CN205396567U - Aircraft, cloud platform and sprinkler - Google Patents
Aircraft, cloud platform and sprinkler Download PDFInfo
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- CN205396567U CN205396567U CN201620144593.3U CN201620144593U CN205396567U CN 205396567 U CN205396567 U CN 205396567U CN 201620144593 U CN201620144593 U CN 201620144593U CN 205396567 U CN205396567 U CN 205396567U
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Abstract
The utility model relates to an aircraft specifically is an aircraft, cloud platform and sprinkler. The problem of present cloud platform can not full the angle and not have the technique of taking at the dead angle is solved. The utility model discloses a three support ring has formed a spherical shell structure, and it is a lot of that this kind of spherical shell structural design makes its flight adaptability improve, also can fly safely in the more spatial comparison of barrier little place, and consequently, novel to spray equipment very convenient as one kind. Especially use in the indoor epidemic prevention that waits under the environment, orientation and the position that can spray according to the image remote control of passback, present aircraft sprays disinfectant can only be used under the big environment in space, and to being accomplished by the people in narrow and small space, the danger that makes the people face like this strengthens. This application is then can overcome above -mentioned problem.
Description
Technical field
This utility model relates to aircraft, is specially a kind of aircraft, The Cloud Terrace and sprinkler.
Background technology
Existing The Cloud Terrace is aloft shot by UAV flight, this The Cloud Terrace can move around own level, roll and pitch axis, this motion mode cause The Cloud Terrace cannot to below or top shoot so that panorama information is complete, limits the practical application of The Cloud Terrace.Therefore be highly desirable to exploitation a kind of can full angle realize target shooting Novel tripod head and relevant aircraft.
Summary of the invention
This utility model be solve current The Cloud Terrace can not the technical problem that shoot without dead angle of full angle, it is provided that one aircraft, The Cloud Terrace and sprinkler.
Full angle aircraft described in the utility model realizes by the following technical solutions: a kind of aircraft, including the vertically taking off and landing flyer setting flight controller in, the fuselage left and right sides of vertically taking off and landing flyer extend horizontally away pair of support rods, and the top rotational support of pair of right and left support bar has first pushing out ring；Described first pushing out ring can rotate with two, left and right support bar for axle, has at least the top of a support bar to be rotationally connected by first conducting slip ring and first pushing out ring；First pushing out ring is driven by the first conducting slip ring and realizes rotating；The position being connected with two support bars on first pushing out ring is as two quadrantal points of this ring, and on first pushing out ring, on outside ring wall corresponding to two other quadrantal points, rotational support has second pushing out ring；Described second pushing out ring can rotate with its two intercardinal lines being connected with first pushing out ring for axle；Two junction points of described first pushing out ring and second pushing out ring have at least one realize being rotationally connected by second conducting slip ring；Second pushing out ring is driven by the second conducting slip ring and realizes rotating；Two positions being connected with first pushing out ring on second pushing out ring are as two quadrantal points of second pushing out ring, on second pushing out ring, on outside ring wall corresponding to two other quadrantal points, rotational support has three-support ring, has at least one to realize being rotationally connected by the 3rd conducting slip ring in two junction points of described second pushing out ring and three-support ring；Described three-support ring can rotate with two intercardinal lines that itself and second pushing out ring connect for axle；Three-support ring is driven by the 3rd conducting slip ring and realizes rotating；The internal diameter of described first pushing out ring, second pushing out ring and three-support ring is all higher than the maximum height of vertically taking off and landing flyer；Vertically taking off and landing flyer is powered to each conducting slip ring by airborne power supply.
Vertically taking off and landing flyer is as the power resources of aircraft described in the utility model, and its structure can have multiple choices.The rotating shaft of first pushing out ring, the rotating shaft of second pushing out ring and the rotating shaft of the 3rd support axle are mutually perpendicular to, three support axle and rotate on three degree of freedom, ensure that being positioned at outermost 3rd support axle realizes the full angle rotation without dead angle, thus can by relevant apparatus as imaged the first-class outer surface being arranged on three-support ring, photographic head just can turn to all of angle (including the bottom of aircraft), it is ensured that the effect of shooting.
