CN106240792A - A kind of unmanned plane wing fast folding development mechanism - Google Patents
A kind of unmanned plane wing fast folding development mechanism Download PDFInfo
- Publication number
- CN106240792A CN106240792A CN201610652451.2A CN201610652451A CN106240792A CN 106240792 A CN106240792 A CN 106240792A CN 201610652451 A CN201610652451 A CN 201610652451A CN 106240792 A CN106240792 A CN 106240792A
- Authority
- CN
- China
- Prior art keywords
- horn
- mounting seat
- sliding sleeve
- unmanned plane
- development mechanism
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 210000003284 Horns Anatomy 0.000 claims abstract description 47
- 230000001105 regulatory Effects 0.000 abstract 1
- 238000000034 method Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006011 modification reaction Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
- B64C1/30—Parts of fuselage relatively movable to reduce overall size for storage
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- B64U10/25—
-
- B64U2101/00—
Abstract
The present invention relates to a kind of unmanned plane wing fast folding development mechanism, including horn and horn mounting seat；Horn mounting seat upper surface is provided with guide pillar, and guide pillar outer surface is arranged with sliding sleeve, and sliding sleeve side is provided with hole, location；Multiple screw coordinated with hole, location it is provided with on guide pillar；Also include the screw coordinated with screw；Also including connecting sliding sleeve and the linking arm of horn, linking arm is connected with horn surface pivots；Horn end is rotationally connected with horn mounting seat；When needing to fold or launch, regulating sliding sleeve, and carry out positioning sliding sleeve by hole, location and screw, drive horn to rotate by linking arm, structural stability is strong and easy to operate；Overall structure is simple, low cost.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, more particularly, it relates to a kind of unmanned plane wing fast folding unwinder
Structure.
Background technology
Unmanned plane is the most manned aircraft of the presetting apparatus manipulation utilizing radio robot with providing for oneself, civilian nothing
Man-machine taking photo by plane, agricultural, plant protection, the field such as the disaster relief have more important application；Currently used unmanned plane wing-folding packs up knot
Structure is complex, the most more inconvenience when folding and launch.
Summary of the invention
The technical problem to be solved in the present invention is, for the drawbacks described above of prior art, it is provided that a kind of energy fast folding
Launch the unmanned plane wing fast folding development mechanism of horn.
The technical solution adopted for the present invention to solve the technical problems is:
A kind of unmanned plane wing fast folding development mechanism of structure, including horn and horn mounting seat；Wherein, described horn
Mounting seat upper surface is provided with guide pillar, and described guide pillar outer surface is arranged with sliding sleeve, and described sliding sleeve side is provided with fixed
Hole, position；The screw that multiple and hole, described location coordinates it is provided with on described guide pillar；Also include the screw coordinated with described screw；Also
Including connecting described sliding sleeve and the linking arm of described horn, described linking arm is connected with described horn surface pivots；Described
Horn end is rotationally connected with described horn mounting seat.
Unmanned plane wing fast folding development mechanism of the present invention, wherein, described horn mounting seat is provided with and institute
Stating the opening that horn coordinates, described opening is positioned in described horn mounting seat in fan column type and covering of the fan.
Unmanned plane wing fast folding development mechanism of the present invention, wherein, also includes and described guide pillar and described machine
The boss that arm mounting seat is fixedly connected with.
Unmanned plane wing fast folding development mechanism of the present invention, wherein, described boss is sleeve-shaped and bottom
Mate with described horn mounting seat surface configuration.
The beneficial effects of the present invention is: when needing to fold or launch, regulate sliding sleeve, and by hole, location and screw
Carrying out positioning sliding sleeve, drive horn to rotate by linking arm, structural stability is strong and easy to operate；Overall structure
Simply, low cost.
Accompanying drawing explanation
In order to be illustrated more clearly that the embodiment of the present invention or technical scheme of the prior art, below in conjunction with accompanying drawing and reality
The invention will be further described to execute example, and the accompanying drawing in describing below is only the section Example of the present invention, for this area
From the point of view of those of ordinary skill, on the premise of not paying creative work, it is also possible to obtain other accompanying drawings according to these accompanying drawings:
Fig. 1 is the unmanned plane wing fast folding development mechanism structural representation of present pre-ferred embodiments.
Detailed description of the invention
In order to make the purpose of the embodiment of the present invention, technical scheme and advantage clearer, implement below in conjunction with the present invention
Technical scheme in example carries out clear, complete description, it is clear that described embodiment is the section Example of the present invention, and
It is not all of embodiment.Based on embodiments of the invention, those of ordinary skill in the art are not before paying creative work
Put the every other embodiment obtained, broadly fall into protection scope of the present invention.
