CN104309801A - Rotary wing type unmanned plane with spherical solar collector at central section and landing seat thereof - Google Patents
Rotary wing type unmanned plane with spherical solar collector at central section and landing seat thereof Download PDFInfo
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- CN104309801A CN104309801A CN201410500652.1A CN201410500652A CN104309801A CN 104309801 A CN104309801 A CN 104309801A CN 201410500652 A CN201410500652 A CN 201410500652A CN 104309801 A CN104309801 A CN 104309801A
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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
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- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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Abstract
A rotary wing type unmanned plane with a spherical solar collector at the central section contains landing racks, supports, motors, rotor wings, connecting rings, an upper spherical shell, a lower spherical shell, a support plate, an electronic control module and a storage battery. The lower end of the upper spherical shell and the upper end of the lower spherical shell are both provided with a connecting ring respectively. The support plate is fixed between the upper spherical shell and the lower spherical shell. The electronic control module is arranged above the support plate. The storage battery is mounted below the support plate. One end of each support is embedded in an external neck of the connecting rings, and the other end of the support is provided with a motor. The central section of each rotor ring is fixed to a rotary shaft of the motor, and a landing rack is arranged below the central section of the support. According to the invention, the spherical solar collector is adopted at the central section, and the rotor rings of the unmanned plane are connected to the connecting rings outside the spherical solar collector through the supports. By the characteristic that the spherical solar collector can collect solar energy in all directions, solar energy collection efficiency and cruising ability of the unmanned plane are further enhanced. In addition, a corresponding landing seat is arranged so as to reasonably utilize electric energy collected by the solar collector.
Description
Technical field
The present invention relates to rotary wind type unmanned plane and landing seat field thereof, particularly relate to rotary wind type unmanned plane and landing seat thereof that a kind of middle part is spherical solar catcher.
Background technology
Along with the development in epoch, the continuous progress of science and technology, the development of unmanned plane is more and more rapider, the continuation of the journey of unmanned plane is very large on the impact of unmanned plane, unmanned plane directly can be subject to illumination awing, solar power is eco-friendly power source, unmanned plane awing charges by solar power, at present by increasing for unmanned plane field, traditional panel solar has with low cost, feature easy for installation, but want to continue to keep efficiency operation the moment must aim at solar direction, and this many resource of extra consumption again, spherical solar cells it makes use of spheroid and has the long-pending principle of maximized surface, light from all directions can be drawn, thus energy conversion efficiency is promoted nearly 20%, far exceed existing panel solar plate, spherical solar cells can also be installed on the position of needs with arbitrary dimension, greatly expand its application, have a extensive future, rotary wind type unmanned plane is due to can hovering, therefore be widely used in every field, its general Shi Yi center is that main body rotor is in its surrounding, therefore it can be combined with spherical solar catcher, if spherical solar catcher can be combined with unmanned plane greatly to improve the collecting effect of solar power.
Summary of the invention
For above problem, the present invention designs the rotary wind type unmanned plane and landing seat thereof that a kind of middle part is spherical solar catcher, spherical solar catcher is adopted in the middle part of it, unmanned plane rotor is connected by the coupling link of connection bracket with spherical solar catcher outside, utilize spherical solar catcher can the feature of comprehensive collection solar power, and then improve solar collection rate and unmanned plane flying power, and be provided with corresponding landing seat to carry out Appropriate application for the electric energy collected by solar collector, for reaching this object, the invention provides the rotary wind type unmanned plane that a kind of middle part is spherical solar catcher, comprise landing gear, support, motor, rotor, coupling link, upper spherical shell, lower spherical shell, stay bearing plate, electrically-controlled component and storage battery, described upper spherical shell and lower spherical shell are semisphere solar panel, all there is a circle coupling link described upper spherical shell lower end and lower spherical shell upper end, described stay bearing plate is fixed in the inner card cage between spherical shell and lower spherical shell, described electrically-controlled component is side on the supporting plate, described storage battery is below stay bearing plate, there is exterior bayonet slot in the outside of the coupling link of described upper spherical shell and lower spherical shell, described exterior bayonet slot angularly around coupling link center one week, described support one end is inserted in exterior bayonet slot, described upper spherical shell and lower spherical shell are fixed by attaching parts, the described support other end has motor, be fixed in the middle part of described rotor on machine shaft, landing gear is had below described mid-stent.
