CN204688401U - Unmanned plane telescopic folding wing device - Google Patents
Unmanned plane telescopic folding wing device Download PDFInfo
- Publication number
- CN204688401U CN204688401U CN201520386526.8U CN201520386526U CN204688401U CN 204688401 U CN204688401 U CN 204688401U CN 201520386526 U CN201520386526 U CN 201520386526U CN 204688401 U CN204688401 U CN 204688401U
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- wing
- lip
- oblique
- magnetic stripe
- half degree
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Abstract
Unmanned plane telescopic folding wing device.Its composition of this product comprises: unmanned aerial vehicle body, the left side of described unmanned aerial vehicle body connects left wing, the right side of described unmanned aerial vehicle body connects right wing, described left wing and described right wing all have grafting cavity, the front side of described cavity connects first half degree of lip-rounding slideway, the rear side of described cavity connects later half degree of lip-rounding slideway, described cavity is built with flexible wing, the both sides flush fit of described flexible wing inserts described first half degree of lip-rounding slideway and described later half degree of lip-rounding slideway respectively, described left wing is all connected upper oblique spring bearer plate and declivity spring bearer plate with the outer end of described right wing, described upper oblique spring bearer plate is all connected magnetic stripe plate with the end of described declivity spring bearer plate, described flexible wing all inlay one group of transversely arranged adhesive magnetic stripe above and below, the magnetic stripe plate described in the adhesive of adhesive magnetic stripe described in when described flexible wing pulls out is fixed.The utility model is used for unmanned plane.
Description
Technical field
the utility model relates to a kind of unmanned plane telescopic folding wing device.
Background technology
the winged length of existing unmanned plane, width, angle are all changeless, can not use, use dumb, inconvenient under different occasions, different height.
Summary of the invention
the purpose of this utility model is to provide one and can changes as required, the unmanned plane telescopic folding wing device used under being applicable to all occasions, height.
above-mentioned object is realized by following technical scheme:
a kind of unmanned plane telescopic folding wing device, its composition comprises: unmanned aerial vehicle body, the left side of described unmanned aerial vehicle body connects left wing, the right side of described unmanned aerial vehicle body connects right wing, described left wing and described right wing all have grafting cavity, the front side of described cavity connects first half degree of lip-rounding slideway, the rear side of described cavity connects later half degree of lip-rounding slideway, described cavity is built with flexible wing, the both sides flush fit of described flexible wing inserts described first half degree of lip-rounding slideway and described later half degree of lip-rounding slideway respectively, described left wing is all connected upper oblique spring bearer plate and declivity spring bearer plate with the outer end of described right wing, described upper oblique spring bearer plate is all connected magnetic stripe plate with the end of described declivity spring bearer plate, described flexible wing all inlay one group of transversely arranged adhesive magnetic stripe above and below, the magnetic stripe plate described in the adhesive of adhesive magnetic stripe described in when described flexible wing pulls out is fixed.
described unmanned plane telescopic folding wing device, the tail end of described unmanned aerial vehicle body connects vertical tail, the left side of described vertical tail connects left oblique secondary wing, the right side of described vertical tail connects right oblique secondary wing, the oblique secondary wing of the oblique secondary wing in a described left side and the described right side all has grafting cavity body, the front side of described cavity body connects front oblique half degree of lip-rounding slideway, the rear side of described cavity body connects half degree of lip-rounding slideway that retreads, described cavity body is built with the wing that tiltedly stretches, the both sides flush fit of described tiltedly flexible wing inserts described front oblique half degree of lip-rounding slideway and described half degree of lip-rounding slideway that retreads respectively, the oblique secondary wing in a described left side is all connected described upper oblique spring bearer plate and described declivity spring bearer plate with the outer end of the oblique secondary wing in the described right side, the adhesive magnetic stripe all inlayed above and below described in one group of described tiltedly flexible wing, the magnetic stripe plate described in the adhesive of adhesive magnetic stripe described in when described tiltedly flexible wing pulls out is fixed.
