CN204750575U - Multiaxis unmanned vehicles - Google Patents
Multiaxis unmanned vehicles Download PDFInfo
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- CN204750575U CN204750575U CN201520339906.6U CN201520339906U CN204750575U CN 204750575 U CN204750575 U CN 204750575U CN 201520339906 U CN201520339906 U CN 201520339906U CN 204750575 U CN204750575 U CN 204750575U
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- solar panel
- multiaxis unmanned
- unmanned vehicle
- fuselage main
- main body
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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
- Y02T50/50—On board measures aiming to increase energy efficiency
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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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- Electric Propulsion And Braking For Vehicles (AREA)
Abstract
The utility model relates to an unmanned aerial vehicle field especially relates to a multiaxis unmanned vehicles who has solar cell panel. Multiaxis unmanned vehicles includes: the fuselage main part, follow the horizontal outside many radical axis that extend are followed to the fuselage main part, separate each other between the arbitrary adjacent two shafts in order to form the betweencenters clearance, from this in many radical axis many radical axis have formed a plurality of betweencenters clearances that correspond, a plurality of mutually independent solar cell panel, each for inciting somebody to action solar energy transformation becomes the electric energy solar cell panel sets up a correspondence in a plurality of betweencenters clearances betweencenters clearance department is in order to cover the correspondence the betweencenters clearance. The utility model discloses a solar cell panel can install on multiaxis unmanned vehicles, and solar cell panel can provide the electric energy for multiaxis unmanned vehicles, has increased multiaxis unmanned vehicles's hang time. The utility model discloses a solar cell panel sets up in betweencenters clearance department, has utilized multiaxis unmanned vehicles's idle space.
Description
Technical field
The utility model relates to unmanned plane field, particularly relates to a kind of multiaxis unmanned vehicle with solar panel.
Background technology
The application of unmanned plane is more and more extensive, they mainly with electric energy as power.Be limited to existing energy-storage battery technical merit, the hang time of unmanned plane is general shorter.Disclosed in CN201420834554.7 shown in multiaxis unmanned vehicle, usually, multiaxis unmanned vehicle generally comprises fuselage and axle, is provided with frame in the bottom of fuselage, is provided with rotor at axle away from the far-end of fuselage.
Utility model content
An object of the present utility model to provide a kind of technical scheme improving the hang time of multiaxis unmanned vehicle.
The utility model further object to provide a kind of technical scheme being removably installed in multiaxis unmanned vehicle, improves the hang time of multiaxis unmanned vehicle further.
Another further object of the utility model is when installing solar panel, reduces the change to multiaxis unmanned vehicle structure as far as possible.
According to an aspect of the present utility model, the utility model provides a kind of multiaxis unmanned vehicle, comprising:
Fuselage main body;
From described fuselage main body transversely outward extending many axles, in described many axles arbitrary neighborhood two axles between be spaced from each other to form between centers gap, described many axles define corresponding multiple between centers gaps thus; With
For solar power being changed into the multiple separate solar panel of electric energy, solar panel described in each is arranged on described between centers gap location corresponding in described multiple between centers gap one, to cover corresponding described between centers gap.
Further, solar panel described in each is connected in described many axles and is formed on two adjacent shafts in gap between described respective shaft, and keeps described solar panel by described two adjacent shafts.
Further, each axle in described two adjacent shafts has the first connection structure extended along its length respectively, and each side of described solar panel has the second connection structure respectively; One in described first connection structure and described second connection structure is guide groove, and another in described first connection structure and described second connection structure is the guide rail that can slide along described guide groove.
Further, described guide groove and described guide rail are arranged so that described solar panel can be inserted between described two adjacent shafts along towards described fuselage main direction in the position away from described fuselage main body.
Further, described solar panel has the first electrical connector towards described fuselage main body, described fuselage main body is provided with the second electrical connector for receiving described first electrical connector, the position of described first electrical connector and described second electrical connector and shape are arranged in described solar panel and are inserted into after between described two adjacent shafts, and described first electrical connector and described second electrical connector form electrical contact.
Further, each the between centers gap location in described multiple between centers gap is equipped with a described solar panel.
Further, described many axles are spacedly distributed along the circumference of described fuselage main body, thus form the identical described multiple between centers gaps of shape; Further, described multiple solar panel is of similar shape and structure.
Further, the quantity of described many axles is at least 4.
According to another aspect of the present utility model, another kind of multiaxis unmanned vehicle is provided, comprises:
Fuselage main body;
From described fuselage main body transversely outward extending many axles, in described many axles arbitrary neighborhood two axles between be spaced from each other to form between centers gap, described many axles define corresponding multiple described between centers gap thus;
For solar power being changed into the single solar panel of electric energy, described solar panel at least covers described multiple between centers gap.
Further, described solar panel also covers the top of described fuselage main body.
Solar panel of the present utility model can be installed on multiaxis unmanned vehicle, and solar panel can provide electric energy for multiaxis unmanned vehicle, adds the hang time of multiaxis unmanned vehicle.
It is especially noted that solar panel of the present utility model is arranged between centers gap location, make use of the idle space of multiaxis unmanned vehicle.
In addition, in the situations such as cloudy day, because now solar panel generating is little, in fact solar panel adds the weight load of multiaxis unmanned vehicle.In the utility model, solar panel is the demountable structure of guide groove and guide rail, install and the dismounting when sunlight is not enough when sunny, when decreasing the cloudy day, the weight load of multiaxis unmanned vehicle, improves the hang time of multiaxis unmanned vehicle further.
According to an embodiment of the present utility model, one of guide groove and guide rail is fixedly connected on the lateral surface of solar panel, and another is such as removably arranged on the medial surface of axle by mode that is bonding or bolt screw.When being dismantled from multiaxis unmanned vehicle by solar panel, can removably be arranged in guide groove on the medial surface of axle by being connected in passing or guide rail takes off.For the multiaxis unmanned vehicle produced, by arranging fixing connection structure on multiaxis unmanned vehicle, the change to multiaxis unmanned vehicle structure need not be decreased, thus again need not carry out die sinking production.
According to hereafter by reference to the accompanying drawings to the detailed description of the utility model specific embodiment, those skilled in the art will understand above-mentioned and other objects, advantage and feature of the present utility model more.
Accompanying drawing explanation
Hereinafter describe specific embodiments more of the present utility model with reference to the accompanying drawings by way of example, and not by way of limitation in detail.Reference numeral identical in accompanying drawing denotes same or similar parts or part.It should be appreciated by those skilled in the art that these accompanying drawings may not be drawn in proportion.In accompanying drawing:
Fig. 1 is the structural representation being provided with the multiaxis unmanned vehicle of solar panel of the utility model embodiment;
Fig. 2 is the structural representation not being provided with the multiaxis unmanned vehicle of solar panel shown in Fig. 1;
Fig. 3 is the structural representation of the solar panel shown in Fig. 1;
Fig. 4 is the structural representation being provided with the multiaxis unmanned vehicle of solar panel of another embodiment of the utility model;
Fig. 5 is the structural representation of solar panel in Fig. 4.
Reference numeral in figure is as follows:
10-solar panel, 11-between centers gap, 11b-plate body upper surface, 11d-neighboring area, 11e-central region, 12-guide groove, 13-guide rail, 14-first electrical connector;
20-multiaxis unmanned vehicle, 21-axle, 22-fuselage roof, 23-rotor, 24-second electrical connector.
Detailed description of the invention
Multiaxis unmanned vehicle 20 of the present utility model, comprises fuselage main body, axle, solar panel 10.Wherein: fuselage main body, there is fuselage roof 22.Axle 21 transversely stretches out from described fuselage main body, and quantity is generally even number, is chosen as 4 in one embodiment, is chosen as the six roots of sensation in the embodiment shown in fig. 1.As shown in Figure 1, the multiaxis unmanned vehicle 20 that the utility model relates to comprises six axles 21 and is positioned at the fuselage at middle part, and fuselage has fuselage roof 22, and one end of each axle 21 has a rotor 23.Multiaxis unmanned vehicle entirety of the present utility model becomes symmetrical structure.In described many axles arbitrary neighborhood two axles between be spaced from each other to form between centers gap 11, described many axles define corresponding multiple between centers gaps 11 thus, have six between centers gaps 11 in fig. 2.Solar power is changed into electric energy by solar panel 10, and solar panel 10 has the plate body upper surface 11b for receiving solar irradiation.Each solar panel 10 is arranged on described between centers gap 11 place corresponding in multiple between centers gap 11 one, to cover corresponding between centers gap 11.That is, each between centers gap 11 all can arrange a solar panel 10, but such as in the situations such as cloudy day, solar panel 10 can be dismantled, the weight load of multiaxis unmanned vehicle 20 when decreasing the cloudy day.Or, such as when sunlight is comparatively sufficient, four solar panels 10 also can be set on the multiaxis unmanned vehicle 20 of Fig. 2 to meet the continuation of the journey requirement of unmanned vehicle 20, compared to installation six solar panels 10, this kind arranges the weight that can reduce unmanned vehicle 20, adds the hang time of multiaxis unmanned vehicle 20.And when sunlight is not enough, a described solar panel 10 can be equipped with by each the between centers gap location in multiple between centers gap, improves the electricity supply of solar panel 10.
For how solar panel 10 being maintained, the utility model provides following technical scheme: solar panel 10 described in each is connected in described many axles and is formed on two adjacent shafts in gap between described respective shaft, and keep described solar panel 10 by described two adjacent shafts, when connecting, solar panel 10 is held in plate body upper surface 11b and can receives solar irradiation by two adjacent shafts.That is, by adjacent shaft, corresponding solar panel 10 is connected, prevent solar panel 10 to the interference in space belonging to other axle and other axle.The utility model also provides a kind of holding structure: each axle in described two adjacent shafts has the first connection structure extended along its length respectively, and each side of described solar panel 10 has the second connection structure respectively; One in described first connection structure and described second connection structure is guide groove 12, and another in described first connection structure and described second connection structure is the guide rail 13 that can slide along described guide groove 12.In Fig. 1-embodiment illustrated in fig. 3, with a between centers gap 11 for benchmark, guide groove 12 is arranged on the medial surface of axle 21, guide rail 13 is arranged on the lateral surface of solar panel 10, described guide groove 12 and described guide rail 13 are arranged so that described solar panel 10 can be inserted between described two adjacent shafts along towards described fuselage main direction in the position away from described fuselage main body, and along away from described fuselage main direction, described guide groove 12 and described guide rail 13 are departed from.
As shown in Figure 3, described solar panel 10 has towards the first electrical connector 14 of described fuselage main body.As shown in Figure 2, described fuselage main body is provided with the second electrical connector 24 for receiving described first electrical connector 14, the position of described first electrical connector 14 and described second electrical connector 24 and shape are arranged in described solar panel 10 and are inserted into after between described two adjacent shafts, and described first electrical connector 14 forms electrical contact with described second electrical connector 24.Such as, interface arrangment is formed when solar panel 10 is inserted into the first electrical connector 14 after between described two adjacent shafts with described second electrical connector 24.
In an embodiment of the present utility model, described many axles are spacedly distributed along the circumference of described fuselage main body, thus form the identical described multiple between centers gaps 11 of shape; Further, described multiple solar panel 10 is of similar shape and structure.Such structure can facilitate solar panel 10 mixed insertion between centers gap 11.
Fig. 4 provides another multiaxis unmanned vehicle 20, and multiaxis unmanned vehicle 20 similarly comprises:
Fuselage main body, has the plate body upper surface 11b for receiving solar irradiation; .
From described fuselage main body transversely outward extending many axles, in described many axles arbitrary neighborhood two axles between be spaced from each other to form between centers gap 11, described many axles define corresponding multiple described between centers gap 11 thus.
For solar power being changed into the single solar panel 10 of electric energy, described solar panel 10 at least covers described multiple between centers gap 11.
More known by Fig. 1 and Fig. 4, in Fig. 1, solar panel 10 is arranged between centers gap 11, and the solar panel 10 in Fig. 4 is an integral structure, is arranged on the top of axle 21 and is connected with the upper surface of axle 21.When connecting, solar panel 10 is held in plate body upper surface 11b and can receives solar irradiation by each axle 21.With Fig. 1-embodiment illustrated in fig. 3 identical, solar panel 10 can provide electric energy for multiaxis unmanned vehicle 20, adds the hang time of multiaxis unmanned vehicle 20.
Solar panel 10 shown in Fig. 5 has neighboring area 11d and central region 11e, central region 11e has projection upwards, the interior shape of this projection and the outer shape of fuselage roof 22 similar, fuselage roof 22 can be covered to make this projection, fuselage size due to a lot of unmanned plane is limited and not smooth, therefore this layout can improve Solar use efficiency.Now, can solar panel 10 be fastened on multiaxis unmanned vehicle 20 choice for use bolt.When running into the cloudy day, solar panel 10 can be taken off from multiaxis unmanned vehicle 20 by this disassembling bolts.
In the same manner, the edge of the solar panel 10 in Fig. 3 and Fig. 5 embodiment is arc-shaped substantially, is fan-shaped in figure 3, is UFO-like in Figure 5, and the solar panel 10 in multiple Fig. 3 substantially can other parts in composition diagram 5 except projection.
So far, those skilled in the art will recognize that, although multiple exemplary embodiment of the present utility model is illustrate and described herein detailed, but, when not departing from the utility model spirit and scope, still can directly determine or derive other modification many or amendment of meeting the utility model principle according to content disclosed in the utility model.Therefore, scope of the present utility model should be understood and regard as and cover all these other modification or amendments.
Claims (10)
1. a multiaxis unmanned vehicle, is characterized in that, comprising:
Fuselage main body;
From described fuselage main body transversely outward extending many axles, in described many axles arbitrary neighborhood two axles between be spaced from each other to form between centers gap, described many axles define corresponding multiple between centers gaps thus; With
For solar power being changed into the multiple separate solar panel of electric energy, solar panel described in each is arranged on described between centers gap location corresponding in described multiple between centers gap one, to cover corresponding described between centers gap.
2. multiaxis unmanned vehicle according to claim 1, it is characterized in that, solar panel described in each is connected in described many axles and is formed on two adjacent shafts in gap between described respective shaft, and keeps described solar panel by described two adjacent shafts.
3. multiaxis unmanned vehicle according to claim 2, is characterized in that, each axle in described two adjacent shafts has the first connection structure extended along its length respectively, and each side of described solar panel has the second connection structure respectively; One in described first connection structure and described second connection structure is guide groove, and another in described first connection structure and described second connection structure is the guide rail that can slide along described guide groove.
4. multiaxis unmanned vehicle according to claim 3, it is characterized in that, described guide groove and described guide rail are arranged so that described solar panel can be inserted between described two adjacent shafts along towards described fuselage main direction in the position away from described fuselage main body.
5. multiaxis unmanned vehicle according to claim 4, it is characterized in that, described solar panel has the first electrical connector towards described fuselage main body, described fuselage main body is provided with the second electrical connector for receiving described first electrical connector, the position of described first electrical connector and described second electrical connector and shape are arranged in described solar panel and are inserted into after between described two adjacent shafts, and described first electrical connector and described second electrical connector form electrical contact.
6. multiaxis unmanned vehicle according to claim 1, is characterized in that, each the between centers gap location in described multiple between centers gap is equipped with a described solar panel.
7. multiaxis unmanned vehicle according to claim 1, is characterized in that, described many axles are spacedly distributed along the circumference of described fuselage main body, thus forms the identical described multiple between centers gaps of shape; Further, described multiple solar panel is of similar shape and structure.
8. multiaxis unmanned vehicle according to claim 1, is characterized in that, the quantity of described many axles is at least 4.
9. a multiaxis unmanned vehicle, is characterized in that, comprising:
Fuselage main body;
From described fuselage main body transversely outward extending many axles, in described many axles arbitrary neighborhood two axles between be spaced from each other to form between centers gap, described many axles define corresponding multiple described between centers gap thus;
For solar power being changed into the single solar panel of electric energy, described solar panel at least covers described multiple between centers gap.
10. multiaxis unmanned vehicle according to claim 9, is characterized in that, described solar panel also covers the top of described fuselage main body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520339906.6U CN204750575U (en) | 2015-05-22 | 2015-05-22 | Multiaxis unmanned vehicles |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520339906.6U CN204750575U (en) | 2015-05-22 | 2015-05-22 | Multiaxis unmanned vehicles |
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| CN204750575U true CN204750575U (en) | 2015-11-11 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201520339906.6U Active CN204750575U (en) | 2015-05-22 | 2015-05-22 | Multiaxis unmanned vehicles |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104908955A (en) * | 2015-05-22 | 2015-09-16 | 中国科学院物理研究所 | Multi-shaft unmanned aerial vehicle |
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2015
- 2015-05-22 CN CN201520339906.6U patent/CN204750575U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104908955A (en) * | 2015-05-22 | 2015-09-16 | 中国科学院物理研究所 | Multi-shaft unmanned aerial vehicle |
| CN104908955B (en) * | 2015-05-22 | 2017-04-12 | 中国科学院物理研究所 | Multi-shaft unmanned aerial vehicle |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |