CN106005364A - Wing insertion connecting structure - Google Patents
Wing insertion connecting structure Download PDFInfo
- Publication number
- CN106005364A CN106005364A CN201610541178.6A CN201610541178A CN106005364A CN 106005364 A CN106005364 A CN 106005364A CN 201610541178 A CN201610541178 A CN 201610541178A CN 106005364 A CN106005364 A CN 106005364A
- Authority
- CN
- China
- Prior art keywords
- wing
- positioning sleeve
- connection sheet
- sleeve
- connected structure
- 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
- B64C3/00—Wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/25—Fixed-wing aircraft
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Connection Of Plates (AREA)
Abstract
The invention discloses a wing insertion connecting structure which comprises a wing arm and an installation seat for fixing the wing arm. The installation seat is provided with a connecting sleeve, the connecting sleeve comprises at least two connecting pieces, a clearance slot is formed between every two adjacent connecting pieces, the wing arm is partially arranged on the inner side of the connecting sleeve, a positioning sleeve is arranged on the outer side of the connecting sleeve and installed on the connecting pieces through threads, and the positioning sleeve presses the connecting pieces to be closed, so that the connecting pieces closely press the wing arm. In this way, according to the wing insertion connecting structure, a wing can be quickly disassembled and assembled, connecting is easy, and the structure is firm, safe and reliable.
Description
Technical field
The present invention relates to unmanned plane field, particularly relate to a kind of wing connected structure.
Background technology
Generally unmanned plane is made up of host wing, fuselage, electromotor etc., and host wing is generally integrally formed, and bodily form length is relatively big, and wing intensity is relatively low.Therefore unmanned plane packaging, transport and collect during take big quantity space, and be easily damaged, once there is breakage in host wing, then need whole to scrap replacing, be therefore not convenient to use.
Summary of the invention
The technical problem that present invention mainly solves is to provide a kind of wing connected structure, it is possible to fast assembling-disassembling wing, connects simple, and sound construction is safe and reliable.
For solving above-mentioned technical problem, the technical scheme that the present invention uses is: provide a kind of wing connected structure, including: wing arm and for fixing the mounting seat of wing arm, described mounting seat is provided with adapter sleeve, described adapter sleeve includes that at least two connects sheet, between described connection sheet, there is clearance groove, the part of described wing arm is arranged on inside adapter sleeve, it is provided with positioning sleeve outside described adapter sleeve, described positioning sleeve is by being threadably mounted on connection sheet, and described positioning sleeve pressing connects sheet makes connection sheet compress wing arm.
In a preferred embodiment of the present invention, the external diameter of described adapter sleeve and positioning sleeve is from left to right gradually increased.
In a preferred embodiment of the present invention, the quantity of described connection sheet is 4, is uniformly arranged in interval between described connection sheet.
In a preferred embodiment of the present invention, described connection sheet having external screw thread, described positioning sleeve has female thread, described positioning sleeve is threaded on connection sheet.
In a preferred embodiment of the present invention, having multiple locating dowel bottom described wing arm, described mounting seat has multiple hole, location matched with locating dowel, the locating dowel of described wing arm is connected to inside the hole, location of mounting seat.
In a preferred embodiment of the present invention, the quantity in described locating dowel and hole, location is 5.
The invention has the beneficial effects as follows: wing connected structure of the present invention, it is possible to fast assembling-disassembling wing, connect simple, sound construction, safe and reliable.
Accompanying drawing explanation
For the technical scheme being illustrated more clearly that in the embodiment of the present invention, in describing embodiment below, the required accompanying drawing used is briefly described, apparently, accompanying drawing in describing below is only some embodiments of the present invention, for those of ordinary skill in the art, on the premise of not paying creative work, it is also possible to obtain other accompanying drawing according to these accompanying drawings, wherein:
Fig. 1 is the structural representation of wing connected structure one of the present invention preferred embodiment；
Fig. 2 is the structural representation of the wing connected structure shown in Fig. 1；
In accompanying drawing, the labelling of each parts is as follows: 1, wing arm, and 2, mounting seat, 3, adapter sleeve, 4, connect sheet, 5, clearance groove, 6, positioning sleeve, 7, locating dowel, 8, hole, location.
Detailed description of the invention
Technical scheme in the embodiment of the present invention will be clearly and completely described below, it is clear that described embodiment is only a part of embodiment of the present invention rather than whole embodiments.Based on the embodiment in the present invention, all other embodiments that those of ordinary skill in the art are obtained under not making creative work premise, broadly fall into the scope of protection of the invention.
Refer to Fig. 1, a kind of wing connected structure, including: wing arm 1 and for fixing the mounting seat 2 of wing arm 1, mounting seat 2 is provided with adapter sleeve 3, and adapter sleeve 3 includes that at least two connects sheet 4, connects and has clearance groove 5 between sheet 4, the part of wing arm 1 is arranged on inside adapter sleeve 3, being provided with positioning sleeve 6 outside adapter sleeve 3, positioning sleeve 6 is by being threadably mounted on connection sheet 4, and positioning sleeve 6 pressing connects sheet 4 makes connection sheet 4 compress wing arm 1.
It addition, the external diameter of adapter sleeve 3 and positioning sleeve 6 is from left to right gradually increased.
It addition, the quantity connecting sheet 4 is 4, connects and be uniformly arranged in interval between sheet 4.Connecting and have external screw thread on sheet 4, positioning sleeve 6 has female thread, positioning sleeve 6 is threaded on connection sheet 4.
It addition, have multiple locating dowel 7 bottom wing arm 1, mounting seat 2 having multiple hole, location 8 matched with locating dowel 7, the hole, location 8 that the locating dowel 7 of wing arm 1 is connected to mounting seat 2 is internal.The quantity in locating dowel 7 and hole 8, location is 5.
Wing connected structure specific works principle of the present invention is as follows: insert in mounting seat 2 by hole 8, the corresponding location of the locating dowel 7 on wing arm 1, then positioning sleeve 6 is threaded on adapter sleeve 3, owing to positioning sleeve 6 and adapter sleeve 3 external diameter are from left to right gradually increased, and connect and there is between sheet 4 clearance groove 5, under effect in the locking that positioning sleeve 3 rotates, connect one end meeting stress downward clamping motor arm 1 of sheet 4, to prevent motor arm 1 from coming off.
It is different from prior art, wing connected structure of the present invention, it is possible to fast assembling-disassembling wing, connects simple, sound construction, safe and reliable.
The foregoing is only embodiments of the invention; not thereby the scope of the claims of the present invention is limited; every equivalent structure utilizing description of the invention content to be made or equivalence flow process conversion; or directly or indirectly it is used in other relevant technical field, the most in like manner it is included in the scope of patent protection of the present invention.
Claims (6)
1. a wing connected structure, it is characterized in that, including: wing arm and for fixing the mounting seat of wing arm, described mounting seat is provided with adapter sleeve, and described adapter sleeve includes that at least two connects sheet, has clearance groove between described connection sheet, the part of described wing arm is arranged on inside adapter sleeve, being provided with positioning sleeve outside described adapter sleeve, described positioning sleeve is by being threadably mounted on connection sheet, and described positioning sleeve pressing connects sheet makes connection sheet compress wing arm.
Wing connected structure the most according to claim 1, it is characterised in that the external diameter of described adapter sleeve and positioning sleeve is from left to right gradually increased.
Wing connected structure the most according to claim 2, it is characterised in that the quantity of described connection sheet is 4, is uniformly arranged in interval between described connection sheet.
Wing connected structure the most according to claim 3, it is characterised in that have external screw thread on described connection sheet, described positioning sleeve has female thread, and described positioning sleeve is threaded on connection sheet.
5. according to the arbitrary described wing connected structure of claim 1-4, it is characterized in that, having multiple locating dowel bottom described wing arm, described mounting seat has multiple hole, location matched with locating dowel, the locating dowel of described wing arm is connected to inside the hole, location of mounting seat.
Wing connected structure the most according to claim 5, it is characterised in that the quantity in described locating dowel and hole, location is 5.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610541178.6A CN106005364A (en) | 2016-07-12 | 2016-07-12 | Wing insertion connecting structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610541178.6A CN106005364A (en) | 2016-07-12 | 2016-07-12 | Wing insertion connecting structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106005364A true CN106005364A (en) | 2016-10-12 |
Family
ID=57109237
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610541178.6A Pending CN106005364A (en) | 2016-07-12 | 2016-07-12 | Wing insertion connecting structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106005364A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109894300A (en) * | 2019-04-22 | 2019-06-18 | 河南流量新材料有限公司 | A kind of paint spraying platform of propeller production |
| CN112027075A (en) * | 2020-09-15 | 2020-12-04 | 惠州众合航空科技有限公司 | Vertical lifting wing for unmanned aerial vehicle |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN86204262U (en) * | 1986-06-19 | 1987-05-27 | 山西省纺织科学研究所 | Combined screw-driver with double workhead rod |
| CN104260879A (en) * | 2014-10-16 | 2015-01-07 | 深圳市科卫泰实业发展有限公司 | High-reliability high-stability multi-rotor-wing unmanned aerial vehicle with quick-dismounting function |
| CN204341415U (en) * | 2014-12-04 | 2015-05-20 | 北方天途航空技术发展（北京）有限公司 | Quick demounting many rotor wing unmanned aerial vehicles horn joint sleeve assembly |
| CN204368420U (en) * | 2014-12-25 | 2015-06-03 | 武汉智能鸟无人机有限公司 | A kind of rotor wing unmanned aerial vehicle of detachable horn |
| CN205891214U (en) * | 2016-07-12 | 2017-01-18 | 无锡觅睿恪科技有限公司 | Wing grafting structure |
-
2016
- 2016-07-12 CN CN201610541178.6A patent/CN106005364A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN86204262U (en) * | 1986-06-19 | 1987-05-27 | 山西省纺织科学研究所 | Combined screw-driver with double workhead rod |
| CN104260879A (en) * | 2014-10-16 | 2015-01-07 | 深圳市科卫泰实业发展有限公司 | High-reliability high-stability multi-rotor-wing unmanned aerial vehicle with quick-dismounting function |
| CN204341415U (en) * | 2014-12-04 | 2015-05-20 | 北方天途航空技术发展（北京）有限公司 | Quick demounting many rotor wing unmanned aerial vehicles horn joint sleeve assembly |
| CN204368420U (en) * | 2014-12-25 | 2015-06-03 | 武汉智能鸟无人机有限公司 | A kind of rotor wing unmanned aerial vehicle of detachable horn |
| CN205891214U (en) * | 2016-07-12 | 2017-01-18 | 无锡觅睿恪科技有限公司 | Wing grafting structure |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109894300A (en) * | 2019-04-22 | 2019-06-18 | 河南流量新材料有限公司 | A kind of paint spraying platform of propeller production |
| CN112027075A (en) * | 2020-09-15 | 2020-12-04 | 惠州众合航空科技有限公司 | Vertical lifting wing for unmanned aerial vehicle |
| CN112027075B (en) * | 2020-09-15 | 2022-04-29 | 惠州众合航空科技有限公司 | Vertical lifting wing for 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 |
Application publication date: 20161012 |
|
| RJ01 | Rejection of invention patent application after publication |