CN107972844A - A kind of folded wing - Google Patents
A kind of folded wing Download PDFInfo
- Publication number
- CN107972844A CN107972844A CN201711299674.6A CN201711299674A CN107972844A CN 107972844 A CN107972844 A CN 107972844A CN 201711299674 A CN201711299674 A CN 201711299674A CN 107972844 A CN107972844 A CN 107972844A
- Authority
- CN
- China
- Prior art keywords
- rib
- wing
- telescopic rod
- folded
- connector
- 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.)
- Withdrawn
Links
- 101100334009 Caenorhabditis elegans rib-2 gene Proteins 0.000 description 9
- 238000010586 diagram Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/54—Varying in area
- B64C3/546—Varying in area by foldable elements
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Catching Or Destruction (AREA)
- Tents Or Canopies (AREA)
Abstract
A kind of folded wing, belongs to aircraft technology field, including telescopic rod, folding rib, flexible covering, draw off gear and connector.Connector is used to be attached with airframe；Folding on rib has the small rib of polylith, and the every piece small mutual upper end of rib is connected with upper end, and lower end is connected with lower end, and rib is entirely folded after expansion and seems undulate；Aperture is equipped with small rib, rib is folded and is serially connected in by aperture on telescopic rod；Draw off gear is fixed on connector；When controlling telescopic rod elongation, under the drive of telescopic rod, rib expansion is folded, while the flexible covering in rolled condition can also be unfolded and wrap the folding rib after expansion by draw off gear；A kind of folded wing of the present invention, it is simple in structure, wingspan length can be changed, the shape of the cross section of wing changes so that the aspect ratio of wing changes, so that obtaining different lift using the aircraft of the wing.
Description
Technical field
A kind of folded wing, belongs to aircraft technology field, more particularly to a kind of wing.
Background technology
Wing be aircraft awing can configuration again critical piece.Awing purposefully change wing shape
The efficiency of wing can effectively be increased.
The content of the invention
The object of the present invention is to provide a kind of wing that can change wing area.
A kind of folded wing, including telescopic rod, folding rib, flexible covering, draw off gear and connector.Telescopic rod is described
The supporting member of wing, can carry out stretching motion；Connector is used to be attached with airframe；Folding on rib has the polylith small
Rib, the every piece small mutual upper end of rib are connected with upper end, and lower end is connected with lower end, and rib is entirely folded after expansion and is seen
Get up undulate；Aperture is equipped with these small ribs, rib is folded and is serially connected in by aperture on telescopic rod；Telescopic rod
Head end be connected on connector, end be connected to fold rib the small rib of last block on；Fold first piece of winglet of rib
Rib is mutually fixedly connected on connector；Flexible covering is divided into two parts, and a part, which is wrapped in, to be folded on rib, another part retracting
In draw off gear；Draw off gear is fixed on connector, and draw off gear can be furled and be unfolded to flexible covering；Work as control
When telescopic rod extends, under the drive of telescopic rod, folding rib is also unfolded, while draw off gear can will also be in rolled condition
Flexible covering be unfolded and wrap expansion after folding rib；The length of wing is seen on the whole, wing length is different,
The cross-sectional area of wing is also different so that the aspect ratio using the aircraft of the wing is also different, so that what wing obtained
Lift is different.
The quantity of telescopic rod can also use two or three or four.
Winglet is equipped with wing tip position, easy to reduce the appearance of tip vortex, improves the efficiency of wing.
A kind of folded wing of the present invention, it is simple in structure, wingspan length can be changed, the shape of the cross section of wing occurs
Change so that the aspect ratio of wing changes, so that obtaining different lift using the aircraft of the wing.
Brief description of the drawings
Fig. 1 is the wing structure schematic perspective view；Fig. 2 is that the wing removes schematic top plan view after flexible covering；Fig. 3
It is to fold rib structure schematic diagram.
In figure, 1- telescopic rods, 2- folds rib, and 3- flexible coverings, 4- draw off gears, 5- connectors, the small ribs of 6-, 7- is small
Hole.
Embodiment
The present invention is illustrated below in conjunction with the accompanying drawings：A kind of folded wing, including telescopic rod 1, fold rib 2, soft
Property covering 3, draw off gear 4 and connector 5.Telescopic rod 1 is the supporting member of the wing, can carry out stretching motion；Connector 5 is used
It is attached in airframe；Folding on rib 2 has the small rib 6 of polylith, every piece small 6 mutual upper end of rib and upper end phase
Connection, lower end are connected with lower end, and rib 2 is entirely folded after expansion and seems undulate；It is all provided with these small ribs 6
There is aperture 7, fold rib 2 and be serially connected in by aperture 7 on telescopic rod 1；The head end of telescopic rod 1 is connected on connector 5, end connection
On the small rib 6 of last block for folding rib 2；First piece small rib, 6 phase for folding rib 2 is fixedly connected on connector 5；It is soft
Property covering 3 be divided to for two parts, a part, which is wrapped in, to be folded on rib 2, and another part is furled in draw off gear 4；Folding and unfolding fills
Put 4 to be fixed on connector 5, draw off gear 4 can be furled and be unfolded to flexible covering 3；When controlling telescopic rod 1 to extend,
Under the drive of telescopic rod 1, folding rib 2 is also unfolded, while draw off gear 4 also can be by the flexible covering in rolled condition
3 are unfolded and wrap the folding rib 2 after expansion；The length of wing is seen on the whole, and wing length is different, wing
Cross-sectional area is also different so that the aspect ratio using the aircraft of the wing is also different, so that the lift that wing obtains is different.
