CN116062200B - Sucker type wave energy self-generating unmanned aerial vehicle - Google Patents
Sucker type wave energy self-generating unmanned aerial vehicle Download PDFInfo
- Publication number
- CN116062200B CN116062200B CN202310131206.7A CN202310131206A CN116062200B CN 116062200 B CN116062200 B CN 116062200B CN 202310131206 A CN202310131206 A CN 202310131206A CN 116062200 B CN116062200 B CN 116062200B
- Authority
- CN
- China
- Prior art keywords
- unmanned aerial
- aerial vehicle
- power generation
- generation device
- wave energy
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C35/00—Flying-boats; Seaplanes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03B—MACHINES OR ENGINES FOR LIQUIDS
- F03B13/00—Adaptations of machines or engines for special use; Combinations of machines or engines with driving or driven apparatus; Power stations or aggregates
- F03B13/12—Adaptations of machines or engines for special use; Combinations of machines or engines with driving or driven apparatus; Power stations or aggregates characterised by using wave or tide energy
- F03B13/14—Adaptations of machines or engines for special use; Combinations of machines or engines with driving or driven apparatus; Power stations or aggregates characterised by using wave or tide energy using wave energy
- F03B13/22—Adaptations of machines or engines for special use; Combinations of machines or engines with driving or driven apparatus; Power stations or aggregates characterised by using wave or tide energy using wave energy using the flow of water resulting from wave movements to drive a motor or turbine
-
- 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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/30—Energy from the sea, e.g. using wave energy or salinity gradient
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
Abstract
Sucking disc formula wave energy is from unmanned aerial vehicle belongs to unmanned aerial vehicle technical field. Not only can effectively generate electricity, solve unmanned aerial vehicle continuation of journey problem, can also adsorb fixedly on arbitrary shape surface. The lower end of the power generation device is arranged on the unmanned aerial vehicle main body, the upper end of the power generation device is provided with the adsorption device, the unmanned aerial vehicle main body is used as an energy receiver to move along with waves in a fluctuation mode after being fixed on a fixed structure on the sea through the adsorption device, and the power generation device is used for cutting the magnetic induction line to generate power. According to the unmanned aerial vehicle, the unmanned aerial vehicle body is used as an energy receiver and moves along with wave fluctuation, the wave energy self-generating function of the unmanned aerial vehicle is realized through the cutting magnetic induction line generating process in the energy conversion device, the power generation can be effectively performed, and the problem of unmanned aerial vehicle endurance is solved. The adsorption device adopts a sucker structure, negative pressure is formed in the sucker through the air pump, and meanwhile, the second electric push rod controls the rigid frame to stretch out and draw back to adjust the negative pressure space in the sucker structure, so that the adsorption device is firmly adsorbed to the surface of an object and serves as a fixed body of the wave energy power generation device.
Description
Technical Field
The application belongs to the technical field of unmanned aerial vehicles, and particularly relates to a sucker type wave energy self-generating unmanned aerial vehicle.
Background
In offshore operation, unmanned aerial vehicle relies on characteristics such as the function is various, flexible concealing, lasting long-range and full-time multi-domain, can accomplish multiple operation requirement, bears multiple task, and long-time, long-range operation task requirement unmanned aerial vehicle has high duration. Therefore, it is very important to develop a flexible small-sized wave energy self-generating unmanned aerial vehicle.
The present patent number is CN 201910221930.2's application patent, discloses a wave energy self-generating fixed wing sea base unmanned aerial vehicle, includes: the device comprises a pair of swing wings, a power generation system, a storage battery, a swing wing damping adjustment system, a fuselage quality adjustment system, a tail wing and a propeller. The machine body adopts a double-layer shell, the inner shell is a watertight pressure-resistant shell, and the outer shell is a non-watertight non-pressure-resistant shell; the two layers of shells are filled with water when in water, so that the wave energy power generation capacity is improved; draining water in the process of leaving the water surface, and completely draining water in the air to lighten the dead weight of the flight. And the total electric power is regulated, so that the damping of the swing wing is regulated, and the stability of the swing wing during sailing in water and flying in air is kept. The device considers that relative motion between the energy receiving body and the fixed body is required when wave energy is utilized to generate electricity, but the adopted machine body quality adjusting system can not only increase a small amount of resistance in fact and is difficult to play a role in adjusting, but also can disturb the self posture of the unmanned aerial vehicle, so that accidents such as integral overturning and the like are caused, and the electricity generating function of the unmanned aerial vehicle cannot be effectively realized.