described unmanned plane telescopic folding wing device, described tiltedly flexible wing connects left oblique pull plate and right oblique pull plate respectively, described left oblique pull plate is all connected lower magnetic sheet with the bottom of described right oblique pull plate, the described adhesive magnetic stripe on the described flexible wing described in lower magnetic sheet adhesive.
beneficial effect:
1. the utility model adopts first half degree of lip-rounding slideway, later half degree of lip-rounding slideway can help the fixing flexible wing inserted in cavity, flexible wing is inserted and pull-out time convenient; Front oblique half degree of lip-rounding slideway, half degree of lip-rounding slideway that retreads can help the fixing tiltedly flexible wing inserted in cavity body, convenient when making tiltedly to stretch wing insertion and pull-out.
the upper oblique spring bearer plate that the utility model adopts, declivity spring bearer plate, magnetic stripe plate, adhesive magnetic stripe are with the use of fixing the flexible wing after stretching well or the wing that tiltedly stretches, make the flexible wing after pull-out, insertion or wing firm stable of tiltedly stretching, use safety.
the flexible wing that the utility model adopts, tiltedly flexible wing can lengthen, can shorten, and under being applicable to differing heights, varying environment, flight uses, use safety, lengthen, shorten all convenient.
the left oblique pull plate that the utility model adopts, right oblique pull plate, lower magnetic sheet are more firm, stable with the use of the connection of tiltedly stretching between wing and flexible wing that can make after lengthening, shortening.
accompanying drawing illustrates:
accompanying drawing 1 is the structural representation of this product.
detailed description of the invention:
embodiment 1:
a kind of unmanned plane telescopic folding wing device, its composition comprises: unmanned aerial vehicle body 1, the left side of described unmanned aerial vehicle body connects left wing 2, the right side of described unmanned aerial vehicle body connects right wing 3, described left wing and described right wing all have grafting cavity 4, the front side of described cavity connects first half degree of lip-rounding slideway 5, the rear side of described cavity connects later half degree of lip-rounding slideway 6, described cavity is built with flexible wing 7, the both sides flush fit of described flexible wing inserts described first half degree of lip-rounding slideway and described later half degree of lip-rounding slideway respectively, described left wing is all connected upper oblique spring bearer plate 8 and declivity spring bearer plate 9 with the outer end of described right wing, described upper oblique spring bearer plate is all connected magnetic stripe plate 10 with the end of described declivity spring bearer plate, described flexible wing all inlay one group of transversely arranged adhesive magnetic stripe 11 above and below, the magnetic stripe plate described in the adhesive of adhesive magnetic stripe described in when described flexible wing pulls out is fixed.
embodiment 2:
unmanned plane telescopic folding wing device described in embodiment 1, the tail end of described unmanned aerial vehicle body connects vertical tail 12, the left side of described vertical tail connects left oblique secondary wing 13, the right side of described vertical tail connects right oblique secondary wing 14, the oblique secondary wing of the oblique secondary wing in a described left side and the described right side all has grafting cavity body 15, the front side of described cavity body connects front oblique half degree of lip-rounding slideway 16, the rear side of described cavity body connects half degree of lip-rounding slideway 17 that retreads, described cavity body is built with the wing 18 that tiltedly stretches, the both sides flush fit of described tiltedly flexible wing inserts described front oblique half degree of lip-rounding slideway and described half degree of lip-rounding slideway that retreads respectively, the oblique secondary wing in a described left side is all connected described upper oblique spring bearer plate and described declivity spring bearer plate with the outer end of the oblique secondary wing in the described right side, the adhesive magnetic stripe all inlayed above and below described in one group of described tiltedly flexible wing, the magnetic stripe plate described in the adhesive of adhesive magnetic stripe described in when described tiltedly flexible wing pulls out is fixed.
embodiment 3:
unmanned plane telescopic folding wing device described in embodiment 2, described tiltedly flexible wing connects left oblique pull plate 19 and right oblique pull plate 20 respectively, described left oblique pull plate is all connected lower magnetic sheet 21 with the bottom of described right oblique pull plate, the described adhesive magnetic stripe on the described flexible wing described in lower magnetic sheet adhesive.