Claims (3)
- A kind of 1. folded wing, it is characterised in that：Including telescopic rod（1）, fold rib（2）, flexible covering（3）, draw off gear （4）And connector（5）；Telescopic rod（1）For the supporting member of the wing；Connector（5）For being attached with airframe；Fold Rib（2）On have the small rib of polylith（6）, every piece small rib（6）Mutual upper end is connected with upper end, and lower end is connected with lower end Connect, rib is entirely folded after expansion（2）Seem undulate；In these small ribs（6）On be equipped with aperture（7）, fold Rib（2）Pass through aperture（7）It is serially connected in telescopic rod（1）On；Telescopic rod（1）Head end be connected to connector（5）On, end is connected to Fold rib（2）The small rib of last block（6）On；Fold rib（2）First piece of small rib（6）Mutually it is fixedly connected on connector （5）On；Flexible covering（3）It is divided into two parts, a part is wrapped in folding rib（2）On, another part retracting is filled in folding and unfolding Put（4）It is interior；Draw off gear（4）It is fixed on connector（5）On.
- A kind of 2. folded wing according to claim 1, it is characterised in that：Telescopic rod（1）Quantity can also use two Or three or four.
- A kind of 3. folded wing according to claim 1 or 2, it is characterised in that：It is small that wing tip is equipped with wing tip position The wing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711299674.6A CN107972844A (en) | 2017-12-09 | 2017-12-09 | A kind of folded wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711299674.6A CN107972844A (en) | 2017-12-09 | 2017-12-09 | A kind of folded wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107972844A true CN107972844A (en) | 2018-05-01 |
Family
ID=62009686
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711299674.6A Withdrawn CN107972844A (en) | 2017-12-09 | 2017-12-09 | A kind of folded wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107972844A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111688913A (en) * | 2020-05-26 | 2020-09-22 | 哈尔滨工业大学 | Dual-drive wing with variable span length and up-down dihedral angle |
| CN114590395A (en) * | 2022-03-11 | 2022-06-07 | 中国人民解放军军事科学院国防科技创新研究院 | Flexible telescopic extension mechanism of folding wing |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102009060611A1 (en) * | 2009-12-28 | 2011-06-30 | Käser, Uwe, 69427 | Vehicle i.e. inflatable flight, for transportation on public road, has inflatable and/or telescopic profile segments swiveling out bearing surface and forming fully span width and profile geometry |
| CN203698648U (en) * | 2014-01-20 | 2014-07-09 | 谭大刚 | Flexible skin A-shaped aerofoil capable of being quickly unfolded and folded |
| US20150136898A1 (en) * | 2013-10-28 | 2015-05-21 | Jeremiah Benjamin Bowe McCoy | Telescopic Wing and Rack System for Automotive Airplane |
| CN105438444A (en) * | 2015-12-08 | 2016-03-30 | 山西大学 | Deformable wings and vertical take-off and landing aircraft using wings |
| CN205345318U (en) * | 2016-01-23 | 2016-06-29 | 蒋开权 | Flexible aircraft wing |
| CN107187581A (en) * | 2017-04-27 | 2017-09-22 | 深圳爱飞科技有限公司 | Retractable wing and aircraft |
-
2017
- 2017-12-09 CN CN201711299674.6A patent/CN107972844A/en not_active Withdrawn
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102009060611A1 (en) * | 2009-12-28 | 2011-06-30 | Käser, Uwe, 69427 | Vehicle i.e. inflatable flight, for transportation on public road, has inflatable and/or telescopic profile segments swiveling out bearing surface and forming fully span width and profile geometry |
| US20150136898A1 (en) * | 2013-10-28 | 2015-05-21 | Jeremiah Benjamin Bowe McCoy | Telescopic Wing and Rack System for Automotive Airplane |
| CN203698648U (en) * | 2014-01-20 | 2014-07-09 | 谭大刚 | Flexible skin A-shaped aerofoil capable of being quickly unfolded and folded |
| CN105438444A (en) * | 2015-12-08 | 2016-03-30 | 山西大学 | Deformable wings and vertical take-off and landing aircraft using wings |
| CN205345318U (en) * | 2016-01-23 | 2016-06-29 | 蒋开权 | Flexible aircraft wing |
| CN107187581A (en) * | 2017-04-27 | 2017-09-22 | 深圳爱飞科技有限公司 | Retractable wing and aircraft |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111688913A (en) * | 2020-05-26 | 2020-09-22 | 哈尔滨工业大学 | Dual-drive wing with variable span length and up-down dihedral angle |
| CN114590395A (en) * | 2022-03-11 | 2022-06-07 | 中国人民解放军军事科学院国防科技创新研究院 | Flexible telescopic extension mechanism of folding wing |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20180501 |
|
| WW01 | Invention patent application withdrawn after publication |