Meanwhile, the surfaces of rocks, ocean engineering structures and the like which can be adsorbed by the unmanned aerial vehicle on the sea are irregular in general shape and different in inclination angle, and the common sucker has the characteristics of wetting, roughness and the like, and is difficult to meet the requirements of adsorption fixation and self-power generation as a fixed body.
Disclosure of Invention
The application aims to solve the problems, and further provides the sucker type wave energy self-generating unmanned aerial vehicle, which not only can effectively generate electricity and solve the problem of unmanned aerial vehicle endurance, but also can be adsorbed and fixed on the surface with any shape.
The technical scheme adopted by the application is as follows:
the sucker type wave energy self-generating unmanned aerial vehicle comprises an unmanned aerial vehicle main body, a power generation device and an adsorption device; the power generation device is characterized in that the lower end of the power generation device is arranged on the unmanned aerial vehicle main body, the adsorption device is arranged at the upper end of the power generation device, the unmanned aerial vehicle main body is used as an energy receptor to move along with waves in a fluctuation mode after being fixed on a fixed structure on the sea through the adsorption device, and the power generation device is used for cutting a magnetic induction line to generate power.
Compared with the prior art, the application has the following beneficial effects:
1. according to the unmanned aerial vehicle, the unmanned aerial vehicle body is used as an energy receiver and moves along with wave fluctuation, the wave energy self-generating function of the unmanned aerial vehicle is realized through the cutting magnetic induction line generating process in the energy conversion device, the power generation can be effectively performed, and the problem of unmanned aerial vehicle endurance is solved.
2. The suction device adopts a sucker structure, negative pressure is formed in the sucker through the air pump, and the second electric push rod controls the telescopic rigid frame to stretch to adjust the negative pressure space in the sucker structure, so that the suction device is firmly sucked to the surface of an object and serves as a fixed body of the wave energy power generation device.
3. The support arm of the rotor wing of the unmanned aerial vehicle main body can retract into the unmanned aerial vehicle main body, so that the support arm and the rotor wing are prevented from being damaged when floating and vibrating in waves.
4. The unmanned aerial vehicle body is modularized, and can be loaded with different functional modules to provide support for offshore operation.
Drawings
FIG. 1 is a schematic diagram of the structure of the present application;
FIG. 2 is a front view of the present application;
FIG. 3 is a schematic view showing the state that the adsorption device of the present application is adsorbed to the surface of an inclined fixture;
FIG. 4 is a schematic illustration of the telescopic link of the present application in a contracted state;
FIG. 5 is a schematic view of the power plant of the present application in a contracted state of the telescopic link;
FIG. 6 is a schematic view of the power plant of the present application in a telescopic link extended state;
FIG. 7 is a schematic view of the structure of the adsorption apparatus of the present application;
FIG. 8 is a schematic view of the support chuck structure of the present application;
fig. 9 is a schematic view of the internal structure of the unmanned aerial vehicle body of the present application;
FIG. 10 is a schematic view of the application illustrating the retraction of the arm into the housing;
FIG. 11 is a top view of the arm retracted back to the housing of the present application;
FIG. 12 is an isometric view of the arm of the present application extended from the housing;
FIG. 13 is a top view of the arm extension housing of the present application;
wherein: 1. an unmanned aerial vehicle main body; 2. a power generation device; 3. an adsorption device; 4. a universal joint; 5. a three-way joint; 11. a rotor; 12. a motor; 13. a support arm; 14. a contracted structure; 15. a housing; 141. a sleeve; 142. a connector; 143. a connecting rod; 21. a retractable connecting rod; 22. an energy conversion device; 31. a fixed rod; 32. a movable lever; 33. a support sucker; 331. a flexible suction cup membrane; 332. a rigid frame; 333. a second electric push rod; 334. a connecting rod; 34. an air pump; 35. a fixing frame; 36. and (5) a base.
Detailed Description
For a better understanding of the objects, structures and functions of the present application, reference should be made to the following detailed description of the application with reference to the accompanying drawings.