The Cloud Terrace described in the utility model adopts the following technical scheme that realization: a kind of The Cloud Terrace, and the outer wall of described three-support ring is installed with a photographic head；The signal output part of described photographic head is by being fixed on wire and the electrical connection of the 3rd conducting slip ring of three-support ring ring wall or inside, and then is realized by the second conducting slip ring, the first conducting slip ring and set the communication of flight controller in vertically taking off and landing flyer.
Sprinkler described in the utility model adopts the following technical scheme that realization: a kind of sprinkler, vertically taking off and landing flyer is loaded with hermetic container；Connected by the first conducting slip ring between only one of which support bar and first pushing out ring, be rotationally connected by the first swivel joint between another support bar and first pushing out ring；Having a junction point to adopt the second conducting slip ring to connect between first pushing out ring and second pushing out ring, another junction point adopts the second swivel joint to be rotationally connected；Second has a junction point to adopt the 3rd conducting slip ring to connect between pushing out ring and three-support ring, another junction point adopts the 3rd swivel joint to be rotationally connected；First, second, third swivel joint has identical structure；Described swivel joint include one in the joint stator of through structure and rotation be nested in the joint rotor in through structure of joint stator interior；The front end of joint stator is stretched out in the front end of described joint rotor；It is provided with sealing member between joint stator and joint rotor；Another support bar described is hollow structure and top is provided with opening, and first, second, third pushing out ring all has the hole matched with corresponding swivel joint；Described three swivel joints both pass through corresponding hole and arrange；The joint stator of described first swivel joint is fixing with the top end opening of another support bar to be connected；The front end of the joint rotor of the first swivel joint is fixing with first pushing out ring to be connected；The joint stator of described second swivel joint and the fixing connection of another junction point of first pushing out ring, the joint rotor of described second swivel joint and the fixing connection of another junction point of second pushing out ring；The joint stator of described 3rd swivel joint and the fixing connection of another junction point of second pushing out ring, the joint rotor of described 3rd swivel joint and the fixing connection of another junction point of three-support ring；Another support bar described is connected with hermetic container；Joint rotor one side opening of the first swivel joint passes through the opening in communication of the joint stator side of conduit and the second swivel joint being fixed on first pushing out ring, the opening of the joint rotor side of the second swivel joint passes through the joint stator side open communication of conduit and the 3rd swivel joint being fixed on second pushing out ring, and joint rotor one side opening of the 3rd swivel joint is connected to one by conduit and is fixed on the shower nozzle on three-support ring outer wall.
Further, the outer wall of described three-support ring is fixedly provided with a photographic head being positioned at above shower nozzle；The signal output part of described photographic head is by being fixed on wire and the electrical connection of the 3rd conducting slip ring of three-support ring ring wall or inside, and then is realized by the second conducting slip ring, the first conducting slip ring and set the communication of flight controller in vertically taking off and landing flyer.
The structure of swivel joint is able to ensure that fluid proper flow；For the second swivel joint (Fig. 3), the medicine of sprinkling is delivered to the second swivel joint by the conduit on first pushing out ring, fluid flows out through the inside of the second swivel joint hollow, and it is flow to the conduit on second pushing out ring by the outlet of joint rotor, until the 3rd swivel joint, such fluid is just delivered to the shower nozzle below photographic head step by step and sprays；Hermetic container is provided with intelligent valve, to control the flow of fluid.
Advantageous Effects of the present utility model:
1. it is truly realized the full angle unobstructed shooting visual field openr；
2. just can be rapidly completed the current panorama shooting method of pan-shot with a photographic head adopts multiple phase unit to complete shooting mostly, so causes panorama shooting device heavy, and inconvenient to carry, cost is high；And The Cloud Terrace described herein adopts a camera just passable, complete to shoot the image of all directions by the control specific angle of cloud platform rotation during shooting, thus alleviate weight of equipment and reduce cost；As rescue robot, it is possible to pass full-view image in real time back, it is simple to commanding checks；
3. fuselage spherical housing may also operate as protective effect aircraft and surprisingly falls and make the power set of inside also in level by the adjustment effect of cardo ring (three pushing out ring), thus can also normally take off；When shell can also avoid flight, propeller is hurted sb.'s feelings；
4. simultaneously or the spray appliance of a kind of flight: (1) can be applied in the pesticide spraying (2) in the more farmland of the barriers such as sylvan life crop as the indoor disinfectant spray appliance such as plant, epidemic-stricken area as plant protection unmanned plane.
Three support ring and define a spherical shell structure.The spherical shell design of aircraft makes its flight acclimatization ability improve a lot, in the place that the more space of barrier is smaller can also safe flight, very convenient accordingly, as a kind of novel spray equipment.Particularly the epidemic prevention under the environment such as indoor uses, and existing aircraft spray disinfectant agent can only use under the environment that space is big, can only be completed by people for small space, so makes the dangerous enhancing that people faces.The application then can overcome the problems referred to above.
The application achieves the full angle rotation without dead angle by unique structural design, thus can carry relevant device and carry out operation；Whole apparatus structure is exquisite, and volume is light and handy, gathers around and has broad application prospects.
Accompanying drawing explanation
The structural representation of Fig. 1 aircraft described in the utility model and The Cloud Terrace.
Fig. 2 conducting slip ring is applied to the attachment structure schematic diagram (sectional view) when connecting.
Fig. 3 swivel joint is applied to the attachment structure schematic diagram (sectional view) when connecting.
The perspective view of Fig. 4 conducting slip ring.
The rotor structure schematic diagram of Fig. 5 conducting slip ring.
The cross-sectional view of Fig. 6 conducting slip ring.
The side-looking structural representation of Fig. 7 conducting slip ring.
The structural representation of Fig. 8 sprinkler described in the utility model.
1-vertically taking off and landing flyer, 2-support bar, first pushing out ring of 3-, 4-the first conducting slip ring, second pushing out ring of 5-, 6-the second conducting slip ring, 7-three-support ring, 8-the 3rd conducting slip ring, 9-slip-ring rotor, 10-slip ring stator, 11-inertia measuring module, 12-aileron, 13-coil, 14-magnetic pole, 15-connection jaws, 16-photographic head, 17-the first swivel joint, 18-the second swivel joint, 19-the 3rd swivel joint, 20-joint stator, 21-joint rotor, 22-shower nozzle, 23-guard, 24-sliding ring part, 25-motor part.
Detailed description of the invention
A kind of aircraft, including the vertically taking off and landing flyer 1 setting flight controller in, the fuselage left and right sides of vertically taking off and landing flyer 1 extend horizontally away pair of support rods 2, and the top rotational support of pair of right and left support bar 2 has first pushing out ring 3；Described first pushing out ring 3 can rotate with two, left and right support bar 2 for axle, has at least the top of a support bar 2 to be rotationally connected by first conducting slip ring 4 and first pushing out ring 3；First pushing out ring 3 is driven realization to rotate by the first conducting slip ring 4；The position being connected with two support bars 2 on first pushing out ring 3 is as two quadrantal points of this ring, and on first pushing out ring 3, on outside ring wall corresponding to two other quadrantal points, rotational support has second pushing out ring 5；Described second pushing out ring 5 can rotate with its two intercardinal lines being connected with first pushing out ring 3 for axle；Two junction points of described first pushing out ring 3 and second pushing out ring 5 have at least one realize being rotationally connected by second conducting slip ring 6；Second pushing out ring 5 is driven realization to rotate by the second conducting slip ring 6；Two positions being connected with first pushing out ring 3 on second pushing out ring 5 are as two quadrantal points of second pushing out ring 5, on second pushing out ring 5, on outside ring wall corresponding to two other quadrantal points, rotational support has three-support ring 7, has at least one to realize being rotationally connected by the 3rd conducting slip ring 8 in two junction points of described second pushing out ring 5 and three-support ring 7；Described three-support ring 7 can rotate with two intercardinal lines that itself and second pushing out ring 5 connect for axle；Three-support ring 7 is driven realization to rotate by the 3rd conducting slip ring 8；The internal diameter of 3, second pushing out ring 5 of described first pushing out ring and three-support ring 7 is all higher than the maximum height of vertically taking off and landing flyer 1；Vertically taking off and landing flyer 1 is powered to each conducting slip ring by airborne power supply.
