CN205499364U - Miniature aircraft of cell -phone folded form - Google Patents
Miniature aircraft of cell -phone folded form Download PDFInfo
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- CN205499364U CN205499364U CN201620119097.2U CN201620119097U CN205499364U CN 205499364 U CN205499364 U CN 205499364U CN 201620119097 U CN201620119097 U CN 201620119097U CN 205499364 U CN205499364 U CN 205499364U
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- fuselage
- rotating shaft
- support module
- shaft support
- phone folded
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Abstract
The utility model provides a miniature aircraft of cell -phone folded form, including fuselage and screw, the fuselage divide into left fuselage and right fuselage, rotates through the pivot subassembly between left fuselage and the right fuselage and connects, and the symmetry is equipped with the screw on left fuselage and the right fuselage, is equipped with miniature cloud platform on the right fuselage. Left fuselage is in the same place with the laminating of right fuselage under this miniature aircraft of cell -phone folded form fold condition for the whole bulk reduction of miniature aircraft, portable, about expanding during the use fuselage can, simple and convenient.
Description
Technical field
This utility model belongs to vehicle technology field, is specifically related to the minute vehicle of a kind of phone folded type.
Background technology
Minute vehicle (MAV, Micro Acnal
Vehicle. be also referred to as micro-robot) concept be first by some developed countries such as the U.S. in phase early 1990s propose.Compared with conventional unmanned vehicle, minute vehicle has that volume is little, the advantage of light weight, low cost, its handiness, maneuverability, noise is little, good concealment, make it have the biggest development prospect at military aspect and civilian aspect, therefore can use it for all kinds of monitoring, go on patrol, search and rescue, photograph, survey and draw investigation and the various fields such as investigation.
In order to easy to carry, minute vehicle can be designed to folding, but, the folding mode of the most traditional minute vehicle is mainly horn and folds or foot rest folding, this traditional folding mode is the biggest at the complete rear volume of aircraft foldable integral so that user carries the most convenient.
Utility model content
The purpose of this utility model is the problem overcoming existing foldable minitype aircraft volume after folding the biggest, inconvenient to carry.
For this, this utility model provides the minute vehicle of a kind of phone folded type, including fuselage and propeller, described fuselage is divided into left fuselage and right fuselage, it is rotationally connected by rotating assembly between described left fuselage and right fuselage, being arranged with propeller on described left fuselage and right fuselage, described right fuselage is provided with miniature The Cloud Terrace.
Further, above-mentioned miniature The Cloud Terrace includes camera, and miniature The Cloud Terrace is embedded in right fuselage edge.
Further, the thickness of above-mentioned miniature The Cloud Terrace is less than the thickness of right fuselage.
Further, the number of above-mentioned propeller is two or more.
Further, the both sides up and down of above-mentioned propeller are provided with protective cover.
Further, propeller is lived in above-mentioned protective cover all standing.
Further, above-mentioned protective cover is engraved structure.
Further, above-mentioned rotating assembly includes taper pin module, spring, rotating shaft support module one, rotating shaft support module two, rotating shaft support module three, rotating shaft support module four and rotating shaft set one, rotating shaft set two；Described rotating shaft set one and rotating shaft set two are separately positioned on the top and bottom of left fuselage and right fuselage junction, one end of rotating shaft support module one is fixed on left fuselage, the other end is enclosed within rotating shaft set one, one end of rotating shaft support module two is fixed on right fuselage, the other end is enclosed within rotating shaft set one, and one end of rotating shaft support module three is fixed on left fuselage, and the other end is enclosed within rotating shaft set two, one end of rotating shaft support module four is fixed on right fuselage, and the other end is enclosed within rotating shaft set two；Described rotating shaft support module one and rotating shaft support module two are provided with detent, and one end of taper pin module is provided with contour localization boss, and this contour localization boss is in mating connection with detent, and the other end of taper pin module connects spring.
The beneficial effects of the utility model:
(1) left fuselage can be realized relatively rotating of certain angle with right fuselage by rotating shaft by the minute vehicle of this phone folded type that this utility model provides, folded state bottom left fuselage fits together with right fuselage, minute vehicle overall volume is reduced, it is easy to carry, left and right fuselage is launched during use, simple and convenient.
(2) propeller of the minute vehicle of this phone folded type that this utility model provides is built in fuselage, it is provided that safety during aircraft flight.
Below with reference to accompanying drawing, this utility model is described in further details.
Accompanying drawing explanation
Fig. 1 is the structural representation of the minute vehicle deployed condition of this utility model phone folded type.
Fig. 2 is the minute vehicle shaft modular construction schematic diagram of this utility model phone folded type.
Fig. 3 is the structural representation of the minute vehicle folded state of this utility model phone folded type.