Aiming at the complex operation environment of the amphibious unmanned aerial vehicle, namely a wet and complex-shape adsorption surface, the application designs a novel unmanned aerial vehicle capable of utilizing wave energy to perform self-power generation, and solves the problem of endurance and adsorption of the unmanned aerial vehicle.
Referring to fig. 1-13, the sucker type wave energy self-generating unmanned aerial vehicle comprises an unmanned aerial vehicle main body 1, a generating device 2 and an adsorption device 3; the power generation device 2 lower extreme is installed on unmanned aerial vehicle main part 1, and adsorption equipment 3 is installed to power generation device 2 upper end, fixes behind the fixed knot structure thing on sea through adsorption equipment 3, and unmanned aerial vehicle main part 1 is as the receiver and wave and fluctuation motion, through power generation device 2 cutting magnetism induction line electricity generation, realizes unmanned aerial vehicle's self-generating function.
The adsorption device 3 is connected with the power generation device 2 through a universal joint 4, and the lower part of the power generation device 2 is connected with the unmanned aerial vehicle main body 1 through a three-way joint 5.
As shown in fig. 9-13, the unmanned aerial vehicle main body 1 includes a contraction structure 14, a housing 15, four rotor wings 11, four motors 12, and four support arms 13; the four support arms 13 are uniformly distributed on the left side and the right side of the shell 15, motors 12 are vertically arranged at the outer ends of the four support arms 13, the four rotary wings 11 are vertically arranged on output shafts of the corresponding motors 12 respectively, the inner ends of the four support arms 13 are slidably inserted into the shell 15 and are connected with a shrinkage structure 14 arranged in the shell 15, and the shrinkage structure 14 can drive the four support arms 13 to retract into the shell 15.
The shrinkage structure 14 comprises a sleeve 141, two connectors 142 and four connecting rods 143; the sleeve 141 is detachably fixed at the middle position of the shell 15 along the front-back direction of the shell 15, the two connectors 142 are respectively and slidably sleeved in the inner cavities at the front end and the rear end of the sleeve 141, one ends of the four connecting rods 143 are hinged to the corresponding connectors 142, the connecting positions of the two connecting rods are hinge points, the other ends of the four connecting rods 143 are hinged to the inner ends of the corresponding support arms 13, four strip openings are formed in the positions of the sleeve 141 corresponding to the four hinge points along the front-back direction, the two connectors 142 are respectively pushed by two first electric push rods which are arranged in the inner cavity of the sleeve 141, and when the connectors 142 slide linearly towards the inside of the sleeve 141, the connectors 142 can drive the four connecting rods 143 to retract into the sleeve 141.
As shown in fig. 9, the outer ends of the two connectors 142 are provided with a platform notch at the position of the strip notch, and the hinge points of the connectors 142 and the connecting rod 143 are arranged at the platform notch.
As shown in fig. 5 and 6, the power generation device 2 includes a telescopic link 21 and an energy conversion device 22; the telescopic connecting rods 21 are arranged at the upper end and the lower end of the energy conversion device 22, the telescopic connecting rods 21 at the lower end are connected with the three-way joint 5 sleeved on the sleeve 141, and the telescopic connecting rods 21 at the upper end are connected with the adsorption device 3 through the universal joint 4.
The telescopic connecting rod 21 adopts an electric telescopic rod, and the expansion and contraction states of each rod section are adjusted by electric control.
As shown in fig. 7 and 8, the adsorption device 3 includes a base 36, two fixing rods 31, two movable rods 32, four supporting suckers 33, four air pumps 34, and two fixing frames 35; the two fixed rods 31 are vertically arranged on the base 36, the two movable rods 32 are rotatably arranged on the fixed frames 35, the two movable rods 32 are driven to rotate by the steering engine, the two fixed frames 35 are arranged on the base 36, the two fixed rods 31 and the two movable rods 32 are distributed in a cross diagonal manner, the two fixed rods 31 and the two movable rods 32 are provided with the supporting suckers 33, and the four supporting suckers 33 are connected with the air pump 34.
The two movable bars 32 are rotatable to adjust the posture. The two fixing rods 31 realize initial adsorption fixation; the two movable rods 32 are then fixed by suction.
