CN203889067U - Two-axis flight vehicle and two-axis flight system capable of carrying large banners - Google Patents
Two-axis flight vehicle and two-axis flight system capable of carrying large banners Download PDFInfo
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- CN203889067U CN203889067U CN201420329517.0U CN201420329517U CN203889067U CN 203889067 U CN203889067 U CN 203889067U CN 201420329517 U CN201420329517 U CN 201420329517U CN 203889067 U CN203889067 U CN 203889067U
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- diaxon
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- axis flight
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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Abstract
The utility model discloses a two-axis flight vehicle and a two-axis flight system capable of carrying large banners. The two-axis flight vehicle comprises a frame, noses, a steering engine, a control surface and an electric control device; the frame is flat plate-shaped; the noses are arranged at the front end of the frame; the steering engine is arranged at the middle part of the bottom surface of the frame and connected with the noses by use of pull rods; the control surface is arranged at the tail of the top surface of the frame; the electric control device is arranged on the top surface of the frame; two noises are arranged; a quick demounting device is arranged at the tail end of the frame. The two-axis flight vehicle is used for solving the problems of the existing flight vehicle, such as large structure volume and inflexible operation and the problem that the advertisement banners only can be hung in fixed regions for advertising and cannot be moved for advertising; the two-axis flight vehicle is light and flexible and has the characteristic of low operation cost; designed on the basis of the two-axis flight vehicle, the two-axis flight system capable of carrying large banners is capable of reaching the purpose of moving the advertisement banners for advertising and has the characteristic of low cost.
Description
Technical field
The utility model relates to advertising technical field, specifically, is a kind of diaxon aircraft and the diaxon flight system that can carry large-scale banner.
Background technology
Aircraft, as a kind of instrument of operation aloft, have conveniently feature, in existing aircraft, because of the difference of effect, to be divided into aircraft, fire balloon, spacecraft, telecontrolled aircraft etc. multiple, and these aircraft are on structure arranges, power unit is all located at horizontal upper part or the bottom of cycle fuselage, and fuselage is adopt structures such as cabin also more, the structural volume heaviness that whole setting forms out, move dumbly, can not serve as the small-sized active tool of low cost and use.
The today emerging internet heroes, various advertising mode layers go out infinite, outdoor advertising publicity conduct a kind of publicity measures wherein, still be widely used, existing outdoor advertising apparatus is multiplex such as X Display Rack, fire balloon, support, wall curtain, lamp box, post stand etc., wherein fire balloon and support are multiplex in the publicity of ad banner, in use utilize fire balloon that ad banner is hung to publicity, or with support by fixing the width axle at ad banner two ends to reach the object of display advertisement banner, but both in use can only carry out advertising display in fixed area, allow movable crowd in this advertising area know, can not allow movable crowd outside this region know, can not play the widely object of publicity.
Utility model content
The purpose of this utility model is to solve existing Flight Vehicle Structure volume heaviness, move dumb, the problem that banner can only publicize in fixed area, can not move publicity to ad banner, and design a kind of diaxon aircraft and can carry the diaxon flight system of large-scale banner, a kind of diaxon aircraft has the characteristic of light and flexible, the feature that operating cost is low, the diaxon flight system that carries large-scale banner designing on a kind of diaxon aircraft basis can be realized the object of mobile exploitation banner, has the characteristic that use cost is cheap.
The utility model is achieved through the following technical solutions: a kind of diaxon aircraft, comprise frame, head, steering wheel, rudder face, electrical controller, described frame is tabular, and described head is arranged on the front end of frame, described steering wheel is arranged on the middle part, bottom surface of frame, and connects with head by pull bar; Described rudder face is arranged on the end face afterbody of frame, and described electrical controller is arranged on frame end face, and described head is two.
Further, for better realizing the utility model, described head comprises motor cabinet, brushless motor, screw propeller, described motor cabinet can vert left and right, and be provided with screw propeller at motor cabinet front end, be provided with brushless motor in described motor cabinet inside, described steering wheel connects with motor cabinet rear end by pull bar.