Improve further as rotary wind type unmanned plane of the present invention, the semisphere solar panel of described upper spherical shell and lower spherical shell is integral type semisphere solar panel or is spliced by spliced solar panel, when upper spherical shell and lower spherical shell are spliced by spliced solar panel, described upper spherical shell and lower spherical shell include solar panel supporting bracket and spliced solar panel, described spliced solar panel is inserted in the groove of corresponding solar panel supporting bracket, in the present invention, the solar panel of spherical shell and lower spherical shell can be integral type semisphere solar panel and also can be spliced by spliced solar panel, integral type semisphere solar panel is convenient easy for installation owing to producing, be suitable for middle-size and small-size rotary wind type unmanned plane, spliced solar panel is then more suitable for the manufacture of the spherical solar catcher of large-scale rotary wind type unmanned plane, in addition the installation of spliced solar panel is convenient to, generally by by spliced solar panel the mode be arranged in the groove of solar panel supporting bracket install, producer can select accordingly according to actual conditions in actual production.
Improve further as rotary wind type unmanned plane of the present invention, described spliced solar panel is curved plates or surface plate, the spliced solar panel that the present invention installs can adopt curved slab or surface plate, adopt surface plate convenient for production with low cost, but solar energy collecting efficiency is relatively low, although adopt curved slab manufacturing cost higher, collecting effect is also better, and producer can select according to actual needs accordingly.
Improve further as rotary wind type unmanned plane of the present invention, described coupling link is solar panel or high transparent glass, the outside coupling link of upper and lower hemispheres of the present invention can be solar panel, the solar power be irradiated on it can be collected like this, but tooling cost can be relatively high, the outside coupling link of upper and lower hemispheres also can adopt high transparent glass to make, its light transmittance is high, such sunshine can be irradiated to another hemisphere through coupling link, thus collect the most solar powers irradiated thereon, and tooling cost relative moderate.
Improve further as rotary wind type unmanned plane of the present invention, there is damping sucker described landing gear lower end, has damping sucker to land the impact brought to reduce unmanned plane bottom landing gear.
Improve further as rotary wind type unmanned plane of the present invention, have circular touch panel bottom described lower spherical shell, circular touch panel is set bottom lower spherical shell, also charge by external power supply after unmanned plane landing.
A kind of middle part of the present invention is the rotary wind type unmanned plane landing seat of spherical solar catcher, comprise landing seat main body, support sucker, link span, cover plate and circle touch face, there is the spherical groove corresponding with the bottom of the lower spherical shell of the spherical solar catcher of rotary wind type unmanned plane described landing seat main body upper surface, in described spherical groove, center has circular face of touching corresponding with the circular touch panel of the bottom of the lower spherical shell of the spherical solar catcher of corresponding rotary wind type unmanned plane, described support sucker is fixed on landing seat bottom part body by link span, described landing seat body height is greater than the height of the landing gear of corresponding rotary wind type unmanned plane, battery case is had in described landing seat main body, storage battery is placed with in described battery case, in described landing seat main body, all there is cover plate four sides of battery case.
Improve further as the present invention's seat that lands, described landing seat main body side has two signal lamps, USB interface, MiniUSB interface, indicator lamp and switch, described two signal lamps are accumulator electric-quantity situation in storage battery and unmanned plane in corresponding landing seat main body respectively, the land side of seat of the present invention arranges USB interface, can be used for charging to compact electric apparatus, the side of landing seat arranges MiniUSB interface and then can be used for connecing power supply and charge to storage battery in landing seat main body, charged to storage battery in unmanned plane by storage battery in landing seat main body again, the side of landing seat arranges switch, can be convenient to manually control the work of landing seat, the side of landing seat arranges two signal lamps and then can be respectively used to judge storage battery and accumulator electric-quantity situation in landing seat main body in unmanned plane, the side of landing seat arranges indicator lamp then for judging landing seat service condition.
Improve further as the present invention's seat that lands, spheric guiding shell is had in the spherical groove of described landing seat main body upper surface, because unmanned plane descent can rub with cell wall, after spheric guiding shell is set in spherical groove, if spheric guiding shell is damaged and can changes at any time, and because the size of the spherical solar catcher of unmanned plane is often different, spheric guiding shell by changing different size is suitable for dissimilar unmanned plane, in addition the impact considered unmanned plane landing wearing and tearing and impact spheric guiding shell, spheric guiding shell can adopt the plastics of nylon and polyolefin how rice melting to make, this material has rigidity and flexibility concurrently and Absorbable rod impacts, under normal circumstances, material can play rigidity and the intensity of nylon, if but when applying the anxious impact swashed, material can be out of shape and absorb impact as rubber.
Rotary wind type unmanned plane tool for spherical solar catcher in the middle part of the present invention has the following advantages:
1, spherical solar catcher is adopted in the middle part of this rotary wind type unmanned plane, spherical solar catcher is combined by upper and lower two hemisphere, upper and lower hemispheres all adopts solar panel to make, the sun can carry out solar energy collecting in any angle, solar energy acquisition rate is high, and then improves unmanned plane flying power.
2, circular touch panel is arranged at the bottom of lower spherical solar catcher, storage battery is coupled by connection lead, can charge to unmanned plane after being connected with the circle face of touching in landing seat groove when unmanned plane drops to circular touch panel after unmanned plane landing seat, also the solar power that excess energy unmanned plane can collected to the storage battery in landing seat to carry out charging to make to collect can carry out Appropriate application, reduces unnecessary waste.
If 3 in case of emergency, unmanned plane can not drop on unmanned plane landing seat, can on general level land, by landing gear and the landing of damping sucker, has damping sucker and then can reduce unmanned plane and land the impact brought bottom landing gear.
Rotary wind type unmanned plane landing seat tool for spherical solar catcher in the middle part of the present invention has the following advantages:
1, the present invention is landed bottom seat cavity, landing seat bottom cavity, there is cover plate cavity four side, storage battery is had in landing seat bottom cavity, the spherical groove corresponding with the bottom of lower spherical solar catcher is arranged at landing seat top, there is circular tactile face the center of spherical groove, because in the middle part of unmanned plane of the present invention, bottom is spherical, and the present invention is landed, a body height is greater than the height of the landing gear of corresponding rotary wind type unmanned plane, as long as therefore unmanned plane roughly lands and can fall on it voluntarily above spherical groove when landing, therefore greatly reduce landing difficulty.
2, circular touch panel is arranged at the bottom of lower spherical solar catcher, storage battery is coupled by connection lead, can charge to unmanned plane after circular touch panel after unmanned plane landing is connected with the circle face of touching in landing seat groove, also excess energy unmanned plane can collected charges to the storage battery in landing seat, to make the solar power collected that Appropriate application can be carried out, reduce unnecessary waste.
3, due to certain pressure can be produced to landing seat in the descent of unmanned plane, in order to reduce pressure, impact being produced to landing seat, the service life of impact landing seat, in the bottom of landing seat, sucker can be set to reduce corresponding impact.
4, in addition the present invention's main body side that lands has two signal lamps, USB interface, MiniUSB interface, indicator lamp and switch, described two signal lamps, USB interface, MiniUSB interface, indicator lamp, switch is connected by connection lead with control panel in landing seat main body, described two signal lamps are accumulator electric-quantity situation in storage battery and unmanned plane in corresponding landing seat main body respectively, the land side of seat of the present invention arranges USB interface, can be used for charging to compact electric apparatus, the side of landing seat arranges MiniUSB interface and then can be used for connecing power supply and charge to storage battery in landing seat main body, charged to storage battery in unmanned plane by storage battery in landing seat main body again, the side of landing seat arranges switch, can be convenient to manually control the work of landing seat, the side signalization lamp of landing seat then can be respectively used to judge storage battery and accumulator electric-quantity situation in landing seat main body in unmanned plane, the side of landing seat arranges indicator lamp then for judging landing seat service condition.
5, the impact considered unmanned plane landing wearing and tearing and impact spheric guiding shell, spheric guiding shell can adopt the plastics of nylon and polyolefin how rice melting to make, this material has rigidity and flexibility concurrently and Absorbable rod impacts, and under normal circumstances, material can play rigidity and the intensity of nylon; If but when applying the anxious impact swashed, material can be out of shape and absorb impact as rubber.
Accompanying drawing explanation
Fig. 1 is rotary wind type unmanned plane schematic diagram of the present invention;
Fig. 2 is spherical solar catcher inner structure schematic diagram of the present invention;
Fig. 3 is the present invention's another kind of spherical solar catcher partial side view;
Fig. 4 is that the present invention is landed a lateral plan;
Fig. 5 is unmanned plane of the present invention and landing seat schematic diagram;
Component in figure is:
1, landing gear; 2, damping sucker; 3, support;
4, motor; 5, rotor; 6, coupling link;
7, attaching parts; 8, upper spherical shell; 9, lower spherical shell;
10, circular touch panel; 11, exterior bayonet slot; 12, stay bearing plate;
13, electrically-controlled component; 14, storage battery; 15, solar panel supporting bracket;
16, spliced solar panel; 17, landing seat main body; 18, sucker is supported;
19, link span; 20, signal lamp; 21, USB interface;
22, MiniUSB interface; 23, indicator lamp; 24, switch;
25, cover plate; 26, spheric guiding shell; 27, circular tactile face.
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Detailed description of the invention
Below in conjunction with drawings and Examples, invention is described in detail:
The present invention designs the rotary wind type unmanned plane and landing seat thereof that a kind of middle part is spherical solar catcher, spherical solar catcher is adopted in the middle part of it, unmanned plane rotor is connected by the coupling link of connection bracket with spherical solar catcher outside, utilize spherical solar catcher can comprehensive collection solar power feature, and then improve solar collection rate and unmanned plane flying power, and be provided with corresponding landing seat to carry out Appropriate application for the electric energy collected by solar collector.
As a kind of embodiment of unmanned plane of the present invention, the invention provides the rotary wind type unmanned plane that a kind of middle part is spherical solar catcher, comprise landing gear 1, support 3, motor 4, rotor 5, coupling link 6, upper spherical shell 8, lower spherical shell 9, stay bearing plate 12, electrically-controlled component 13 and storage battery 14, described upper spherical shell 8 and lower spherical shell 9 are semisphere solar panel, all there is a circle coupling link 6 described upper spherical shell 8 lower end and lower spherical shell 9 upper end, described stay bearing plate 12 is fixed in the inner card cage between spherical shell 8 and lower spherical shell 9, described electrically-controlled component 13 is above stay bearing plate 12, described storage battery 14 is below stay bearing plate 12, there is exterior bayonet slot 11 in the outside of the coupling link 6 of described upper spherical shell 8 and lower spherical shell 9, described exterior bayonet slot 11 angularly around coupling link 6 center one week, described support 3 one end is inserted in exterior bayonet slot 11, described upper spherical shell 8 and lower spherical shell 9 are fixed by attaching parts 7, described support 3 other end has motor 4, be fixed in motor 4 rotating shaft in the middle part of described rotor 5, in the middle part of described support 3, there is landing gear 1 below.
As a kind of specific embodiment of unmanned plane of the present invention, the invention provides the rotary wind type unmanned plane that a kind of middle part is spherical solar catcher, comprise landing gear 1, support 3, motor 4, rotor 5, coupling link 6, upper spherical shell 8, lower spherical shell 9, stay bearing plate 12, electrically-controlled component 13 and storage battery 14, described upper spherical shell 8 and lower spherical shell 9 are semisphere solar panel, the semisphere solar panel of described upper spherical shell 8 and lower spherical shell 9 is spliced by spliced solar panel, described upper spherical shell 8 and lower spherical shell 9 include solar panel supporting bracket 15 and spliced solar panel 16 as shown in Figure 3, described spliced solar panel 16 is inserted in the groove of corresponding solar panel supporting bracket 15, in the present invention, the solar panel of spherical shell and lower spherical shell can be integral type semisphere solar panel and also can be spliced by spliced solar panel, integral type semisphere solar panel is convenient easy for installation owing to producing, be suitable for middle-size and small-size rotary wind type unmanned plane, spliced solar panel is then more suitable for the manufacture of the spherical solar catcher of large-scale rotary wind type unmanned plane, in addition the installation of spliced solar panel is convenient to, generally by by spliced solar panel the mode be arranged in the groove of solar panel supporting bracket install, producer can select accordingly according to actual conditions in actual production, described spliced solar panel 16 is curved slab or surface plate, the spliced solar panel that the present invention installs can adopt curved slab or surface plate, adopt surface plate convenient for production with low cost, but solar energy collecting efficiency is relatively low, although adopt curved slab manufacturing cost higher, but collecting effect is also better, producer can select according to actual needs accordingly, all there is a circle coupling link 6 described upper spherical shell 8 lower end and lower spherical shell 9 upper end, described coupling link 6 is solar panel, the outside coupling link of upper and lower hemispheres of the present invention can be solar panel, the solar power be irradiated on it can be collected like this, but tooling cost can be relatively high, the outside coupling link of upper and lower hemispheres also can adopt high transparent glass to make, its light transmittance is high, such sunshine can be irradiated to another hemisphere through coupling link, thus collect the most solar powers irradiated thereon, and tooling cost relative moderate, described stay bearing plate 12 is fixed in the inner card cage between spherical shell 8 and lower spherical shell 9, described electrically-controlled component 13 is above stay bearing plate 12, described storage battery 14 is below stay bearing plate 12, there is exterior bayonet slot 11 in the outside of the coupling link 6 of described upper spherical shell 8 and lower spherical shell 9, described exterior bayonet slot 11 angularly around coupling link 6 center one week, described support 3 one end is inserted in exterior bayonet slot 11, described upper spherical shell 8 and lower spherical shell 9 are fixed by attaching parts 7, described support 3 other end has motor 4, be fixed in motor 4 rotating shaft in the middle part of described rotor 5, in the middle part of described support 3, there is landing gear 1 below.