Fig. 4 be this utility model phone folded type minute vehicle in mounting structure for propeller schematic diagram.
Description of reference numerals: 1, left fuselage；2, rotating assembly；3, right fuselage；4, miniature The Cloud Terrace；5, propeller；6, protective cover；7, taper pin module；8, spring；9, rotating shaft support module one；10, rotating shaft support module two；11, rotating shaft support module three；12, rotating shaft support module four；13, rotating shaft set one；14, rotating shaft set two.
Detailed description of the invention
Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is clearly and completely described, it is clear that described embodiment is only a part of embodiment of this utility model rather than whole embodiments.Based on the embodiment in this utility model, 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 this utility model protection.
As shown in Figure 1, Figure 2, Figure 3 and Figure 4, present embodiments provide the minute vehicle of a kind of phone folded type, including fuselage and propeller 5, described fuselage is divided into left fuselage 1 and right fuselage 3, it is rotationally connected by rotating assembly 2 between described left fuselage 1 and right fuselage 3, being arranged with propeller 5 on described left fuselage 1 and right fuselage 3, described right fuselage 3 is provided with miniature The Cloud Terrace 4.
Wherein, according to the actual demand of different aircraft wing, the number of described propeller 5 is two or more, as each in two propellers 5, left fuselage 1 and right fuselage 3 one and symmetrical；During four propellers 5, as it is shown in figure 1, left fuselage 1 and each two and four of right fuselage 3 are distributed symmetrically and evenly；During six propellers 5, left fuselage 1 and each three and symmetrical of right fuselage 3.
Left fuselage 1 is connected with right fuselage 3 by rotating assembly 2 and is realized relatively rotating of certain angle, as it is shown on figure 3, left fuselage 1 fits together with right fuselage 3 under folded state, minute vehicle overall volume reduces, user can be directly loadable in pocket after being folded by this aircraft, easy to carry.And take out from pocket in use, spacing fixing by rotating assembly 2 after the left the rightest fuselage of fuselage 13 is realized the relatively rotating of 180 ° of angles, as it is shown in figure 1, aircraft reaches 180 ° of deployed conditions and can use, simple to operation.
A kind of embodiment of refinement, rotating assembly 2 concrete as in figure 2 it is shown, include taper pin module 7, spring 8, rotating shaft support module 1, rotating shaft support module 2 10, rotating shaft support module 3 11, rotating shaft support module 4 12 and rotating shaft set 1, rotating shaft set 2 14；Described rotating shaft set 1 and rotating shaft set 2 14 are separately positioned on the top and bottom of left fuselage 1 and right fuselage 3 junction, one end of rotating shaft support module 1 is fixed on left fuselage 1, the other end is enclosed within rotating shaft set 1, one end of rotating shaft support module 2 10 is fixed on right fuselage 3, the other end is enclosed within rotating shaft set 1, one end of rotating shaft support module 3 11 is fixed on left fuselage 1, the other end is enclosed within rotating shaft set 2 14, one end of rotating shaft support module 4 12 is fixed on right fuselage 3, and the other end is enclosed within rotating shaft set 2 14；Rotating shaft support module 1 and rotating shaft support module 3 11 can rotate with left fuselage 1 and rotate, and rotating shaft support module 2 10 and rotating shaft support module 4 12 can rotate with right fuselage 3 and rotate.
Described rotating shaft support module 1 and rotating shaft support module 2 10 are provided with detent, and one end of taper pin module 7 is provided with contour localization boss, and this contour localization boss is in mating connection with detent, and the other end of taper pin module 7 connects spring 8.When aircraft needs to launch flight, the left the rightest fuselage of fuselage 13 realizes when relatively rotating of 180 ° of angles, detent in rotating shaft support module 1 and rotating shaft support module 2 10 aligns with the contour localization boss of taper pin module 7, under the elastic force effect of spring 8, the contour localization boss of taper pin module 7 snaps in the detent of rotating shaft support module 1 and rotating shaft support module 2 10, make left fuselage 1 cannot relatively rotate with right fuselage 3, keep 180 ° of angle states.When aircraft make to be finished need fold time, by hand propelled taper pin module 7, make taper pin module 7 depart from from the detent of rotating shaft support module 1 and rotating shaft support module 2 10, the most left the rightest fuselage of fuselage 13 can relatively rotate, such that it is able to realize folding.
Miniature The Cloud Terrace 4 includes camera, is used for monitoring, observation etc.；And for more convenient observation, described miniature The Cloud Terrace 4 is embedded in right fuselage 3 edge；The thickness of described miniature The Cloud Terrace 4 is less than the thickness of right fuselage 3 so that when folding fuselage, the profile of miniature The Cloud Terrace 4 is unaffected.
Additionally; hurted sb.'s feelings in order to avoid flying out after during flight, propeller lost efficacy; improve the safety of minute vehicle; as shown in Figure 4; the both sides up and down of described propeller 5 are provided with protective cover 6; the protective cover 6 of both sides is fixing with fuselage up and down is connected, and the protective cover 6 of upper and lower both sides forms the cavity accommodating propeller 5 with fuselage.In order to more fully protect propeller 5, preventing propeller 5 from flying out and hurt sb.'s feelings, propeller 5 is lived in all standing of described protective cover 6.
And described protective cover 6 is engraved structure, engraved structure alleviates the weight of minute vehicle, can play protective action, bring excessive burden will not to again this minute vehicle.
Shown in sum up, after the minute vehicle of this phone folded type that this utility model provides folds, overall volume is less, it is simple to carry；, propeller is built in fuselage meanwhile, improves the safety of minute vehicle.
Exemplified as above is only to illustration of the present utility model, is not intended that the restriction to protection domain of the present utility model, within the every and same or analogous design of this utility model belongs to protection domain of the present utility model.
Claims (8)
1. the minute vehicle of a phone folded type, including fuselage and propeller (5), it is characterized in that: described fuselage is divided into left fuselage (1) and right fuselage (3), it is rotationally connected by rotating assembly (2) between described left fuselage (1) and right fuselage (3), being arranged with propeller (5) on described left fuselage (1) and right fuselage (3), described right fuselage (3) is provided with miniature The Cloud Terrace (4).
2. the minute vehicle of phone folded type as claimed in claim 1, it is characterised in that: described miniature The Cloud Terrace (4) includes camera, and miniature The Cloud Terrace (4) is embedded in right fuselage (3) edge.
3. the minute vehicle of phone folded type as claimed in claim 2, it is characterised in that: the thickness of described miniature The Cloud Terrace (4) is less than the thickness of right fuselage (3).
4. the minute vehicle of phone folded type as claimed in claim 1, it is characterised in that: the number of described propeller (5) is two or more.
5. the minute vehicle of phone folded type as claimed in claim 1, it is characterised in that: the both sides up and down of described propeller (5) are provided with protective cover (6).
6. the minute vehicle of phone folded type as claimed in claim 5, it is characterised in that: propeller (5) is lived in described protective cover (6) all standing.
7. the minute vehicle of phone folded type as claimed in claim 6, it is characterised in that: described protective cover (6) is engraved structure.
8. the minute vehicle of phone folded type as claimed in claim 1, it is characterised in that: described rotating assembly (2) includes taper pin module (7), spring (8), rotating shaft support module one (9), rotating shaft support module two (10), rotating shaft support module three (11), rotating shaft support module four (12) and rotating shaft set one (13), rotating shaft set two (14)；
Described rotating shaft set one (13) and rotating shaft set two (14) are separately positioned on the top and bottom of left fuselage (1) and right fuselage (3) junction, one end of rotating shaft support module one (9) is fixed on left fuselage (1), the other end is enclosed within rotating shaft set one (13), one end of rotating shaft support module two (10) is fixed on right fuselage (3), the other end is enclosed within rotating shaft set one (13), one end of rotating shaft support module three (11) is fixed on left fuselage (1), the other end is enclosed within rotating shaft set two (14), one end of rotating shaft support module four (12) is fixed on right fuselage (3), the other end is enclosed within rotating shaft set two (14)；
Described rotating shaft support module one (9) and rotating shaft support module two (10) are provided with detent, one end of taper pin module (7) is provided with contour localization boss, this contour localization boss is in mating connection with detent, and the other end of taper pin module (7) connects spring (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620119097.2U CN205499364U (en) | 2016-02-14 | 2016-02-14 | Miniature aircraft of cell -phone folded form |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620119097.2U CN205499364U (en) | 2016-02-14 | 2016-02-14 | Miniature aircraft of cell -phone folded form |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205499364U true CN205499364U (en) | 2016-08-24 |
Family
ID=56725241
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620119097.2U Active CN205499364U (en) | 2016-02-14 | 2016-02-14 | Miniature aircraft of cell -phone folded form |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205499364U (en) |
-
2016
- 2016-02-14 CN CN201620119097.2U patent/CN205499364U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address | ||
| CP03 | Change of name, title or address |
Address after: 518000 Room 201, building A, No. 1, Qian Wan Road, Qianhai Shenzhen Hong Kong cooperation zone, Shenzhen, Guangdong (Shenzhen Qianhai business secretary Co., Ltd.) Patentee after: Puzhou Technology (Shenzhen) Co.,Ltd. Address before: 518000 Room 201, building A, 1 front Bay Road, Shenzhen Qianhai cooperation zone, Shenzhen, Guangdong Patentee before: PRODRONE TECHNOLOGY (SHENZHEN) Co.,Ltd. |