Further, for better realizing the utility model, described electrical controller comprises battery pack, battery, central controller, electronic governor, described battery pack is arranged on frame end face, described battery is placed in battery pack, described central controller is connecting electronic governor and brushless motor successively, and described central controller connects steering wheel.
Further, for better realizing the utility model, also comprise protective case, described protective case is arranged on frame end face and covers central controller, electronic governor and battery pack.
Further, for better realizing the utility model, also comprise handgrip, described handgrip is arranged on frame bottom surface.
Can carry the diaxon flight system of large-scale banner, comprise a kind of diaxon aircraft and device for quickly disassembling, described device for quickly disassembling is arranged on the tail end of frame.
Further, for better realizing the utility model, described device for quickly disassembling adopts clamp structure.
The utility model compared with prior art, has the following advantages and beneficial effect:
(1) the utility model solves existing Flight Vehicle Structure volume heaviness, move dumb, the problem that ad banner can only publicize in fixed area, can not move publicity to ad banner, a kind of diaxon aircraft has the characteristic of light and flexible, the feature that operating cost is low, the diaxon flight system that carries large-scale banner designing on a kind of basis of diaxon aircraft can be realized the object of mobile exploitation banner, has the characteristic that use cost is cheap.
(2) steering wheel described in the utility model drives two brushless motors to vert around two motor cabinets by pull bar, thereby the component about producing is realized the driftage of aircraft.
(3) frame described in the utility model is tabular, and this special aerodynamic arrangement has determined its manoevreability, can realize the exceedingly difficult movements such as inverted flight, wide-angle pitching, gives magnificent visual enjoyment.
(4) action of rudder face described in the utility model can realize roll and the pitching of aircraft in flight course.
(5) device for quickly disassembling described in the utility model can be settled ad banner and colored dragon and phoenix silk ribbon etc., thereby makes aircraft give magnificent visual enjoyment.
(6) in the utility model use, device for quickly disassembling hangs banner or other public's campaign materials, because of lighter weight, can control easily suspension attitude by the flexible control of head, and clear displaying neatly in public.
(7) the utility model is made accessory and extensively maturation of material market supply, and cost is low, and Installation and Debugging are convenient, and technical risk is low.
Brief description of the drawings
Fig. 1 is birds-eye view of the present utility model.
Fig. 2 is upward view of the present utility model.
Fig. 3 is the left view of Fig. 1.
Fig. 4 is electrical connection diagram of the present utility model.
Wherein, 1-frame, 2-motor cabinet, 3-brushless motor, 4-screw propeller, 5-steering wheel, 6-rudder face, 7-device for quickly disassembling, 8-electrical controller, 9-pull bar, 10-protective case, 11-battery pack, 12-battery, 13-handgrip, 14-central controller, 15-electronic governor.
Detailed description of the invention
Below in conjunction with embodiment, the utility model is described in further detail, but embodiment of the present utility model is not limited to this.
Embodiment 1:
A kind of diaxon aircraft, shown in Fig. 1, Fig. 2, Fig. 3, Fig. 4, comprise frame 1, head, steering wheel 5, rudder face 6, electrical controller 8, described frame 1 is tabular, described head is arranged on the front end of frame 1, described steering wheel 5 is arranged on the middle part, bottom surface of frame 1, and connects with head by pull bar 9; Described rudder face 6 is arranged on the end face afterbody of frame 1, and described electrical controller 8 is arranged on frame 1 end face, and described head is two.