As the another kind of specific embodiment of unmanned plane of the present invention, the invention provides schematic diagram inner structure schematic diagram as shown in Figure 1, a kind of middle part is as shown in Figure 2 the rotary wind type unmanned plane of spherical solar catcher, comprise landing gear 1, support 3, motor 4, rotor 5, coupling link 6, upper spherical shell 8, lower spherical shell 9, stay bearing plate 12, electrically-controlled component 13 and storage battery 14, described upper spherical shell 8 and lower spherical shell 9 are semisphere solar panel, the semisphere solar panel of described upper spherical shell 8 and lower spherical shell 9 is integral type solar panel, in the present invention, the solar panel of spherical shell and lower spherical shell can be integral type semisphere solar panel and also can be spliced by spliced solar panel, integral type semisphere solar panel is convenient easy for installation owing to producing, be suitable for middle-size and small-size rotary wind type unmanned plane, spliced solar panel is then more suitable for the manufacture of the spherical solar catcher of large-scale rotary wind type unmanned plane, in addition the installation being convenient to spliced solar panel generally by by spliced solar panel the mode be arranged in the groove of solar panel supporting bracket install, producer can select accordingly according to actual conditions in actual production, all there is a circle coupling link 6 described upper spherical shell 8 lower end and lower spherical shell 9 upper end, described coupling link 6 is high transparent glass, the outside coupling link of upper and lower hemispheres of the present invention can be solar panel, the solar power be irradiated on it can be collected like this, but tooling cost can be relatively high, the outside coupling link of upper and lower hemispheres also can adopt high transparent glass to make, its light transmittance is high, such sunshine can be irradiated to another hemisphere through coupling link, thus collect the most solar powers irradiated thereon, and tooling cost relative moderate, described stay bearing plate 12 is fixed in the inner card cage between spherical shell 8 and lower spherical shell 9, described electrically-controlled component 13 is above stay bearing plate 12, described storage battery 14 is below stay bearing plate 12, there is exterior bayonet slot 11 in the outside of the coupling link 6 of described upper spherical shell 8 and lower spherical shell 9, described exterior bayonet slot 11 angularly around coupling link 6 center one week, described support 3 one end is inserted in exterior bayonet slot 11, described upper spherical shell 8 and lower spherical shell 9 are fixed by attaching parts 7, described support 3 other end has motor 4, be fixed in motor 4 rotating shaft in the middle part of described rotor 5, in the middle part of described support 3, there is landing gear 1 below, there is damping sucker 2 described landing gear 1 lower end, damping sucker is had to land the impact brought to reduce unmanned plane bottom landing gear, circular touch panel 10 is had bottom described lower spherical shell 8, bottom lower spherical shell, circular touch panel is set, also charge by external power supply after unmanned plane landing.
To land a kind of specific embodiment of seat as the present invention, the invention provides the rotary wind type unmanned plane landing seat that a kind of middle part is spherical solar catcher, comprise landing seat main body 17, support sucker 18, link span 19, cover plate 25 and circle touch face 27, there is the spherical groove corresponding with the bottom of the lower spherical shell 9 of the spherical solar catcher of rotary wind type unmanned plane described landing seat main body 17 upper surface, in described spherical groove, center has circular face 27 of touching corresponding with the circular touch panel 10 of the bottom of the lower spherical shell 9 of the spherical solar catcher of corresponding rotary wind type unmanned plane, described support sucker 18 is fixed on bottom landing seat main body 17 by link span 19, described landing seat main body 17 is highly greater than the height of the landing gear 1 of corresponding rotary wind type unmanned plane, battery case is had in described landing seat main body 17, storage battery is placed with in described battery case, in described landing seat main body 17, all there is cover plate 25 four sides of battery case.
To land a kind of best specific embodiment of seat as the present invention, a kind of middle part that the invention provides as shown in Figure 4 is the rotary wind type unmanned plane landing seat of spherical solar catcher, comprise landing seat main body 17, support sucker 18, link span 19, cover plate 25 and circle touch face 27, there is the spherical groove corresponding with the bottom of the lower spherical shell 9 of the spherical solar catcher of rotary wind type unmanned plane described landing seat main body 17 upper surface, spheric guiding shell 26 is had in the spherical groove of described landing seat main body 17 upper surface, because unmanned plane descent can rub with cell wall, if spherical guiding shell is damaged and can changes at any time after arranging spherical guiding shell in spherical groove, and because the size of the spherical solar catcher of unmanned plane is often different, spheric guiding shell by changing different size is suitable for dissimilar unmanned plane, in addition the impact considered unmanned plane landing wearing and tearing and impact spherical guiding shell, spherical guiding shell can adopt the plastics of nylon and polyolefin how rice melting to make, this material has rigidity and flexibility concurrently and Absorbable rod impacts, under normal circumstances, material can play rigidity and the intensity of nylon, if but when applying the anxious impact swashed, material can be out of shape and absorb impact as rubber, in described spherical groove, center has circular face 27 of touching corresponding with the circular touch panel 10 of the bottom of the lower spherical shell 9 of the spherical solar catcher of corresponding rotary wind type unmanned plane, described support sucker 18 is fixed on bottom landing seat main body 17 by link span 19, described landing seat main body 17 is highly greater than the height of the landing gear 1 of corresponding rotary wind type unmanned plane, battery case is had in described landing seat main body 17, storage battery is placed with in described battery case, in described landing seat main body 17, all there is cover plate 25 four sides of battery case, described landing seat main body 17 side has two signal lamps 20, USB interface 21, MiniUSB interface 22, indicator lamp 23 and switch 24, described two signal lamps 20 are storage battery 14 charge condition in storage battery and unmanned plane in corresponding landing seat main body 17 respectively, the land side of seat of the present invention arranges USB interface, can be used for charging to compact electric apparatus, the side of landing seat arranges MiniUSB interface and then can be used for connecing power supply and charge to storage battery in landing seat main body, charged to storage battery in unmanned plane by storage battery in landing seat main body again, the side of landing seat arranges switch, can be convenient to manually control the work of landing seat, the side of landing seat arranges two signal lamps and then can be respectively used to judge storage battery and accumulator electric-quantity situation in landing seat main body in unmanned plane, the side of landing seat arranges indicator lamp then for judging landing seat service condition.
Unmanned plane of the present invention can land as Fig. 5 formula mode, after unmanned plane landing, can be charged to storage battery in unmanned plane by storage battery and spherical solar catcher in landing seat, to meet its requirement of again taking off, if the storage battery of this unmanned plane is full of, spherical solar catcher can be charged to storage battery in landing seat, be used fully to make electric energy, and the seat side that lands is provided with multiple interfaces, can power to different electrical equipment.
The above is only preferred embodiment of the present invention, is not restriction the present invention being made to any other form, and any amendment done according to technical spirit of the present invention or equivalent variations, still belong to the present invention's scope required for protection.
Claims (10)
1. a middle part is the rotary wind type unmanned plane of spherical solar catcher, comprise landing gear (1), support (3), motor (4), rotor (5), coupling link (6), upper spherical shell (8), lower spherical shell (9), stay bearing plate (12), electrically-controlled component (13) and storage battery (14), it is characterized in that: described upper spherical shell (8) and lower spherical shell (9) are semisphere solar panel, all there is a circle coupling link (6) described upper spherical shell (8) lower end and lower spherical shell (9) upper end, described stay bearing plate (12) is fixed in the inner card cage between spherical shell (8) and lower spherical shell (9), described electrically-controlled component (13) is in stay bearing plate (12) top, described storage battery (14) is in stay bearing plate (12) below, there is exterior bayonet slot (11) in the outside of the coupling link (6) of described upper spherical shell (8) and lower spherical shell (9), described exterior bayonet slot (11) angularly around coupling link (6) center one week, described support (3) one end is inserted in exterior bayonet slot (11), described upper spherical shell (8) and lower spherical shell (9) are fixed by attaching parts (7), described support (3) other end has motor (4), described rotor (5) middle part is fixed in motor (4) rotating shaft, there is landing gear (1) below, described support (3) middle part.
2. a kind of middle part according to claim 1 is the rotary wind type unmanned plane of spherical solar catcher, it is characterized in that: the semisphere solar panel of described upper spherical shell (8) and lower spherical shell (9) is integral type solar panel or is spliced by spliced solar panel.
3. a kind of middle part according to claim 2 is the rotary wind type unmanned plane of spherical solar catcher, it is characterized in that: when upper spherical shell (8) and lower spherical shell (9) are spliced by spliced solar panel, described upper spherical shell (8) and lower spherical shell (9) include solar panel supporting bracket (15) and spliced solar panel (16), and described spliced solar panel (16) is inserted in the groove of corresponding solar panel supporting bracket (15).
4. a kind of middle part according to claim 3 is the rotary wind type unmanned plane of spherical solar catcher, it is characterized in that: described spliced solar panel (16) is curved slab or surface plate.
5. a kind of middle part according to claim 1 is the rotary wind type unmanned plane of spherical solar catcher, it is characterized in that: described coupling link (6) is solar panel or high transparent glass.
6. a kind of middle part according to claim 1 is the rotary wind type unmanned plane of spherical solar catcher, it is characterized in that: there is damping sucker (2) described landing gear (1) lower end.
7. a kind of middle part according to claim 1 is the rotary wind type unmanned plane of spherical solar catcher, it is characterized in that: circular touch panel (10) is arranged at described lower spherical shell (9) bottom.
8. a kind of middle part according to claim 1-7 is the rotary wind type unmanned plane landing seat of spherical solar catcher, comprise landing seat main body (17), support sucker (18), link span (19), cover plate (25) and circle touch face (27), it is characterized in that: there is the spherical groove corresponding with the bottom of the lower spherical shell (9) of the spherical solar catcher of rotary wind type unmanned plane described landing seat main body (17) upper surface, in described spherical groove, center has circular face (27) of touching corresponding with the circular touch panel (10) of the bottom of the lower spherical shell (9) of the spherical solar catcher of corresponding rotary wind type unmanned plane, described support sucker (18) is fixed on landing seat main body (17) bottom by link span (19), described landing seat main body (17) is highly greater than the height of the landing gear (1) of corresponding rotary wind type unmanned plane, battery case is had in described landing seat main body (17), storage battery is placed with in described battery case, all there is cover plate (25) four sides of the interior battery case of described landing seat main body (17).
9. a kind of middle part according to claim 8 is the rotary wind type unmanned plane landing seat of spherical solar catcher, it is characterized in that: described landing seat main body (17) side has two signal lamps (20), USB interface (21), MiniUSB interface (22), indicator lamp (23) and switch (24), storage battery (14) charge condition in described two signal lamps (20) difference corresponding land seat main body (17) interior storage battery and unmanned plane.
10. a kind of middle part according to claim 8 is the rotary wind type unmanned plane landing seat of spherical solar catcher, it is characterized in that: have spheric guiding shell (26) in the spherical groove of described landing seat main body (17) upper surface.