Described first conducting slip ring the 4, second conducting slip ring the 6, the 3rd conducting slip ring 8 has identical structure；Described conducting slip ring includes slip-ring rotor 9 and is set in the slip ring stator 10 of the outer border of slip-ring rotor 9；Realize electrically connecting by conduction carbon brush between slip ring stator 10 with slip-ring rotor 9；The slip ring stator 10 of the first conducting slip ring 4 is fixing with the top of support bar 2 to be connected, and the slip-ring rotor 9 of the first conducting slip ring 4 is fixing with first pushing out ring 3 to be connected；Described power supply electrically connects by being located at support bar 2 inside or the wire on surface and the slip ring stator 10 of the first conducting slip ring 4；The slip-ring rotor 9 of described second conducting slip ring 6 is fixing with second pushing out ring 5 to be connected, the slip ring stator 10 of the second conducting slip ring 6 is fixing with first pushing out ring 3 to be connected, and the slip-ring rotor 9 of the first conducting slip ring 4 passes through to be located at the slip ring stator 10 of wire and the second conducting slip ring 6 inside first pushing out ring 3 or on ring wall and electrically connects；The slip-ring rotor 9 of described 3rd conducting slip ring 8 is fixing with three-support ring 7 to be connected, the slip ring stator 10 of the 3rd conducting slip ring 8 is fixing with second pushing out ring 5 to be connected, and the slip-ring rotor 9 of the second conducting slip ring 6 passes through to be located at the slip ring stator 10 of wire and the 3rd conducting slip ring 8 inside second pushing out ring 5 or on ring wall and electrically connects.
The internal ring wall of first, second, third pushing out ring is respectively provided with an inertia measuring module 11 in the position near each self-corresponding conducting slip ring；Described inertia measuring module 11 realizes and the communication of the internal flight controller of vertically taking off and landing flyer 1 by being located at internal or outer surface and each pushing out ring ring wall or inside the wire of support bar 2.
Described vertically taking off and landing flyer 1 adopts single rotor No Tail Rotor structure, and the fuselage left and right sides is respectively provided with an aileron 12 being positioned at the position below pair of support rods.
Support bar and first pushing out ring, first pushing out ring and second pushing out ring, second realize being rotationally connected each through at least one conducting slip ring between pushing out ring and three-support ring, and the power of rotation be provided.Conducting slip ring realizes the rotation of rotor in the energized state, this makes it possible to drive first pushing out ring, second pushing out ring, the separate rotation of three-support ring.
Wire is connected to three-support ring through first pushing out ring, second pushing out ring, achieve (at least) three connections propping up pushing out rings and power supply, just can be realized the rotation control of three, aircraft pushing out ring and the control to aircraft entirety flight path by the flight controller communication set in remote control device and vertically taking off and landing flyer.
Inertia measuring module can measure the rotational angle of each pushing out ring in real time, and then rotation information is fed back to flight controller, is controlled according to practical situation for operator, or realizes automatically controlling according to pre-set flight control program.
Single rotor No Tail Rotor simple in construction, it is simple to manipulation；Aileron is for controlling the flight attitude of vertically taking off and landing flyer.
Realize electrically connecting by conduction carbon brush between outer wall and the inwall of slip ring stator 10 first half of slip-ring rotor 9 first half of described conducting slip ring；Having interval, slip-ring rotor 9 latter half border to be provided with coil between latter half and slip ring stator 10 latter half of slip-ring rotor 9, slip ring stator 10 latter half inwall border is provided with magnetic pole 14；Slip-ring rotor 9 leads to the connection jaws 15 for being connected wire respectively with slip ring stator 10.As shown in Figure 6, the first half of conducting slip ring is sliding ring part, and latter half is for providing the motor part of power.
Three-support ring 7 external stability is covered with guard 23.Guard 23 is used for protecting aerial small items and clashes into aircraft, it is ensured that the safety of fuselage and Ge Zhi pushing out ring.
A kind of The Cloud Terrace, 7 outer walls of described three-support ring are installed with a photographic head 16；The signal output part of described photographic head 16 is electrically connected by the wire and the 3rd conducting slip ring 8 being fixed on three-support ring 7 ring wall or inside, and then is realized by second conducting slip ring the 6, first conducting slip ring 4 and set the communication of flight controller in vertically taking off and landing flyer 1.