The supporting sucker 33 forms negative pressure in the supporting sucker 33 through the air pump 34, and meanwhile, the second electric push rod 333 controls the telescopic rigid frame 332 to telescopically adjust the negative pressure space in the supporting sucker 33, so that extremely strong suction force can be generated, and the supporting sucker can be firmly adhered to the surfaces of various dry or wet fixed structures with any shapes on the sea surface to be used as a stator for realizing energy conversion.
As shown in fig. 8, the support chuck 33 includes an outer flexible chuck membrane 331 and a flexible rigid frame 332 mounted inside the flexible chuck membrane 331.
The rigid frame 332 adopts a scissor type telescopic structure, the middle part of the rigid frame 332 is fixed in the flexible sucker membrane 331 by a connecting rod 334, a second electric push rod 333 is further connected between the connecting rod 334 and the rigid frame 332, and the expansion and contraction of the second electric push rod 333 can control the expansion and contraction of the rigid frame 332.
The second electric push rod 333 is connected with the connecting rod 334 to control the expansion and contraction of the rigid frame 332, so that the internal negative pressure space formed after adsorption is increased and reduced, and the adsorption effect is adjusted.
Principle of operation
1. The navigation state of the unmanned aerial vehicle is shown in fig. 4, and in the navigation state, the telescopic connecting rod 21 of the unmanned aerial vehicle is in a contracted state, so that navigation is facilitated; when the unmanned aerial vehicle automatically monitors that the electric quantity is low, the unmanned aerial vehicle falls to the vicinity of the sea surface, finds adsorbable substances, and performs adsorption fixation and wave self-power generation.
2. A schematic diagram of the adsorption device 3 is shown in fig. 7; the surface of the unmanned aerial vehicle adsorbing object comprises two processes, namely an initial adsorbing and fixing process, wherein under the action of an air pump 34, a supporting sucker 33 connected with the upper ends of two fixing rods 31 of the adsorbing device 3 is adsorbed to the solid surface first, so that the initial adsorbing and fixing effect is achieved; then, the solid surface is automatically identified by the two movable rods 32, and then the self angle is automatically adjusted under the control of the steering engine, so that the supporting sucker 33 connected with the upper end is completely adsorbed on the solid surface, and the effect of reinforcing adsorption fixation is achieved.
3. The schematic diagrams of the unmanned aerial vehicle for wave energy self-power generation are shown in fig. 1 and 3, the wave energy self-power generation process of the unmanned aerial vehicle is performed after the adsorption process is completed, and when the adsorption device 3 is adsorbed and fixed on other marine fixed structures, the telescopic connecting rod 21 stretches to the maximum length. When the surface of the adsorbed fixed structure is an inclined surface, the telescopic connecting rod 21 can automatically rotate to the vertical direction under the action of gravity through the connecting universal joint 4, and mechanical self-locking is realized. The adsorption device 3 and the telescopic connecting rod 21 connected with the adsorption device are used as a fixed body, the unmanned aerial vehicle main body 1 is used as an energy receiving body and moves along with the fluctuation of waves, and the wave energy self-generating function of the unmanned aerial vehicle is realized through the cutting magnetic induction line generating process inside the energy conversion device 22.
4. The support arm 13 of the connecting rotor 11 is hinged with the connectors 142 through the connecting rods 143, the two connectors 142 are respectively sleeved in the inner cavities at the front end and the rear end of the two sleeves 141 in a sliding mode, the two sleeves 141 are detachably fixed in the through cavity in the front-rear direction of the three-way joint 5, the diameters of the inner cavities of the three-way joint 5 and the sleeves 141 and the outer diameter of the connectors 142 are reduced, and four strip openings are formed in the positions, corresponding to the four hinge points of the connecting rods 143, of the connectors 142 on the sleeves 141 along the front-rear direction. When the unmanned aerial vehicle adsorbs the fixed knot structure that is fixed in other seas and gets into the power generation state, first electric putter control connector 142 slides to sleeve 141 inside to drive four connecting rods 143 and retract sleeve 141, make support arm 13 shrink to in the casing 15, in order to prevent support arm 13 and rotor 11 to float when vibrating in the wave and take place to damage.
5. The inside scalable rigid frame 332 that is provided with the rigidity material of support sucking disc 33, after the sucking disc adsorbs to object surface back formation negative pressure space, rigid frame 332 extends all around, props up outside flexible sucking disc membrane 331 to increase the volume in inside negative pressure space, more firmly adsorb to object surface, act as wave energy power generation device's stator.
It will be understood that the application has been described in terms of several embodiments, and that various changes and equivalents may be made to these features and embodiments by those skilled in the art without departing from the spirit and scope of the application. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the application without departing from the essential scope thereof. Therefore, it is intended that the application not be limited to the particular embodiment disclosed, but that the application will include all embodiments falling within the scope of the appended claims.
Claims (5)
1. The utility model provides a sucking disc formula wave energy is from unmanned aerial vehicle which characterized in that: comprises an unmanned plane main body (1), a power generation device (2) and an adsorption device (3); the lower end of the power generation device (2) is arranged on the unmanned aerial vehicle main body (1), the upper end of the power generation device (2) is provided with the adsorption device (3), the unmanned aerial vehicle main body (1) is used as an energy receiving body to move along with waves in a fluctuation way after being fixed on a marine fixed structure through the adsorption device (3), the power generation device (2) is used for cutting a magnetic induction line to generate power, the adsorption device (3) is connected with the power generation device (2) through the universal joint (4), the lower part of the power generation device (2) is connected with the unmanned aerial vehicle main body (1) through the tee joint (5),
the power generation device (2) comprises a telescopic connecting rod (21) and an energy conversion device (22); the upper end and the lower end of the energy conversion device (22) are respectively provided with a telescopic connecting rod (21), the telescopic connecting rod (21) at the lower end is connected with a three-way joint (5) sleeved on a sleeve (141), the telescopic connecting rod (21) at the upper end is connected with the adsorption device (3) through a universal joint (4),
the adsorption device (3) comprises a base (36), two fixed rods (31), two movable rods (32), four supporting suckers (33), four air pumps (34) and two fixing frames (35); the two fixed rods (31) are vertically arranged on the base (36), the two movable rods (32) are rotatably arranged on the fixed frames (35), the two movable rods (32) are driven by the steering engine to rotate, the two fixed frames (35) are arranged on the base (36), the two fixed rods (31) and the two movable rods (32) are respectively provided with a supporting sucker (33), the four supporting suckers (33) are respectively connected with the air pump (34),
the supporting sucker (33) comprises an external flexible sucker membrane (331) and a rigid frame (332) which is arranged inside the flexible sucker membrane (331) and is connected and controlled to stretch by a second electric push rod (333).
2. The suction cup type wave energy self-generating unmanned aerial vehicle according to claim 1, wherein: the unmanned aerial vehicle main body (1) comprises a contraction structure (14), a shell (15), four rotary wings (11), four motors (12) and four support arms (13); the four support arms (13) are uniformly distributed on the left side and the right side of the shell (15), motors (12) are vertically arranged at the outer ends of the four support arms (13), the four rotary wings (11) are vertically arranged on output shafts corresponding to the motors (12) respectively, the inner ends of the four support arms (13) are slidably inserted into the shell (15) and are connected with a contraction structure (14) arranged in the shell (15), and the contraction structure (14) can drive the four support arms (13) to retract into the shell (15).
3. The suction cup type wave energy self-generating unmanned aerial vehicle according to claim 2, wherein: the shrinkage structure (14) comprises a sleeve (141), two connectors (142) and four connecting rods (143); the sleeve (141) can be dismantled along casing (15) fore-and-aft direction and fix in casing (15) middle part position department, two connector (142) slip respectively in the inner chamber at both ends around sleeve (141), four connecting rod (143) one end articulates on corresponding connector (142), the position that both connect is the hinge, four connecting rod (143) other ends articulate on corresponding support arm (13) inner end, four rectangular openings are seted up along fore-and-aft direction in the position department of corresponding four hinge on sleeve (141), two connectors (142) are pushed by two first electric putter built-in sleeve (141) inner chamber respectively, when connector (142) are slided along straight line to sleeve (141) inside, connector (142) can drive four connecting rods (143) and withdraw sleeve (141).
4. A suction cup type wave energy self-generating unmanned aerial vehicle as claimed in claim 3, wherein: the outer ends of the two connectors (142) are provided with platform notches at the positions of the strip notches, and hinge points of the connectors (142) and the connecting rods (143) are arranged at the platform notches.