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| CN201410500652.1A CN104309801B (en) | 2014-09-26 | 2014-09-26 | A kind of middle part is rotary wind type unmanned plane and the landing seat thereof of spherical solar catcher |
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Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104753144A (en) * | 2015-04-19 | 2015-07-01 | 中南大学 | Rotor-wing unmanned aerial vehicle charging pile and charging method thereof |
| CN104908933A (en) * | 2015-05-14 | 2015-09-16 | 苏州绿农航空植保科技有限公司 | Protective cover of multi-rotor aircraft |
| CN104908955A (en) * | 2015-05-22 | 2015-09-16 | 中国科学院物理研究所 | Multi-shaft unmanned aerial vehicle |
| CN105083563A (en) * | 2015-07-31 | 2015-11-25 | 清华大学深圳研究生院 | Double-battery-powered aircraft and power supply control method thereof |
| CN105720649A (en) * | 2016-04-12 | 2016-06-29 | 张萍 | Internet of Things based intelligent searching and rescuing unmanned aerial vehicle |
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| CN105966594A (en) * | 2016-05-10 | 2016-09-28 | 傲飞创新科技（深圳）有限公司 | Unmanned aerial vehicle body structure, groove assisting positioning platform and landing positioning method of unmanned aerial vehicle |
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| CN106864763A (en) * | 2017-03-16 | 2017-06-20 | 山东大学 | It is a kind of to aid in being accurately positioned and fixing device for unmanned plane landing |
| CN107161345A (en) * | 2017-05-16 | 2017-09-15 | 吴李海 | A kind of full-automatic unmanned machine system of latent nest type |
| CN108045585A (en) * | 2017-11-21 | 2018-05-18 | 中国电子科技集团公司第四十八研究所 | The unmanned plane that can remotely charge supplies electric installation, UAV system and control method |
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| CN104753144A (en) * | 2015-04-19 | 2015-07-01 | 中南大学 | Rotor-wing unmanned aerial vehicle charging pile and charging method thereof |
| CN104908933A (en) * | 2015-05-14 | 2015-09-16 | 苏州绿农航空植保科技有限公司 | Protective cover of multi-rotor aircraft |
| 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 |
| CN105083563A (en) * | 2015-07-31 | 2015-11-25 | 清华大学深圳研究生院 | Double-battery-powered aircraft and power supply control method thereof |
| CN105882966B (en) * | 2016-03-30 | 2018-08-07 | 浙江聚楼信息科技有限公司 | A kind of novel unmanned plane based on Internet of Things |
| CN105882966A (en) * | 2016-03-30 | 2016-08-24 | 夏士桀 | Novel unmanned aerial vehicle based on internet of things |
| CN105720649A (en) * | 2016-04-12 | 2016-06-29 | 张萍 | Internet of Things based intelligent searching and rescuing unmanned aerial vehicle |
| CN105966594A (en) * | 2016-05-10 | 2016-09-28 | 傲飞创新科技（深圳）有限公司 | Unmanned aerial vehicle body structure, groove assisting positioning platform and landing positioning method of unmanned aerial vehicle |
| CN105966594B (en) * | 2016-05-10 | 2019-01-01 | 傲飞创新科技（深圳）有限公司 | Unmanned aerial vehicle body structure, groove auxiliary positioning platform and its landing localization method |
| CN106451722A (en) * | 2016-08-10 | 2017-02-22 | 深圳市昂佳科技有限公司 | Unmanned aerial vehicle battery management system and method |
| CN106081092A (en) * | 2016-08-26 | 2016-11-09 | 威海星煜无人机科技有限公司 | A kind of many rotor wing unmanned aerial vehicles |
| CN106864763A (en) * | 2017-03-16 | 2017-06-20 | 山东大学 | It is a kind of to aid in being accurately positioned and fixing device for unmanned plane landing |
| CN106864763B (en) * | 2017-03-16 | 2019-09-13 | 山东大学 | A kind of accurate positioning that auxiliary unmanned plane lands and fixed device |
| CN107161345A (en) * | 2017-05-16 | 2017-09-15 | 吴李海 | A kind of full-automatic unmanned machine system of latent nest type |
| CN107161345B (en) * | 2017-05-16 | 2023-09-12 | 深圳市阿拉丁无人机有限公司 | Bird nest type full-automatic unmanned aerial vehicle system of hiding |
| CN108045585A (en) * | 2017-11-21 | 2018-05-18 | 中国电子科技集团公司第四十八研究所 | The unmanned plane that can remotely charge supplies electric installation, UAV system and control method |
| WO2019206483A1 (en) * | 2018-04-24 | 2019-10-31 | Viafly Gmbh | Unmanned aircraft system and aircraft for an unmanned aircraft system and base station therefor |
| WO2019206400A1 (en) * | 2018-04-24 | 2019-10-31 | Viafly Gmbh | Unmanned aircraft system and aircraft for an unmanned aircraft system and base station therefor |
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