In use, electrical controller 8 is controlled steering wheel 5, steering wheel 5 changes the service direction of head by pull bar 9, electrical controller also provides head operation power simultaneously, under the effect of head operation power and service direction, drive fuselage to make various run action on high, the action of rudder face 6 can realize roll and the pitching of aircraft in flight course, electrical controller 8 is provided with GPS module and self-control system can complete the task of spot hover and autonomous cruise, solve existing Flight Vehicle Structure volume heaviness, move dumb, the problem that ad banner can only publicize in fixed area, can not move publicity to ad banner, a kind of diaxon aircraft has the characteristic of light and flexible, the feature that operating cost is low, the diaxon flight system that carries large-scale banner designing on a kind of basis of diaxon aircraft can be realized the object of mobile exploitation banner, there is the characteristic that use cost is cheap.
Embodiment 2:
The present embodiment is at the enterprising one-step optimization in the basis of above-described embodiment, further, for better realizing the utility model, be convenient to steering wheel and control flexibly the direction of head, the component that produces left and right is realized the driftage of aircraft, in conjunction with Fig. 1, Fig. 2, Fig. 3, shown in Fig. 4, be arranged to especially following structure: described head comprises motor cabinet 2, brushless motor 3, screw propeller 4, described motor cabinet 2 can vert left and right, and be provided with screw propeller 4 at motor cabinet 2 front ends, be provided with brushless motor 3 in described motor cabinet 2 inside, described steering wheel 5 connects with motor cabinet 2 rear ends by pull bar 9.
Embodiment 3:
The present embodiment is at the enterprising one-step optimization in the basis of above-described embodiment, further, for better realizing the utility model, being convenient to provides power to aircraft, control speed, the direction of aircraft, as shown in Figure 4, be arranged to especially following structure: described electrical controller 8 comprises battery pack 11, battery 12, central controller 14, electronic governor 15, described battery pack 11 is arranged on frame 1 end face, described battery 12 is placed in battery pack 11, described central controller 14 is connecting electronic governor 15 and brushless motor 3 successively, and described central controller 14 connects steering wheel 5.
Embodiment 4:
The present embodiment is at the enterprising one-step optimization in the basis of above-described embodiment; further; for better realizing the utility model; can protect the electric-control system equipment such as central process unit, electronic governor, battery pack; shown in Fig. 1, Fig. 2, Fig. 3; be arranged to especially following structure: also comprise protective case 10, described protective case 10 is arranged on frame 1 end face and covers central controller 14, electronic governor 15 and battery pack 11.
Embodiment 5:
The present embodiment is at the enterprising one-step optimization in the basis of above-described embodiment, further, and for better realizing the utility model, facilitate grabbing of aircraft to take, shown in Fig. 1, Fig. 3, following structure is set especially: also comprise handgrip 13, described handgrip 13 is arranged on frame 1 bottom surface.
Embodiment 6:
The present embodiment is at the enterprising one-step optimization in the basis of above-described embodiment, large for solving the material amounts of expending such as traditional publicity measures support, balloon; Take up room large and install inconvenient; Because placement location large contingent easily damages, cause material waste; Can only fix a place, can not move the problem of publicity, shown in Fig. 1, Fig. 2, Fig. 3, Fig. 4, following structure is set especially: the diaxon flight system that can carry large-scale banner, comprise a kind of diaxon aircraft and device for quickly disassembling 7, described device for quickly disassembling 7 is arranged on the tail end of frame 1.
Embodiment 7:
The present embodiment is at the enterprising one-step optimization in the basis of above-described embodiment, further, for better realizing the utility model, adapt to different size banner, join extension thing, realize on a large scale, repeatedly several recycling, economize on resources and cost, be arranged to especially following structure: described device for quickly disassembling 7 adopts clamp structure.
In use, by central controller, can realize real-time monitoring according to field conditions, also can realize setting path autonomous flight and the flight of setting regions automatic cruising.
The utility model solves existing Flight Vehicle Structure volume heaviness, move dumb, the problem that ad banner can only publicize in fixed area, can not move publicity to ad banner, a kind of diaxon aircraft has the characteristic of light and flexible, the feature that operating cost is low, the diaxon flight system that carries large-scale banner designing on a kind of basis of diaxon aircraft can be realized the object of mobile exploitation banner, has the characteristic that use cost is cheap.
The above; it is only preferred embodiment of the present utility model; not the utility model is done to any pro forma restriction, any simple modification, equivalent variations that every foundation technical spirit of the present utility model is done above embodiment, within all falling into protection domain of the present utility model.
Claims (7)
1. a diaxon aircraft, it is characterized in that: comprise frame (1), head, steering wheel (5), rudder face (6), electrical controller (8), described frame (1) is tabular, described head is arranged on the front end of frame (1), described steering wheel (5) is arranged on the middle part, bottom surface of frame (1), and connects with head by pull bar (9); Described rudder face (6) is arranged on the end face afterbody of frame (1), and described electrical controller (8) is arranged on frame (1) end face, and described head is two.
2. a kind of diaxon aircraft according to claim 1, it is characterized in that: described head comprises motor cabinet (2), brushless motor (3), screw propeller (4), described motor cabinet (2) can vert left and right, and be provided with screw propeller (4) at motor cabinet (2) front end, be provided with brushless motor (3) in described motor cabinet (2) inside, described steering wheel (5) connects by the same motor cabinet of pull bar (9) (2) rear end.
3. a kind of diaxon aircraft according to claim 1, it is characterized in that: described electrical controller (8) comprises battery pack (11), battery (12), central controller (14), electronic governor (15), described battery pack (11) is arranged on frame (1) end face, described battery (12) is placed in battery pack (11), described central controller (14) is connecting electronic governor (15) and brushless motor (3) successively, and described central controller (14) connects steering wheel (5).
4. a kind of diaxon aircraft according to claim 3, is characterized in that: also comprise protective case (10), described protective case (10) is arranged on frame (1) end face and covers central controller (14), electronic governor (15) and battery pack (11).
5. according to a kind of diaxon aircraft described in claim 1-4 any one, it is characterized in that: also comprise handgrip (13), described handgrip (13) is arranged on frame (1) bottom surface.
6. the diaxon flight system that can carry large-scale banner, is characterized in that: comprise a kind of diaxon aircraft and device for quickly disassembling (7) described in claim 1-5, described device for quickly disassembling (7) is arranged on the tail end of frame (1).
7. the diaxon flight system that can carry according to claim 6 large-scale banner, is characterized in that: described device for quickly disassembling (7) adopts clamp structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420329517.0U CN203889067U (en) | 2014-06-20 | 2014-06-20 | Two-axis flight vehicle and two-axis flight system capable of carrying large banners |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420329517.0U CN203889067U (en) | 2014-06-20 | 2014-06-20 | Two-axis flight vehicle and two-axis flight system capable of carrying large banners |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203889067U true CN203889067U (en) | 2014-10-22 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420329517.0U Expired - Fee Related CN203889067U (en) | 2014-06-20 | 2014-06-20 | Two-axis flight vehicle and two-axis flight system capable of carrying large banners |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203889067U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105404310A (en) * | 2015-11-27 | 2016-03-16 | 深圳一电科技有限公司 | Unmanned plane flying control method and unmanned plane flying control device |
| CN109260721A (en) * | 2018-11-08 | 2019-01-25 | 重庆大学 | A kind of model rocket of pinpoint landing |
| CN109493762A (en) * | 2019-01-19 | 2019-03-19 | 海安荣民汽车配件有限公司 | Automobile plant's propaganda scroll lifting jack |
-
2014
- 2014-06-20 CN CN201420329517.0U patent/CN203889067U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105404310A (en) * | 2015-11-27 | 2016-03-16 | 深圳一电科技有限公司 | Unmanned plane flying control method and unmanned plane flying control device |
| CN109260721A (en) * | 2018-11-08 | 2019-01-25 | 重庆大学 | A kind of model rocket of pinpoint landing |
| CN109493762A (en) * | 2019-01-19 | 2019-03-19 | 海安荣民汽车配件有限公司 | Automobile plant's propaganda scroll lifting jack |
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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 |
Granted publication date: 20141022 Termination date: 20160620 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |