CN210364380U - Maritime search and rescue unmanned aerial vehicle - Google Patents
Maritime search and rescue unmanned aerial vehicle Download PDFInfo
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- CN210364380U CN210364380U CN201921011235.5U CN201921011235U CN210364380U CN 210364380 U CN210364380 U CN 210364380U CN 201921011235 U CN201921011235 U CN 201921011235U CN 210364380 U CN210364380 U CN 210364380U
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- 230000001681 protective effect Effects 0.000 claims abstract description 28
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- 238000004519 manufacturing process Methods 0.000 abstract description 3
- 230000000694 effects Effects 0.000 description 6
- 230000003139 buffering effect Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000010030 laminating Methods 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
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- 230000003993 interaction Effects 0.000 description 1
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- 238000000034 method Methods 0.000 description 1
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Abstract
The utility model discloses an unmanned aerial vehicle searches for ands rescue at sea, including the unmanned aerial vehicle main part, the unmanned aerial vehicle main part is ball shell structure, and the equal fixed welding in both ends has connecting plate one about the unmanned aerial vehicle main part, the tip upper surface of connecting plate one is provided with waterproof protective housing, the equal fixed welding in lower surface both ends of waterproof protective housing has connecting plate two, and connecting plate two passes through the upper surface of fix with screw at connecting plate one. Has the advantages that: the utility model discloses a be the arc form of upwards sunken with the setting of flight oar for the air current that can the bearing when the flight oar rotates becomes many, the laborsaving flight that the unmanned aerial vehicle main part can be better, the unmanned aerial vehicle main part sets up and is the spheroid form, has reduced the influence of air current, and the flight is more stable. The utility model discloses a be provided with waterproof protective housing in the flight motor outside to make unmanned aerial vehicle flight on the sea when searching for and rescuing difficult because of moisture influences motor and battery production and damages, thereby guarantee unmanned aerial vehicle's normal search for and rescue operation.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle field particularly, relates to an unmanned aerial vehicle is searched for andd rescue at sea.
Background
The unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, and the application of the unmanned aerial vehicle is expanded.
Patent number CN201821431052.4 discloses an unmanned aerial vehicle maritime search and rescue device, which can realize control over a plurality of control units, that is, the number of unmanned aerial vehicles exceeds two, so as to realize distributed search, and the search effect is better; but have automatic positioning, cruise efficient, distribution range is wide, the timely advantage of rescue, however, it has following problem: search for and rescue through the search and rescue ship in this scheme, the efficiency of search and rescue is lower, and the high altitude search and rescue is efficient when there is not unmanned aerial vehicle search and rescue. Patent number CN201621364857.2 discloses an unmanned aerial vehicle for field search and rescue, this unmanned aerial vehicle can patrol the trip in the place that often appears the accident, through sound such as speech recognition system discernment "rescue", "HELP", the initiative rescue, however, the shock-absorbing capacity is relatively poor when unmanned aerial vehicle descends, unmanned aerial vehicle's life has been reduced, and unmanned aerial vehicle electric connection's position waterproof nature is relatively poor, fragile such as motor, can not guarantee normal search and rescue operation.
An effective solution to the problems in the related art has not been proposed yet.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
Not enough to prior art, the utility model provides an unmanned aerial vehicle is searched for andd rescue at sea possesses the flight stably, not fragile and the wide angle advantage of shooting, and then solves the problem among the above-mentioned background.
(II) technical scheme
For realizing above-mentioned flight stability, not fragile and wide angle advantage of shooting, the utility model discloses a specific technical scheme as follows:
an unmanned aerial vehicle for maritime search and rescue comprises an unmanned aerial vehicle main body, wherein the unmanned aerial vehicle main body is of a spherical shell structure, a first connecting plate is fixedly welded at each of the left end and the right end of the unmanned aerial vehicle main body, a waterproof protective shell is arranged on the upper surface of the end part of the first connecting plate, a second connecting plate is fixedly welded at each of the two ends of the lower surface of the waterproof protective shell, the second connecting plate is fixed on the upper surface of the first connecting plate through screws, a flight motor and a battery are sequentially arranged in the waterproof protective shell from top to bottom, the upper end of the flight motor is in transmission connection with a flight rotating shaft, a flight propeller is fixedly sleeved at the upper end part of the flight rotating shaft and is in an upwards-concave arc shape, an electric push rod is fixedly welded at the bottom end inside the unmanned aerial vehicle main body, a first fixing plate, the fixed surface of the upper surface of No. two fixed plates is provided with the camera, the sealed rubber seal that is provided with of upper end opening part of unmanned aerial vehicle main part.
