CN106081053A - A kind of SUAV folded wing - Google Patents
A kind of SUAV folded wing Download PDFInfo
- Publication number
- CN106081053A CN106081053A CN201610657636.2A CN201610657636A CN106081053A CN 106081053 A CN106081053 A CN 106081053A CN 201610657636 A CN201610657636 A CN 201610657636A CN 106081053 A CN106081053 A CN 106081053A
- Authority
- CN
- China
- Prior art keywords
- horn
- mounting seat
- hole
- retainer ring
- suav
- 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
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/061—Frames
- B64C1/063—Folding or collapsing to reduce overall dimensions, e.g. foldable tail booms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Catching Or Destruction (AREA)
Abstract
The present invention relates to a kind of SUAV folded wing, including horn and horn mounting seat, horn mounting seat end is provided with the blind hole coordinated with horn；Both sides, horn mounting seat end sidewall is provided with the first through hole connected with blind hole, and upper surface is provided with opening；Horn end is provided with the second through hole coordinated with the first through hole；Also include running through the first through hole and the pin of the second through hole；Horn mounting seat end outer surface is arranged with retainer ring, and retainer ring inwall is provided with female thread；Horn mounting seat end outer surface is provided with the external screw thread with screw-internal thread fit；When needing to launch, being rotated by horn and put down, horn is fixed by then turn retainer ring to be sheltered port part, and stability by force and simple in construction, operates very convenient；When needing to pack up, turn retainer ring opens opening, can rotate horn and pack up；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 SUAV folded wing.
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 folding and expanding side
Just SUAV folded wing.
The technical solution adopted for the present invention to solve the technical problems is:
A kind of SUAV folded wing of structure, including horn and horn mounting seat；Wherein, described horn mounting seat end
Portion is provided with the blind hole coordinated with described horn；Both sides, described horn mounting seat end sidewall is provided with and connects with described blind hole
The first through hole, and upper surface is provided with opening；Described horn end is provided with the second through hole coordinated with described first through hole；
Also include running through described first through hole and the pin of described second through hole；Described horn mounting seat end outer surface is arranged with fixing
Ring, described retainer ring inwall is provided with female thread；Described horn mounting seat end outer surface is provided with and described screw-internal thread fit
External screw thread.
SUAV folded wing of the present invention, wherein, described horn end and described blind hole bottom surface are arc
Face is arranged.
SUAV folded wing of the present invention, wherein, described horn mounting seat is fixedly installed promising described
The spacing ring that retainer ring is spacing.
SUAV folded wing of the present invention, wherein, described horn mounting seat end end face edge is provided with
For the chimb that described retainer ring is spacing.
SUAV folded wing of the present invention, wherein, described horn mounting seat end end face external diameter is more than institute
State retainer ring internal diameter.
The beneficial effects of the present invention is: when needing to launch, rotated by horn and put down, then turn retainer ring is to be sheltered
Horn is fixed by port part, and stability is strong and simple in construction, operates very convenient；When needing to pack up, turn is fixed
Ring opens opening, can rotate horn and pack up；Overall structure is simple, low cost, and overall weight is lighter.
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 SUAV folded wing structural blast figure 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 SUAV folded wing of present pre-ferred embodiments as it is shown in figure 1, include horn 1 and horn mounting seat 2,
Horn mounting seat 2 end is provided with the blind hole 20 coordinated with horn 1；Both sides, horn mounting seat 2 end sidewall is provided with blind
First through hole 21 of hole 20 connection, and upper surface is provided with opening 22；Horn 1 end is provided with coordinated with the first through hole 21
Two through holes 10；Also include running through the first through hole 21 and pin (not shown) of the second through hole 10；Outside horn mounting seat 2 end
Surface is arranged with retainer ring 23, and retainer ring 23 inwall is provided with female thread (not shown)；Horn mounting seat 2 end outer surface
It is provided with the external screw thread (not shown) coordinated with female thread (not shown)；When needing to launch, horn 1 is rotated and puts
Under, horn 1 is fixed by then turn retainer ring 23 to cover opening 22 position, and stability is strong and simple in construction, behaviour
Make very convenient；When needing to pack up, turn retainer ring 23 opens opening 22 position, can rotate horn 1 and pack up；Overall knot
Structure is simple, low cost.
Arranging as it is shown in figure 1, horn 1 end and blind hole 20 bottom surface are cambered surface, during rotation, contact friction is less, and minimizing sets
Standby loss, and be easy to launch and draw in, moreover it is possible to play positioning action.
As it is shown in figure 1, be fixedly installed the spacing ring 25 that promising retainer ring 23 is spacing in horn mounting seat 2, prevent wing from receiving
When holding together, retainer ring 23 moves in horn mounting seat 2.
As it is shown in figure 1, horn mounting seat 2 end end face edge arranges the chimb 26 that promising retainer ring 23 is spacing, prevent machine
When the span is opened, retainer ring 23 transition screws, and causes dismounting inconvenience and equipment damage.
As it is shown in figure 1, horn mounting seat 2 end end face external diameter is more than retainer ring internal diameter, it is simple to retainer ring 23 screws.
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 (5)
1. a SUAV folded wing, including horn and horn mounting seat；It is characterized in that, described horn mounting seat end
Portion is provided with the blind hole coordinated with described horn；Both sides, described horn mounting seat end sidewall is provided with and connects with described blind hole
The first through hole, and upper surface is provided with opening；Described horn end is provided with the second through hole coordinated with described first through hole；
Also include running through described first through hole and the pin of described second through hole；Described horn mounting seat end outer surface is arranged with fixing
Ring, described retainer ring inwall is provided with female thread；Described horn mounting seat end outer surface is provided with and described screw-internal thread fit
External screw thread.
SUAV folded wing the most according to claim 1, it is characterised in that described horn end and described blind hole
Bottom surface is cambered surface and arranges.
SUAV folded wing the most according to claim 1, it is characterised in that fix in described horn mounting seat and set
It is equipped with as the spacing spacing ring of described retainer ring.
SUAV folded wing the most according to claim 1, it is characterised in that described horn mounting seat end end face
Edge arranges the chimb that promising described retainer ring is spacing.
SUAV folded wing the most according to claim 1, it is characterised in that described horn mounting seat end end face
External diameter is more than described retainer ring internal diameter.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610657636.2A CN106081053A (en) | 2016-08-10 | 2016-08-10 | A kind of SUAV folded wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610657636.2A CN106081053A (en) | 2016-08-10 | 2016-08-10 | A kind of SUAV folded wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106081053A true CN106081053A (en) | 2016-11-09 |
Family
ID=57455623
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610657636.2A Pending CN106081053A (en) | 2016-08-10 | 2016-08-10 | A kind of SUAV folded wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106081053A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018027681A1 (en) * | 2016-08-10 | 2018-02-15 | 张琬彬 | Foldable wing of small unmanned aerial vehicle |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2909972A1 (en) * | 2006-12-18 | 2008-06-20 | Novadem Sarl | Vertical take-off and land aircraft for military application, has blocking unit selecting blocking configuration of arms in deployed position and releasing configuration of arms for authorizing arms to pass through folding position of arms |
| CN204713418U (en) * | 2015-04-30 | 2015-10-21 | 深圳一电科技有限公司 | Collapsible paddle arm assembly and unmanned plane |
| CN204713419U (en) * | 2015-04-30 | 2015-10-21 | 深圳一电科技有限公司 | Collapsible paddle arm assembly and unmanned plane |
| CN204802065U (en) * | 2015-04-30 | 2015-11-25 | 深圳一电科技有限公司 | Collapsible oar arm component and unmanned aerial vehicle |
| EP2233393B1 (en) * | 2009-03-23 | 2016-01-06 | Gregor Schnoell | Locking system |
-
2016
- 2016-08-10 CN CN201610657636.2A patent/CN106081053A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2909972A1 (en) * | 2006-12-18 | 2008-06-20 | Novadem Sarl | Vertical take-off and land aircraft for military application, has blocking unit selecting blocking configuration of arms in deployed position and releasing configuration of arms for authorizing arms to pass through folding position of arms |
| EP2233393B1 (en) * | 2009-03-23 | 2016-01-06 | Gregor Schnoell | Locking system |
| CN204713418U (en) * | 2015-04-30 | 2015-10-21 | 深圳一电科技有限公司 | Collapsible paddle arm assembly and unmanned plane |
| CN204713419U (en) * | 2015-04-30 | 2015-10-21 | 深圳一电科技有限公司 | Collapsible paddle arm assembly and unmanned plane |
| CN204802065U (en) * | 2015-04-30 | 2015-11-25 | 深圳一电科技有限公司 | Collapsible oar arm component and unmanned aerial vehicle |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018027681A1 (en) * | 2016-08-10 | 2018-02-15 | 张琬彬 | Foldable wing of small 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: 20161109 |