5. The suction cup type wave energy self-generating unmanned aerial vehicle according to claim 1, wherein: the two fixed rods (31) and the two movable rods (32) are distributed in a cross diagonal line.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310131206.7A CN116062200B (en) | 2023-02-17 | 2023-02-17 | Sucker type wave energy self-generating unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310131206.7A CN116062200B (en) | 2023-02-17 | 2023-02-17 | Sucker type wave energy self-generating unmanned aerial vehicle |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN116062200A CN116062200A (en) | 2023-05-05 |
| CN116062200B true CN116062200B (en) | 2023-08-29 |
Family
ID=86181842
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202310131206.7A Active CN116062200B (en) | 2023-02-17 | 2023-02-17 | Sucker type wave energy self-generating unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN116062200B (en) |
Citations (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2009076714A1 (en) * | 2007-12-17 | 2009-06-25 | Seapower Pacific Pty Ltd | Apparatus for extraction of energy from wave motion |
| CN102099570A (en) * | 2008-05-15 | 2011-06-15 | 海洋能量系统有限责任公司 | Wave energy recovery system |
| CN103827477A (en) * | 2011-08-31 | 2014-05-28 | 李晟佑 | Power generation apparatus including a floating body, ship propelling apparatus, and foldable and windable wing included in the power generation apparatus |
| CN108061013A (en) * | 2017-12-06 | 2018-05-22 | 天津大学 | Portable sea complex energy transformation platform |
| KR101912101B1 (en) * | 2017-09-07 | 2018-10-26 | 한국해양대학교 산학협력단 | Self-charging drone |
| CN109098920A (en) * | 2018-10-30 | 2018-12-28 | 浙江海洋大学 | A kind of sensorcraft waterborne with generating function |
| CN109707556A (en) * | 2019-02-19 | 2019-05-03 | 李安 | A kind of fixed seashore wave oscillations power generator |
| CN208979098U (en) * | 2018-10-30 | 2019-06-14 | 浙江海洋大学 | A kind of structure improved sensorcraft waterborne |
| CN109911198A (en) * | 2019-03-22 | 2019-06-21 | 武汉理工大学 | A kind of wave energy self power generation fixed-wing sea base unmanned plane |
| CN110945234A (en) * | 2019-10-29 | 2020-03-31 | 中山大学 | Offshore energy island device |
| CN111305995A (en) * | 2019-02-26 | 2020-06-19 | 北京纳米能源与系统研究所 | Self-assembly wave energy generator network and self-assembly method |
| CN111608850A (en) * | 2020-05-28 | 2020-09-01 | 谭银朝 | Power generation device based on ship use and implementation method thereof |
| CN212766743U (en) * | 2020-06-08 | 2021-03-23 | 福建中利科技有限公司 | Unmanned aerial vehicle capable of independently supplying power and suitable for offshore search |
| CN213235314U (en) * | 2020-08-24 | 2021-05-18 | 中国科学院南海海洋研究所 | Wave energy power generation device of marine environment unmanned monitoring ship |
| CN115042922A (en) * | 2022-03-24 | 2022-09-13 | 武汉理工大学 | Ocean monitor based on self-adsorption principle |
| CN115535234A (en) * | 2022-11-10 | 2022-12-30 | 哈尔滨工程大学 | Water take-off and landing unmanned aerial vehicle capable of generating power by utilizing wave energy |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113120182B (en) * | 2021-04-09 | 2022-04-01 | 中国科学院广州能源研究所 | Deep sea multi-energy complementary power generation production and life detection comprehensive platform |
-
2023
- 2023-02-17 CN CN202310131206.7A patent/CN116062200B/en active Active
Patent Citations (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2009076714A1 (en) * | 2007-12-17 | 2009-06-25 | Seapower Pacific Pty Ltd | Apparatus for extraction of energy from wave motion |
| CN102099570A (en) * | 2008-05-15 | 2011-06-15 | 海洋能量系统有限责任公司 | Wave energy recovery system |
| CN103827477A (en) * | 2011-08-31 | 2014-05-28 | 李晟佑 | Power generation apparatus including a floating body, ship propelling apparatus, and foldable and windable wing included in the power generation apparatus |