Further, electric connection between flying motor and the battery, the battery is fixed to be set up in the bottom of waterproof protective housing.
Furthermore, the upper end of the flight rotating shaft movably penetrates through the upper surface of the waterproof protective shell, a waterproof sealing ring is arranged at the outer ring of the flight rotating shaft penetrating through the waterproof protective shell in a sealing mode, and the waterproof sealing ring is fixedly arranged on the waterproof protective shell.
Further, rubber seal activity laminating is around electric putter, and rubber seal keeps away from the fixed upper end opening part that sets up in the unmanned aerial vehicle main part of electric putter's outer lane department.
Furthermore, an inner groove is formed in one end, close to the electric push rod, of the rubber sealing ring, and a magnetic attraction block is filled in the inner groove.
Further, the equal fixed welding in both ends has the landing leg about the lower surface of unmanned aerial vehicle main part, and the lower extreme of landing leg is rotated through removing the wheel pivot and is connected with the removal wheel.
(III) advantageous effects
Compared with the prior art, the utility model provides an unmanned aerial vehicle is searched for andd rescue at sea possesses following beneficial effect:
(1) the utility model discloses a be the arc form of upwards caving in with the setting of flight oar for the air current that can the bearing when the flight oar rotates becomes many, the laborsaving flight that the unmanned aerial vehicle main part can be better, the unmanned aerial vehicle main part sets up and is the spheroid form, has reduced the influence of air current, and the flight is more stable.
(2) The utility model discloses a be provided with waterproof protective housing in the flight motor outside to it is difficult for influencing motor and battery production and damaging because of the moisture when searching for and rescuing to make unmanned aerial vehicle fly on the sea, thereby guarantees unmanned aerial vehicle's normal search for and rescue operation.
(3) The utility model discloses a camera is scalable inside and outside the unmanned aerial vehicle main part, and the protectiveness is stronger, stretches out when only using, and can carry out 360 degrees rotations, and 360 degrees shooting of camera when guaranteeing to search for and rescue.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings required to be used in the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.
Fig. 1 is a schematic structural diagram of an unmanned maritime search and rescue vehicle according to an embodiment of the present invention;
fig. 2 is a schematic structural view of a flight propeller of an unmanned aerial vehicle for maritime search and rescue according to an embodiment of the present invention;
fig. 3 is an enlarged view of the structure according to a in fig. 1.
In the figure:
1. an unmanned aerial vehicle main body; 2. a first connecting plate; 3. a flying motor; 4. a flight shaft; 5. a flight paddle; 6. a rubber seal ring; 7. an electric push rod; 8. a first fixing plate; 9. rotating the motor; 10. a second fixing plate; 11. a camera; 12. a support leg; 13. a moving wheel; 14. a movable wheel rotating shaft; 15. a waterproof sealing ring; 16. a waterproof protective shell; 17. a battery; 18. a second connecting plate; 19. an inner tank; 20. and a magnetic attraction block.
Detailed Description
For further explanation of the embodiments, the drawings are provided as part of the disclosure and serve primarily to illustrate the embodiments and, together with the description, to explain the principles of operation of the embodiments, and to provide further explanation of the invention and advantages thereof, it will be understood by those skilled in the art that various other embodiments and advantages of the invention are possible, and that elements in the drawings are not to scale and that like reference numerals are generally used to designate like elements.
According to the utility model discloses an embodiment provides an unmanned aerial vehicle is searched for andd rescue at sea.
The utility model is further explained by combining the attached drawings and the detailed embodiment, as shown in fig. 1-3, the unmanned aerial vehicle for maritime search and rescue according to the embodiment of the utility model comprises an unmanned aerial vehicle main body 1, the unmanned aerial vehicle main body 1 is a spherical shell structure, a first connecting plate 2 is fixedly welded at the left and right ends of the unmanned aerial vehicle main body 1, a waterproof protective shell 16 is arranged on the upper surface of the end part of the first connecting plate 2, a second connecting plate 18 is fixedly welded at the two ends of the lower surface of the waterproof protective shell 16, the second connecting plate 18 is fixed on the upper surface of the first connecting plate 2 through screws, a flying motor 3 and a battery 17 are sequentially arranged in the waterproof protective shell 16 from top to bottom, the upper end of the flying motor 3 is in transmission connection with a flying rotating shaft 4, a flying paddle 5 is fixedly sleeved at the upper end part of the flying shaft 4, the, laborsaving flight that unmanned aerial vehicle main part 1 can be better, the inside bottom fixed welding of unmanned aerial vehicle main part 1 has electric putter 7, the fixed welding in upper end of electric putter 7 has fixed plate 8 No. one, the last fixed surface welding of fixed plate 8 has rotation motor 9, fixed welding has No. two fixed plates 10 in the pivot of rotating motor 9 upper end, the last fixed surface of No. two fixed plates 10 is provided with camera 11, camera 11 use ordinary camera can, for current common technique, the sealed rubber seal 6 that is provided with of the upper end opening part of unmanned aerial vehicle main part 1.
In one embodiment, the flying motor 3 is electrically connected with the battery 17, the battery 17 is fixedly arranged at the bottom of the waterproof protective shell 16, the battery 17 supplies power to the flying motor 3, and each flying motor 3 is provided with one battery 17 and jointly protected in the waterproof protective shell 16, so that good waterproof and anti-breaking effects are achieved.
In one embodiment, the upper end of the flying spindle 4 movably passes through the upper surface of the waterproof protective shell 16, the flying spindle 4 is provided with a waterproof sealing ring 15 by sealing and sealing the outer ring of the waterproof protective shell 16, the waterproof sealing ring 15 is fixedly arranged on the waterproof protective shell 16, the waterproof protective shell 16 has good sealing and waterproof effects on the flying motor 3 through the waterproof sealing ring 15, and the flying motor 3 can use some small dc motors with better waterproof performance, for example: ks-n30va, but not limited to this type of motor, can be selected according to actual needs, and is a common technology in the prior art and is not described herein.
In one embodiment, rubber seal 6 activity laminating is around electric putter 7, and rubber seal 6 is kept away from the fixed setting of the upper end opening part at unmanned aerial vehicle main part 1 of electric putter 7's outer lane department, and electric putter 7's model can use: the ANT-26, but not limited to the electric putter of this type, may select some electric putters with higher waterproofness according to actual needs, and so on, which is a common technology in the prior art and will not be described herein.
In one embodiment, an inner groove 19 is formed inside one end of the rubber sealing ring 6 close to the electric push rod 7, a magnetic attraction block 20 is filled in the inner groove 19, the inner groove 19 facilitates installation of the magnetic attraction block 20, the magnetic attraction block 20 can be fixed on the outer side surface of the electric push rod 7 in an adsorption mode, when the electric push rod 7 is partially extended, the sealing performance inside the unmanned aerial vehicle main body 1 is kept, a controller can be installed inside the unmanned aerial vehicle main body 1, electric elements such as a power supply and a wireless receiving and sending device are used normally, when the electric push rod 7 is extended into the unmanned aerial vehicle main body 1, the middle position of the rubber sealing ring 6 is sealed through the magnetic attraction block 20 fixed in an.
In one embodiment, the equal fixed welding in both ends has landing leg 12 about the lower surface of unmanned aerial vehicle main part 1, and the lower extreme of landing leg 12 rotates through removing wheel pivot 14 to be connected with and removes wheel 13, and removal wheel 13 on the landing leg 12 of bottom has the purpose of buffering unmanned aerial vehicle main part 1 whereabouts for unmanned aerial vehicle life increases.
The working principle is as follows:
flying motor 3 drives flight oar 5 through flight pivot 4 and rotates, take unmanned aerial vehicle main part 1 aloft, realize maritime search and rescue, utilize electric putter 7 to stretch out and drive camera 11 and stretch out and shoot, camera 11 rotates through rotating motor 9 and can realize 360 degrees wide angles and shoot, electric putter 7 can protect it when stretching into unmanned aerial vehicle main part 1 with camera 11 inside, the protectiveness is stronger, only stretch out when using, the removal wheel 13 on the bottom landing leg 12 has the purpose of buffering unmanned aerial vehicle main part 1 whereabouts, make unmanned aerial vehicle life increase.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "disposed," "connected," "fixed," "screwed" and the like are to be construed broadly, e.g., as meaning fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; they may be directly connected or indirectly connected through an intermediate medium, and may be connected through the inside of two elements or in an interaction relationship between two elements, unless otherwise specifically defined, and the specific meaning of the above terms in the present invention will be understood by those skilled in the art according to specific situations.
The above description is only a preferred embodiment of the present invention, and should not be taken as limiting the invention, and any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (6)
1. The unmanned aerial vehicle for maritime search and rescue is characterized by comprising an unmanned aerial vehicle main body (1), wherein the unmanned aerial vehicle main body (1) is of a spherical shell structure, a first connecting plate (2) is fixedly welded at each of the left end and the right end of the unmanned aerial vehicle main body (1), a waterproof protective shell (16) is arranged on the upper surface of the upper end of the first connecting plate (2), a second connecting plate (18) is fixedly welded at each of the two ends of the lower surface of the waterproof protective shell (16), the second connecting plate (18) is fixed on the upper surface of the first connecting plate (2) through screws, a flight motor (3) and a battery (17) are sequentially arranged in the waterproof protective shell (16), the upper end of the flight motor (3) is in transmission connection with a flight rotating shaft (4), a flight paddle (5) is fixedly sleeved at the upper end of the flight rotating shaft (4), the flight paddle (5) is in an upwards-sunken arc, fixed welding in the upper end of electric putter (7) has fixed plate (8) No. one, and the last fixed surface welding of fixed plate (8) has rotation motor (9), and fixed welding has fixed plate (10) No. two in the pivot of rotation motor (9) upper end, and the last fixed surface of No. two fixed plates (10) is provided with camera (11), the sealed rubber seal (6) that is provided with of upper end opening part of unmanned aerial vehicle main part (1).
2. The unmanned aerial vehicle for maritime search and rescue of claim 1, wherein the flying motor (3) is electrically connected with a battery (17), and the battery (17) is fixedly arranged at the bottom of the waterproof protective shell (16).
3. The unmanned aerial vehicle for maritime search and rescue of claim 1, wherein the upper end of the flying rotating shaft (4) movably penetrates through the upper surface of the waterproof protective shell (16), a waterproof sealing ring (15) is arranged at the position, where the flying rotating shaft (4) penetrates through the outer ring of the waterproof protective shell (16), in a sealing manner, and the waterproof sealing ring (15) is fixedly arranged on the waterproof protective shell (16).
4. The unmanned aerial vehicle for maritime search and rescue of claim 1, wherein the rubber sealing ring (6) is movably attached to the periphery of the electric push rod (7), and the outer ring of the rubber sealing ring (6) far away from the electric push rod (7) is fixedly arranged at an opening at the upper end of the unmanned aerial vehicle main body (1).
5. The unmanned aerial vehicle for maritime search and rescue according to claim 1, wherein an inner groove (19) is formed inside one end, close to the electric push rod (7), of the rubber sealing ring (6), and a magnetic suction block (20) is filled in the inner groove (19).
6. The unmanned aerial vehicle for maritime search and rescue according to claim 1, wherein the left end and the right end of the lower surface of the unmanned aerial vehicle main body (1) are fixedly welded with supporting legs (12), and the lower ends of the supporting legs (12) are rotatably connected with moving wheels (13) through moving wheel rotating shafts (14).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921011235.5U CN210364380U (en) | 2019-07-02 | 2019-07-02 | Maritime search and rescue unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921011235.5U CN210364380U (en) | 2019-07-02 | 2019-07-02 | Maritime search and rescue unmanned aerial vehicle |
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| Publication Number | Publication Date |
|---|---|
| CN210364380U true CN210364380U (en) | 2020-04-21 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201921011235.5U Expired - Fee Related CN210364380U (en) | 2019-07-02 | 2019-07-02 | Maritime search and rescue unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114524095A (en) * | 2022-02-18 | 2022-05-24 | 江苏佰通智能科技有限公司 | Unmanned aerial vehicle with automatically, keep away dangerous function |
-
2019
- 2019-07-02 CN CN201921011235.5U patent/CN210364380U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114524095A (en) * | 2022-02-18 | 2022-05-24 | 江苏佰通智能科技有限公司 | Unmanned aerial vehicle with automatically, keep away dangerous function |
| CN114524095B (en) * | 2022-02-18 | 2023-08-18 | 江苏佰通智能科技有限公司 | Unmanned aerial vehicle with automatic danger avoiding function |
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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20221207 Address after: 1105-02, Building B, International Headquarters, Han Street, No. 86, Zhongbei Road, Guoguohu Street, Wuchang District, Wuhan City, 430000 Hubei Province Patentee after: Hubei Warring Wolf Airlines Co.,Ltd. Address before: No.81 Baiyang village, Baizhang Town, Minqing County, Fuzhou City, Fujian Province Patentee before: Zhan Gongqiang |
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200421 |