The unmanned plane wing fast folding development mechanism of present pre-ferred embodiments is as it is shown in figure 1, include horn 1 and horn
Mounting seat 2；Horn mounting seat 2 upper surface is provided with guide pillar 20, and guide pillar 20 outer surface is arranged with sliding sleeve 21, sliding sleeve 21
Side is provided with hole 210, location；Multiple screw 200 coordinated with hole 210, location it is provided with on guide pillar 20；Also include and screw
The 200 screw (not shown) coordinated；Also include connecting sliding sleeve 21 and the linking arm 3 of horn 1, linking arm 3 and horn 1
Surface pivots connects；Horn 1 end is rotationally connected with horn mounting seat 2；When needing to fold or launch, regulate sliding sleeve 21,
And carry out sliding sleeve 21 is positioned by hole 210, location and screw (not shown), drive horn 1 turn by linking arm 3
Dynamic, structural stability is strong and easy to operate；Overall structure is simple, low cost.
As it is shown in figure 1, horn mounting seat 2 is provided with the opening 22 coordinated with horn 1, opening 22 is in fan column type and covering of the fan position
In horn mounting seat 2, transfer highly reliable and effectively prevent horn from shifting.
As it is shown in figure 1, also include the boss 23 being fixedly connected with guide pillar 20 and horn mounting seat 2, strengthen fixing company
Connect, it is ensured that stability.
As it is shown in figure 1, boss 23 in sleeve-shaped and bottom is mated with horn mounting seat 2 surface configuration, connective stability
By force, it is simple to welding.
It should be appreciated that for those of ordinary skills, can be improved according to the above description or be converted,
And all these modifications and variations all should belong to the protection domain of claims of the present invention.
Claims (4)
1. a unmanned plane wing fast folding development mechanism, including horn and horn mounting seat；It is characterized in that, described horn
Mounting seat upper surface is provided with guide pillar, and described guide pillar outer surface is arranged with sliding sleeve, and described sliding sleeve side is provided with fixed
Hole, position；The screw that multiple and hole, described location coordinates it is provided with on described guide pillar；Also include the screw coordinated with described screw；Also
Including connecting described sliding sleeve and the linking arm of described horn, described linking arm is connected with described horn surface pivots；Described
Horn end is rotationally connected with described horn mounting seat.
Unmanned plane wing fast folding development mechanism the most according to claim 1, it is characterised in that described horn mounting seat
Being provided with the opening coordinated with described horn, described opening is positioned in described horn mounting seat in fan column type and covering of the fan.
Unmanned plane wing fast folding development mechanism the most according to claim 1, it is characterised in that also include leading with described
The boss that post and described horn mounting seat are fixedly connected with.
Unmanned plane wing fast folding development mechanism the most according to claim 3, it is characterised in that described boss is set
Tubular and bottom are mated with described horn mounting seat surface configuration.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610652451.2A CN106240792A (en) | 2016-08-10 | 2016-08-10 | A kind of unmanned plane wing fast folding development mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610652451.2A CN106240792A (en) | 2016-08-10 | 2016-08-10 | A kind of unmanned plane wing fast folding development mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106240792A true CN106240792A (en) | 2016-12-21 |
Family
ID=58079184
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610652451.2A Pending CN106240792A (en) | 2016-08-10 | 2016-08-10 | A kind of unmanned plane wing fast folding development mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106240792A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018027684A1 (en) * | 2016-08-10 | 2018-02-15 | 张琬彬 | Mechanism for quickly folding and unfolding wings of unmanned aerial vehicle |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204701387U (en) * | 2015-06-19 | 2015-10-14 | 新乡学院 | Paint from life and use drawing board in a kind of open air of dismountable foldable |
| EP2233393B1 (en) * | 2009-03-23 | 2016-01-06 | Gregor Schnoell | Locking system |
| CN205194282U (en) * | 2015-11-09 | 2016-04-27 | 石家庄铁道大学 | Multifunctional advertising board |
| CN105539827A (en) * | 2016-01-26 | 2016-05-04 | 南京航空航天大学 | Arm folding device of multi-axial air vehicle |
-
2016
- 2016-08-10 CN CN201610652451.2A patent/CN106240792A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2233393B1 (en) * | 2009-03-23 | 2016-01-06 | Gregor Schnoell | Locking system |
| CN204701387U (en) * | 2015-06-19 | 2015-10-14 | 新乡学院 | Paint from life and use drawing board in a kind of open air of dismountable foldable |
| CN205194282U (en) * | 2015-11-09 | 2016-04-27 | 石家庄铁道大学 | Multifunctional advertising board |
| CN105539827A (en) * | 2016-01-26 | 2016-05-04 | 南京航空航天大学 | Arm folding device of multi-axial air vehicle |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018027684A1 (en) * | 2016-08-10 | 2018-02-15 | 张琬彬 | Mechanism for quickly folding and unfolding wings of unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20161221 |