A kind of sprinkler, vertically taking off and landing flyer 1 is loaded with hermetic container；It is connected by the first conducting slip ring 4 between only one of which support bar 2 with first pushing out ring 3, is rotationally connected by the first swivel joint 17 between another support bar 2 and first pushing out ring 3；Having a junction point to adopt the second conducting slip ring 6 to be connected between first pushing out ring 3 and second pushing out ring 5, another junction point adopts the second swivel joint 18 to be rotationally connected；Having a junction point to adopt the 3rd conducting slip ring 8 to be connected between second pushing out ring 5 and three-support ring 7, another junction point adopts the 3rd swivel joint 19 to be rotationally connected；First, second, third swivel joint has identical structure；Described swivel joint include one in through structure joint stator 20 and rotate be nested in joint stator 20 within be through structure joint rotor 21；The front end of joint stator 20 is stretched out in the front end of described joint rotor 21；It is provided with sealing member between joint stator 20 and joint rotor 21；Another support bar 2 described is provided with opening for hollow structure and top, and first, second, third pushing out ring all has the hole matched with corresponding swivel joint；Described three swivel joints both pass through corresponding hole and arrange；The joint stator 20 of described first swivel joint 17 is fixing with the top end opening of another support bar 2 to be connected；The front end of the joint rotor 21 of the first swivel joint 17 is fixing with first pushing out ring 3 to be connected；The joint stator 20 of described second swivel joint 18 is fixing with another junction point of first pushing out ring 3 to be connected, and the joint rotor 21 of described second swivel joint 18 is fixing with another junction point of second pushing out ring 5 to be connected；The joint stator 20 of described 3rd swivel joint 19 is fixing with another junction point of second pushing out ring 5 to be connected, and the joint rotor 21 of described 3rd swivel joint 19 is fixing with another junction point of three-support ring 7 to be connected；Another support bar 2 described is connected with hermetic container；Joint rotor 21 1 side opening of the first swivel joint 17 passes through the opening in communication of joint stator 20 side of conduit and the second swivel joint 18 being fixed on first pushing out ring 3, the opening of joint rotor 21 side of the second swivel joint 18 passes through the joint stator 20 side open communication of conduit and the 3rd swivel joint 19 being fixed on second pushing out ring 5, and joint rotor 21 1 side opening of the 3rd swivel joint 19 is connected to a shower nozzle 22 being fixed on three-support ring 7 outer wall by conduit；The outer wall of described three-support ring 7 is fixedly provided with a photographic head being positioned at above shower nozzle 22 16；The signal output part of described photographic head 16 is electrically connected by the wire and the 3rd conducting slip ring 8 being fixed on three-support ring 7 ring wall or inside, and then is realized by second conducting slip ring the 6, first conducting slip ring 4 and set the communication of flight controller in vertically taking off and landing flyer 1.
As it is shown on figure 3, arrow points is the flow direction of fluid, fluid supports circulation to second pushing out ring through the swivel joint of hollow from first, and conduit seals the two ends being connected on swivel joint.Joint stator is stretched out in the joint rotor front end of swivel joint, and namely the opening of this side of joint rotor stretches out the opening of formation joint rotor side for being connected with conduit；And joint stator stretches out (rear end beyond joint rotor) in rear end, form the opening of joint stator side for being connected with conduit；Joint rotor is nested in the groove set by joint stator inner wall, it is possible to flexible rotating, and sealing member guarantees to seal.
