pipe clamp main body
Respectively the both sides of contact wing fixed block and wing fixed block is securely folded between fixture block and travelling pipe clamp main body；Trip
Dynamic pipe clamp main body lower end is connected with lower fixture block, and rotor connecting rod passes through and is fixed on the cambered surface and lower card of travelling pipe clamp main body lower end
In the circle that the cambered surface of block upper end is surrounded.
The both sides of wing fixed block have an inclined-plane upward, the inclined-planes upward of both sides respectively with upper fixture block
Inclined-plane downward and the inclined-plane phase contact downward of travelling pipe clamp main body.
Wing fixed block is coattail board form, namely the both sides of wing fixed block have triangular hill outwardly respectively,
The triangular hill of wing fixed block both sides insert respectively fixture block triangular groove and travelling pipe clamp main body triangle it is recessed
In groove.
Down, the two ends of cambered surface have the mounting blocks extended towards both sides to the cambered surface of travelling pipe clamp main body lower end；Lower fixture block
Upward, the two ends of cambered surface have the mounting blocks extended towards both sides to the cambered surface of upper end；Unit bolt nut is each passed through corresponding
Travelling pipe clamp main body and lower fixture block are connected after the mounting blocks of travelling pipe clamp main body and the mounting blocks of lower fixture block, rotor connecting rod is passed through
And be fixed in the circle that the cambered surface of the cambered surface of travelling pipe clamp main body lower end and lower fixture block upper end is surrounded.
It is of the present utility model to be beneficial in that：
The utility model has entered the installation operation of composite wing Vertical Dynamic device, employs dovetail groove fit structure and is divided into
The travelling pipe clamp of three parts, makes installation enhanced convenience simple, on the basis of power set and wing self-strength are met, real
The purpose of existing fast assembling-disassembling, saves the working time, improves operating efficiency.
Brief description of the drawings
The utility model is further illustrated with reference to the accompanying drawings and examples.
Fig. 1 is the utility model structure chart.
Embodiment
In order to illustrate more clearly of the technical solution of the utility model, the required accompanying drawing used in description will be made below
Simply introduce, it should be apparent that, drawings in the following description are only some embodiments of the present utility model, for this area
For those of ordinary skill, on the premise of not paying creative work, other implement can also be obtained according to these accompanying drawings
Example.
As shown in Figure 1：
The utility model connects the rotor between corresponding two rotors and rotor drive mechanism of composite wing unmanned plane
Bar is connected to the device below fixed-wing.
Fig. 1 show the fixation wing 1 of composite wing unmanned plane side, and the structure that opposite side fixes wing is identical.
(namely the both sides of wing fixed block 2 have triangle outwardly to the wing fixed block 2 of one coattail board form respectively
Projection 21,22, so-called triangle refers to vertical section for triangle) pass through connector in the lower surface of wing 1 and fixed with wing 1 and connect
Connect.
Travelling pipe clamp 3 includes travelling pipe clamp main body 31, upper fixture block 32, lower fixture block 33.
During installation, the triangular groove 321 of upper fixture block 32 is pressed on the triangular hill 21 in the left side of wing fixed block 2,
The triangular groove of the upper end of travelling pipe clamp main body 31 is pressed on the triangular hill 22 on the right side of wing fixed block 2 (in figure not
The triangular groove of the upper end of the travelling pipe clamp main body 31 of display, its structure and the triangular groove 321 of upper fixture block 32 are identical
), then by the bolt 4 of a transverse direction through upper fixture block 32 through hole after, set by the top for being screwed into travelling pipe clamp main body 31
In screw, bolt 4 is screwed tight, so upper fixture block 32 is just fixedly connected with travelling pipe clamp main body 31, and difference tightly contact wing
The both sides of fixed block 2 and wing fixed block 2 is clipped in the middle, due to the respective outer side edges of triangular hill and triangular groove, institute
Above fixture block 32 and travelling pipe clamp main body 31 are not only to clamp wing fixed block 2, and are hung on wing fixed block 2, from
And two rotors and the weight of rotor drive mechanism at rotor connecting rod 6 and its two ends can be undertaken.
Then by rotor connecting rod 6, (current material is carbon fiber pipe, and two ends can first set up rotor and rotor driving machine
Structure, can also install on wing 1 and install rotor and rotor drive mechanism after rotor connecting rod 6 again) it is inserted in travelling pipe clamp master
In the cambered surface directed downwardly of the lower end of body 31, the cambered surface upward of the lower upper end of fixture block 33 is arranged on below rotor connecting rod 6, and both sides are respectively used
Two groups of bolts 5, which are passed through, connects travelling pipe clamp main body after the mounting blocks of corresponding travelling pipe clamp main body 31 and the mounting blocks of lower fixture block 33
31 and lower fixture block 33 (two mounting blocks that the bolt 5 of side is shown in figure and its is passed through, another side structure is identical).Such rotor
Connecting rod 6 pass through and be fixed on the cambered surface of the travelling lower end of pipe clamp main body 31 and circle that the cambered surface of the lower upper end of fixture block 33 is surrounded in.
After operating above, the rotor and rotor drive mechanism at rotor connecting rod 6 and its two ends are just fixedly connected on fixed-wing 1
Lower section.
That is, disassembly process only needs to turn round several bolts, it is very easy to be quick and very firm after installation.
The embodiment of each in this specification is described by the way of progressive, and what each embodiment was stressed is and other
Between the difference of embodiment, each embodiment identical similar portion mutually referring to.To the upper of the disclosed embodiments
State bright, professional and technical personnel in the field is realized or use the utility model.A variety of modifications pair to these embodiments
It will be apparent for those skilled in the art, generic principles defined herein can not depart from this reality
In the case of with new spirit or scope, realize in other embodiments.Therefore, the utility model is not intended to be limited to this
These embodiments shown in text, and it is to fit to the most wide scope consistent with features of novelty with principles disclosed herein.
Claims (4)
1. a kind of VTOL composite wing Vertical Dynamic device for quickly disassembling, it is characterised in that：Including wing, wing lower section is fixed organic
Wing fixed block；With travelling pipe clamp, the pipe clamp that moves about includes travelling pipe clamp main body, upper fixture block, lower fixture block；The bolt of a piece transverse direction is worn
Cross the top of fixture block and travelling pipe clamp main body and be connected and go up fixture block and travelling pipe clamp main body, upper fixture block and travelling pipe clamp main body point
The both sides of other contact wing fixed block and wing fixed block is securely folded between fixture block and travelling pipe clamp main body；It is travelling
Pipe clamp main body lower end is connected with lower fixture block, and rotor connecting rod passes through and is fixed on the cambered surface and lower fixture block of travelling pipe clamp main body lower end
In the circle that the cambered surface of upper end is surrounded.
2. a kind of VTOL composite wing Vertical Dynamic device for quickly disassembling as claimed in claim 1, it is characterised in that：Wing is fixed
The both sides of block have an inclined-plane upward, the inclined-planes upward of both sides respectively with the inclined-plane downward of upper fixture block and
The inclined-plane phase contact downward of travelling pipe clamp main body.
3. a kind of VTOL composite wing Vertical Dynamic device for quickly disassembling as claimed in claim 2, it is characterised in that：Wing is fixed
Block is coattail board form, namely the both sides of wing fixed block have triangular hill outwardly respectively, wing fixed block both sides
Triangular hill is inserted in the triangular groove of fixture block and the triangular groove of travelling pipe clamp main body respectively.
4. a kind of VTOL composite wing Vertical Dynamic device for quickly disassembling as claimed in claim 1, it is characterised in that：Travelling pipe clamp
Down, the two ends of cambered surface have the mounting blocks extended towards both sides to the cambered surface of main body lower end；The cambered surface of lower fixture block upper end upward, arc
The two ends in face have the mounting blocks extended towards both sides；Unit bolt nut is each passed through the installation of corresponding travelling pipe clamp main body
Travelling pipe clamp main body and lower fixture block are connected after the mounting blocks of block and lower fixture block, rotor connecting rod passes through and is fixed on travelling pipe clamp master
In the circle that the cambered surface of body lower end and the cambered surface of lower fixture block upper end are surrounded.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720165667.6U CN206511106U (en) | 2017-02-23 | 2017-02-23 | A kind of VTOL composite wing Vertical Dynamic device for quickly disassembling |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720165667.6U CN206511106U (en) | 2017-02-23 | 2017-02-23 | A kind of VTOL composite wing Vertical Dynamic device for quickly disassembling |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206511106U true CN206511106U (en) | 2017-09-22 |
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ID=59867967
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720165667.6U Active CN206511106U (en) | 2017-02-23 | 2017-02-23 | A kind of VTOL composite wing Vertical Dynamic device for quickly disassembling |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206511106U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108725775A (en) * | 2018-07-20 | 2018-11-02 | 平湖市职业中学 | A kind of VTOL fixed-wing unmanned plane |
| CN110015401A (en) * | 2017-12-13 | 2019-07-16 | 空中客车营运有限公司 | Part external member, airfoil structure and the method for assembling airfoil structure |
-
2017
- 2017-02-23 CN CN201720165667.6U patent/CN206511106U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110015401A (en) * | 2017-12-13 | 2019-07-16 | 空中客车营运有限公司 | Part external member, airfoil structure and the method for assembling airfoil structure |
| CN108725775A (en) * | 2018-07-20 | 2018-11-02 | 平湖市职业中学 | A kind of VTOL fixed-wing unmanned plane |
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