Claims (3)
1. a unmanned plane telescopic folding wing device, its composition comprises: unmanned aerial vehicle body, it is characterized in that: the left side of described unmanned aerial vehicle body connects left wing, the right side of described unmanned aerial vehicle body connects right wing, described left wing and described right wing all have grafting cavity, the front side of described cavity connects first half degree of lip-rounding slideway, the rear side of described cavity connects later half degree of lip-rounding slideway, described cavity is built with flexible wing, the both sides flush fit of described flexible wing inserts described first half degree of lip-rounding slideway and described later half degree of lip-rounding slideway respectively, described left wing is all connected upper oblique spring bearer plate and declivity spring bearer plate with the outer end of described right wing, described upper oblique spring bearer plate is all connected magnetic stripe plate with the end of described declivity spring bearer plate, described flexible wing all inlay one group of transversely arranged adhesive magnetic stripe above and below, the magnetic stripe plate described in the adhesive of adhesive magnetic stripe described in when described flexible wing pulls out is fixed.
2. unmanned plane telescopic folding wing device according to claim 1, it is characterized in that: the tail end of described unmanned aerial vehicle body connects vertical tail, the left side of described vertical tail connects left oblique secondary wing, the right side of described vertical tail connects right oblique secondary wing, the oblique secondary wing of the oblique secondary wing in a described left side and the described right side all has grafting cavity body, the front side of described cavity body connects front oblique half degree of lip-rounding slideway, the rear side of described cavity body connects half degree of lip-rounding slideway that retreads, described cavity body is built with the wing that tiltedly stretches, the both sides flush fit of described tiltedly flexible wing inserts described front oblique half degree of lip-rounding slideway and described half degree of lip-rounding slideway that retreads respectively, the oblique secondary wing in a described left side is all connected described upper oblique spring bearer plate and described declivity spring bearer plate with the outer end of the oblique secondary wing in the described right side, the adhesive magnetic stripe all inlayed above and below described in one group of described tiltedly flexible wing, the magnetic stripe plate described in the adhesive of adhesive magnetic stripe described in when described tiltedly flexible wing pulls out is fixed.
3. unmanned plane telescopic folding wing device according to claim 2, it is characterized in that: described tiltedly flexible wing connects left oblique pull plate and right oblique pull plate respectively, described left oblique pull plate is all connected lower magnetic sheet with the bottom of described right oblique pull plate, the described adhesive magnetic stripe on the described flexible wing described in lower magnetic sheet adhesive.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201520386526.8U CN204688401U (en) | 2015-06-08 | 2015-06-08 | Unmanned plane telescopic folding wing device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201520386526.8U CN204688401U (en) | 2015-06-08 | 2015-06-08 | Unmanned plane telescopic folding wing device |
Publications (1)
Publication Number | Publication Date |
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CN204688401U true CN204688401U (en) | 2015-10-07 |
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Family Applications (1)
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CN201520386526.8U Expired - Fee Related CN204688401U (en) | 2015-06-08 | 2015-06-08 | Unmanned plane telescopic folding wing device |
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CN (1) | CN204688401U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105667761A (en) * | 2016-03-02 | 2016-06-15 | 同济大学 | Foldable connecting joined wing unmanned aerial vehicle |
-
2015
- 2015-06-08 CN CN201520386526.8U patent/CN204688401U/en not_active Expired - Fee Related
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105667761A (en) * | 2016-03-02 | 2016-06-15 | 同济大学 | Foldable connecting joined wing unmanned aerial vehicle |
CN105667761B (en) * | 2016-03-02 | 2017-12-26 | 同济大学 | A kind of foldable connection wing layout unmanned plane |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20151007 Termination date: 20160608 |