Claims (9)
1. an aircraft, it is characterized in that, including the vertically taking off and landing flyer (1) setting flight controller in, the fuselage left and right sides of vertically taking off and landing flyer (1) extend horizontally away pair of support rods (2), and the top rotational support of pair of right and left support bar (2) has first pushing out ring (3)；Described first pushing out ring (3) can rotate with two, left and right support bar (2) for axle, has at least the top of a support bar (2) to be rotationally connected by first conducting slip ring (4) and first pushing out ring (3)；First pushing out ring (3) is driven by the first conducting slip ring (4) and realizes rotating；The position being connected with two support bars (2) on first pushing out ring (3) is as two quadrantal points of this ring, and on first upper outside ring wall corresponding to two other quadrantal points of pushing out ring (3), rotational support has second pushing out ring (5)；Described second pushing out ring (5) can rotate with its two intercardinal lines being connected with first pushing out ring (3) for axle；Described first pushing out ring (3) and two junction points of second pushing out ring (5) have at least one to realize being rotationally connected by second conducting slip ring (6)；Second pushing out ring (5) is driven by the second conducting slip ring (6) and realizes rotating；Two positions being connected with first pushing out ring (3) on second pushing out ring (5) are as two quadrantal points of second pushing out ring (5), on second upper outside ring wall corresponding to two other quadrantal points of pushing out ring (5), rotational support has three-support ring (7), has at least one to realize being rotationally connected by the 3rd conducting slip ring (8) in described second pushing out ring (5) and two junction points of three-support ring (7)；Described three-support ring (7) can rotate with two intercardinal lines that itself and second pushing out ring (5) connect for axle；Three-support ring (7) is driven by the 3rd conducting slip ring (8) and realizes rotating；The internal diameter of described first pushing out ring (3), second pushing out ring (5) and three-support ring (7) is all higher than the maximum height of vertically taking off and landing flyer (1)；Vertically taking off and landing flyer is powered to each conducting slip ring by airborne power supply on (1).
2. a kind of aircraft as claimed in claim 1, it is characterised in that described first conducting slip ring (4), the second conducting slip ring (6), the 3rd conducting slip ring (8) have identical structure；Described conducting slip ring includes slip-ring rotor (9) and is set in the slip ring stator (10) of slip-ring rotor (9) outer border；Realize electrically connecting by conduction carbon brush between slip ring stator (10) with slip-ring rotor (9)；The slip ring stator (10) of the first conducting slip ring (4) is fixing with the top of support bar (2) to be connected, and the slip-ring rotor (9) of the first conducting slip ring (4) is fixing with first pushing out ring (3) to be connected；Slip ring stator (10) electrical connection of described power supply wire and the first conducting slip ring (4) by being located at support bar (2) inside or surface；The slip-ring rotor (9) of described second conducting slip ring (6) is fixing with second pushing out ring (5) to be connected, the slip ring stator (10) of the second conducting slip ring (6) is fixing with first pushing out ring (3) to be connected, and the slip-ring rotor (9) of the first conducting slip ring (4) passes through slip ring stator (10) electrical connection of the wire and the second conducting slip ring (6) that are located on first pushing out ring (3) inside or ring wall；The slip-ring rotor (9) of described 3rd conducting slip ring (8) is fixing with three-support ring (7) to be connected, the slip ring stator (10) of the 3rd conducting slip ring (8) is fixing with second pushing out ring (5) to be connected, and the slip-ring rotor (9) of the second conducting slip ring (6) passes through slip ring stator (10) electrical connection of the wire and the 3rd conducting slip ring (8) that are located on second pushing out ring (5) inside or ring wall.
3. a kind of aircraft as claimed in claim 2, it is characterised in that be respectively provided with an inertia measuring module (11) in the position near each self-corresponding conducting slip ring on the internal ring wall of first, second, third pushing out ring；Described inertia measuring module (11) realizes and the communication of the internal flight controller of vertically taking off and landing flyer (1) by being located at internal or outer surface and each pushing out ring ring wall or inside the wire of support bar (2).
4. a kind of aircraft as claimed in claim 3, it is characterised in that described vertically taking off and landing flyer (1) adopts single rotor No Tail Rotor structure, the fuselage left and right sides is respectively provided with an aileron (12) in the position being positioned at pair of support rods (2) lower section.
5. a kind of aircraft as claimed in claim 2, it is characterised in that realize electrically connecting by conduction carbon brush between outer wall and the inwall of slip ring stator (10) first half of slip-ring rotor (9) first half of described conducting slip ring；Having interval, slip-ring rotor (9) latter half border to be provided with coil (13) between latter half and slip ring stator (10) latter half of slip-ring rotor (9), slip ring stator (10) latter half inwall border is provided with magnetic pole (14)；Slip-ring rotor (9) leads to the connection jaws (15) for being connected wire respectively with slip ring stator (10).
6. a kind of aircraft as described in any one of claim 1 ~ 5, it is characterised in that three-support ring (7) external stability is covered with guard (23).
7. a The Cloud Terrace, adopts the aircraft as described in any one of claim 2 ~ 5, it is characterised in that be installed with a photographic head (16) on the outer wall of described three-support ring (7)；The signal output part of described photographic head (16) is by being fixed on wire and the electrical connection of the 3rd conducting slip ring (8) of three-support ring (7) ring wall or inside, and then is realized by the second conducting slip ring (6), the first conducting slip ring (4) and set the communication of flight controller in vertically taking off and landing flyer (1).
8. a sprinkler, adopts the aircraft as described in any one of claim 2 ~ 5, it is characterised in that vertically taking off and landing flyer (1) is loaded with hermetic container；It is connected by the first conducting slip ring (4) between only one of which support bar (2) with first pushing out ring (3), is rotationally connected by the first swivel joint (17) between another support bar (2) and first pushing out ring (3)；Having a junction point to adopt the second conducting slip ring (6) to be connected between first pushing out ring (3) and second pushing out ring (5), another junction point adopts the second swivel joint (18) to be rotationally connected；Having a junction point to adopt the 3rd conducting slip ring (8) to be connected between second pushing out ring (5) and three-support ring (7), another junction point adopts the 3rd swivel joint (19) to be rotationally connected；First, second, third swivel joint has identical structure；Described swivel joint includes a joint stator (20) in through structure and rotates and be nested in the joint rotor (21) in through structure that joint stator (20) is internal；The front end of joint stator (20) is stretched out in the front end of described joint rotor (21)；It is provided with sealing member between joint stator (20) and joint rotor (21)；Described another support bar (2) is provided with opening for hollow structure and top, and first, second, third pushing out ring all has the hole matched with corresponding swivel joint；Described three swivel joints both pass through corresponding hole and arrange；The joint stator (20) of described first swivel joint (17) is fixing with the top end opening of another support bar (2) to be connected；The front end of the joint rotor (21) of the first swivel joint (17) is fixing with first pushing out ring (3) to be connected；The joint stator (20) of described second swivel joint (18) is fixing with another junction point of first pushing out ring (3) to be connected, and the joint rotor (21) of described second swivel joint (18) is fixing with another junction point of second pushing out ring (5) to be connected；The joint stator (20) of described 3rd swivel joint (19) is fixing with another junction point of second pushing out ring (5) to be connected, and the joint rotor (21) of described 3rd swivel joint (19) is fixing with another junction point of three-support ring (7) to be connected；Described another support bar (2) is connected with hermetic container；Joint rotor (21) one side opening of the first swivel joint (17) passes through the opening in communication of joint stator (20) side of conduit and the second swivel joint (18) being fixed on first pushing out ring (3), the opening of joint rotor (21) side of the second swivel joint (18) passes through joint stator (20) the side open communication of conduit and the 3rd swivel joint (19) being fixed on second pushing out ring (5), joint rotor (21) one side opening of the 3rd swivel joint (19) is connected to a shower nozzle (22) being fixed on three-support ring (7) outer wall by conduit.
9. sprinkler as claimed in claim 8, it is characterised in that be fixedly provided with a photographic head (16) being positioned at shower nozzle (22) top on the outer wall of described three-support ring (7)；The signal output part of described photographic head (16) is by being fixed on wire and the electrical connection of the 3rd conducting slip ring (8) of three-support ring (7) ring wall or inside, and then is realized by the second conducting slip ring (6), the first conducting slip ring (4) and set the communication of flight controller in vertically taking off and landing flyer (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620144593.3U CN205396567U (en) | 2016-02-26 | 2016-02-26 | Aircraft, cloud platform and sprinkler |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620144593.3U CN205396567U (en) | 2016-02-26 | 2016-02-26 | Aircraft, cloud platform and sprinkler |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205396567U true CN205396567U (en) | 2016-07-27 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620144593.3U Withdrawn - After Issue CN205396567U (en) | 2016-02-26 | 2016-02-26 | Aircraft, cloud platform and sprinkler |
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| Country | Link |
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| CN (1) | CN205396567U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105752353A (en) * | 2016-02-26 | 2016-07-13 | 李俊明 | Aircraft, pan-tilt and sprinkler |
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2016
- 2016-02-26 CN CN201620144593.3U patent/CN205396567U/en not_active Withdrawn - After Issue
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105752353A (en) * | 2016-02-26 | 2016-07-13 | 李俊明 | Aircraft, pan-tilt and sprinkler |
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