| KR101912101B1 (en) * | 2017-09-07 | 2018-10-26 | 한국해양대학교 산학협력단 | Self-charging drone |
| CN108061013A (en) * | 2017-12-06 | 2018-05-22 | 天津大学 | Portable sea complex energy transformation platform |
| CN109098920A (en) * | 2018-10-30 | 2018-12-28 | 浙江海洋大学 | A kind of sensorcraft waterborne with generating function |
| CN208979098U (en) * | 2018-10-30 | 2019-06-14 | 浙江海洋大学 | A kind of structure improved sensorcraft waterborne |
| CN109707556A (en) * | 2019-02-19 | 2019-05-03 | 李安 | A kind of fixed seashore wave oscillations power generator |
| CN111305995A (en) * | 2019-02-26 | 2020-06-19 | 北京纳米能源与系统研究所 | Self-assembly wave energy generator network and self-assembly method |
| CN109911198A (en) * | 2019-03-22 | 2019-06-21 | 武汉理工大学 | A kind of wave energy self power generation fixed-wing sea base unmanned plane |
| CN110945234A (en) * | 2019-10-29 | 2020-03-31 | 中山大学 | Offshore energy island device |
| CN111608850A (en) * | 2020-05-28 | 2020-09-01 | 谭银朝 | Power generation device based on ship use and implementation method thereof |
| CN212766743U (en) * | 2020-06-08 | 2021-03-23 | 福建中利科技有限公司 | Unmanned aerial vehicle capable of independently supplying power and suitable for offshore search |
| CN213235314U (en) * | 2020-08-24 | 2021-05-18 | 中国科学院南海海洋研究所 | Wave energy power generation device of marine environment unmanned monitoring ship |
| CN115042922A (en) * | 2022-03-24 | 2022-09-13 | 武汉理工大学 | Ocean monitor based on self-adsorption principle |
| CN115535234A (en) * | 2022-11-10 | 2022-12-30 | 哈尔滨工程大学 | Water take-off and landing unmanned aerial vehicle capable of generating power by utilizing wave energy |
Also Published As
| Publication number | Publication date |
|---|---|
| CN116062200A (en) | 2023-05-05 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN108639287B (en) | Large-scale heavy-load hybrid-driven underwater glider | |
| US11208186B2 (en) | Water-air amphibious cross-medium bio-robotic flying fish | |
| CN112140820B (en) | Automatic many rotors of folding water-air amphibious robot | |
| KR101912101B1 (en) | Self-charging drone | |
| CN110116793A (en) | A kind of leg-arm-paddle composite underwater robot | |
| CN106516110A (en) | Water-air amphibious glider capable of vertically taking-off, landing and flying | |
| CN111703562B (en) | Foldable wave energy self-sufficient underwater vehicle | |
| CN105501405A (en) | Folding propeller for above-water platform | |
| CN112124583A (en) | H-shaped four-rotor amphibious unmanned aerial vehicle with Magnus anti-rolling device | |
| CN112158318B (en) | Hybrid bidirectional vertical profiler based on telescopic wings and bidirectional localization method thereof | |
| CN113788132A (en) | Vector-propelled hybrid drive underwater robot | |
| CN116062200B (en) | Sucker type wave energy self-generating unmanned aerial vehicle | |
| CN110816830A (en) | Water-air amphibious robot capable of achieving vector propulsion | |
| CN117429591A (en) | Underwater expandable active sonar aircraft | |
| CN110103650B (en) | Amphibious balance car | |
| CN115285325B (en) | Anti-collision underwater robot | |
| CN208102299U (en) | A kind of propulsion device for capableing of two-sided water suction | |
| CN104443343A (en) | Vectored thruster suspension type flight device | |
| CN214165267U (en) | Novel unmanned navigation ware can dive | |
| CN113682435A (en) | Novel wave glider of multi-link formula | |
| CN213008735U (en) | Retractable cloud platform survey and drawing unmanned aerial vehicle | |
| CN113386950A (en) | Adjustable skid undercarriage for unmanned helicopter | |
| CN112894845A (en) | Underwater robot | |
| CN217260681U (en) | Protective structure for aircraft shell | |
| CN220577469U (en) | Movable supporting seat of oblique stone throwing guide pipe |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |