CN221251732U - Unmanned vehicle on water surface - Google Patents
Unmanned vehicle on water surface Download PDFInfo
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- CN221251732U CN221251732U CN202323426291.4U CN202323426291U CN221251732U CN 221251732 U CN221251732 U CN 221251732U CN 202323426291 U CN202323426291 U CN 202323426291U CN 221251732 U CN221251732 U CN 221251732U
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- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 title claims abstract description 30
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- 238000010295 mobile communication Methods 0.000 claims description 15
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- 230000002708 enhancing effect Effects 0.000 claims description 3
- 238000000034 method Methods 0.000 abstract description 3
- 230000008569 process Effects 0.000 abstract description 3
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- 108010066114 cabin-2 Proteins 0.000 description 29
- 239000000463 material Substances 0.000 description 7
- 238000004364 calculation method Methods 0.000 description 4
- 238000001514 detection method Methods 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 4
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- 229920005830 Polyurethane Foam Polymers 0.000 description 2
- 230000006378 damage Effects 0.000 description 2
- 239000006261 foam material Substances 0.000 description 2
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- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 239000011496 polyurethane foam Substances 0.000 description 2
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 238000013473 artificial intelligence Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000009189 diving Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005358 geomagnetic field Effects 0.000 description 1
- 238000003384 imaging method Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 229910052744 lithium Inorganic materials 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000004377 microelectronic Methods 0.000 description 1
- 239000002985 plastic film Substances 0.000 description 1
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- 238000004451 qualitative analysis Methods 0.000 description 1
- 238000012876 topography Methods 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- 238000004078 waterproofing Methods 0.000 description 1
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- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The application belongs to the field of unmanned aircrafts and relates to a water surface unmanned aircrafts, which comprises a controller, a trapezoid connecting frame with a short side and a bevel side, wherein the short side is the upper bottom edge of the trapezoid connecting frame, and the water surface unmanned aircrafts also comprise an electric cabin arranged above the short side of the trapezoid connecting frame, a battery cabin arranged below the short side of the trapezoid connecting frame and positioned at the inner side of the bevel side of the connecting frame, a propeller fixed at the bottom end of the bevel side of the trapezoid connecting frame, and a floating block positioned above the propeller and fixed at the middle part of the bevel side of the trapezoid connecting frame; according to the application, the electric appliance cabin, the battery cabin, the propeller and the floating block are fixedly arranged on the trapezoid connecting frame, and the electric appliance cabin and the battery cabin are respectively arranged at the upper end and the lower end of the trapezoid connecting frame, so that parts in the electric appliance cabin and the battery cabin are mutually independent, the battery in the battery cabin is convenient to detach or replace, the parts in the electric appliance cabin cannot be damaged in the replacement process, and the service life of the aircraft is prolonged.
Description
Technical Field
The application belongs to the field of unmanned aircrafts, and particularly relates to an unmanned aircrafts on water.
Background
Unmanned aircraft refers to an instrument which is not driven by a person and is controlled under the water by remote control or automatic control, and mainly refers to an intelligent system which replaces a diver or a manned small submarine to carry out high-risk underwater operations such as deep sea detection, lifesaving, mine removal and the like. Therefore, unmanned submarines are also known as "submersible robots" or "underwater robots". The development of the unmanned underwater vehicle starts in the 50 s, and with the sudden rapid advance of computer technology, artificial intelligence technology, microelectronic technology, small navigation equipment, command and control hardware and logic and software technology, the unmanned underwater vehicle is greatly developed and is increasingly valued by ocean technical departments of various countries.
The traditional unmanned vehicle on water surface can not be quickly replaced due to the battery, the lead and other parts arranged in the cabin, and other parts are easy to damage when the battery is disassembled or replaced.
Disclosure of utility model
In order to overcome the problems in the background technology, the application provides a water surface unmanned aircraft, and aims to solve the problem that the water surface unmanned aircraft is complex in structure.
In order to achieve the above purpose, the application is realized by the following technical scheme:
The utility model provides an unmanned vehicles of surface of water, includes the controller, has the trapezoidal link of minor face and hypotenuse, the minor face is the last base of trapezoidal link, its characterized in that: the unmanned water surface vehicle further comprises an electric appliance cabin arranged above the short side of the trapezoid connecting frame, a battery cabin arranged below the short side of the trapezoid connecting frame and positioned on the inner side of the bevel edge of the connecting frame, a propeller fixed at the bottom end of the bevel edge of the trapezoid connecting frame, and a floating block positioned above the propeller and fixed in the middle of the bevel edge of the trapezoid connecting frame;
A first U-shaped frame is arranged between the electric appliance cabin and the trapezoid connecting frame, an outer shell of the electric appliance cabin is fixedly connected to the inner wall of the first U-shaped frame, and the upper end face of the short side of the trapezoid connecting frame is fixedly connected with the outer wall of the first U-shaped frame;
The upper end of the electric appliance cabin is fixedly connected with a picture transmission antenna for enhancing signals, and a controller is arranged in the electric appliance cabin and used for controlling the motion state of the aircraft and transmitting back images; the bottom of the electric appliance cabin is also provided with a side-scan sonar for detecting underwater structures and objects in water.
A second U-shaped frame is arranged between the battery compartment and the trapezoid connecting frame, the outer shell of the battery compartment is fixedly connected to the inner wall of the second U-shaped frame, and the lower end face of the short side of the trapezoid connecting frame is fixedly connected with the outer wall of the second U-shaped frame;
At least one battery is arranged in the battery compartment, and the battery is electrically connected with the motor of the propeller and the controller.
Optionally, the horizontal central axis of the electrical compartment and the horizontal central axis of the battery compartment are located on the same vertical plane.
Optionally, the propeller comprises two groups, each group of the propeller comprises a propeller shaft and a propeller, and the propulsion direction of the propeller is changed by adjusting the angle of the propeller.
Optionally, the bevel edges are divided into two groups, the two groups of bevel edges are symmetrically arranged by taking the vertical central line of the short edge as a symmetrical axis, and the two groups of propellers are respectively fixed at the bottom ends of the two groups of bevel edges.
Optionally, the floating blocks comprise two groups, and the two groups of floating blocks are respectively fixed at the middle parts of the two groups of inclined sides and are used for providing buoyancy for the aircraft.
Optionally, the unmanned water surface vehicle further comprises an onshore operation terminal, the controller is a mobile communication terminal with 4G communication, and the mobile communication terminal is in wireless connection with the onshore operation terminal;
The integrated functional module of controller includes control panel, magnetic compass, propeller drive plate, picture pass module, side scan sonar module and wireless mobile communication unit.
Optionally, a handle is arranged on the shell of the electric appliance cabin.
Optionally, a supporting rod is arranged between the bevel edge and the battery compartment, one end of the supporting rod is fixedly connected with the bevel edge of the trapezoid connecting frame, and the other end of the supporting rod is fixedly connected with the shell of the battery compartment.
Optionally, the head and the tail of the electric appliance cabin are in a round head shape.
The application has the beneficial effects that: according to the application, the electric appliance cabin, the battery cabin, the propeller and the floating block are fixedly arranged on the trapezoid connecting frame, and the electric appliance cabin and the battery cabin are respectively arranged at the upper end and the lower end of the trapezoid connecting frame, so that parts in the electric appliance cabin and the battery cabin are mutually independent, and when the battery in the battery cabin is dismounted or replaced, the parts in the electric appliance cabin are not damaged, and the service life of the aircraft is prolonged; the controller is installed in the electric appliance cabin, and the controller and the on-shore operation terminal are used for controlling and transmitting data to the aircraft, so that underwater detection operation is realized.
Drawings
FIG. 1 is a schematic view of the overall structure of the present application;
FIG. 2 is a top view of the present application;
FIG. 3 is a schematic view of a third embodiment of the present application;
Fig. 4 is a control diagram of the electrical compartment of the present application.
In the figure, a trapezoid connecting frame 1, an electric appliance cabin 2, a battery cabin 3, a propeller 4, a floating block 5, a side-scan sonar 6, a short side 11, a bevel edge 12, a supporting rod 13, a first U-shaped frame 21, a picture transmission antenna 22, a handle 23, a second U-shaped frame 31, a propeller shaft 41 and a propeller 42.
Detailed Description
In the description of the present invention, it should be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", "axial", "radial", "circumferential", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings are merely for convenience in describing the present invention and simplifying the description, and do not indicate or imply that the device or element being referred to must have a specific orientation, be configured and operated in a specific orientation, and therefore should not be construed as limiting the present invention.
Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defining "a first" or "a second" may explicitly or implicitly include at least one such feature. In the description of the present invention, the meaning of "plurality" means at least two, for example, two, three, etc., unless specifically defined otherwise.
In the present invention, unless explicitly specified and limited otherwise, the terms "mounted," "connected," "secured," and the like are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally formed; may be mechanically connected, may be electrically connected or may be in communication with each other; either directly or indirectly, through intermediaries, or both, may be in communication with each other or in interaction with each other, unless expressly defined otherwise. The specific meaning of the above terms in the present invention will be understood by those of ordinary skill in the art as the case may be.
In the present invention, unless expressly stated or limited otherwise, a first feature "up" or "down" a second feature may be the first and second features in direct contact, or the first and second features in indirect contact via an intervening medium. Moreover, a first feature being "above," "over" and "on" a second feature may be a first feature being directly above or obliquely above the second feature, or simply indicating that the first feature is level higher than the second feature. The first feature being "under", "below" and "beneath" the second feature may be the first feature being directly under or obliquely below the second feature, or simply indicating that the first feature is less level than the second feature.
In the present disclosure, the terms "one embodiment," "some embodiments," "examples," "specific examples," or "some examples," etc., mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the present disclosure. In this specification, schematic representations of the above terms are not necessarily directed to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples. Furthermore, the different embodiments or examples described in this specification and the features of the different embodiments or examples may be combined and combined by those skilled in the art without contradiction.
While embodiments of the present invention have been shown and described above, it will be understood that the above embodiments are illustrative and not to be construed as limiting the invention, and that variations, modifications, alternatives and variations may be made to the above embodiments by one of ordinary skill in the art within the scope of the invention.
The foregoing description of the preferred embodiments of the present application is not intended to limit the application, but is intended to cover all modifications, equivalents, alternatives, and improvements falling within the spirit and principles of the application.
In order to make the objects, technical solutions and advantageous effects of the present application more apparent, preferred embodiments of the present application will be described in detail below with reference to the accompanying drawings, so as to facilitate understanding of the skilled person.
Embodiment one:
Referring to fig. 1 and 2, a unmanned surface vehicle, comprising a controller (not shown in the figures), a trapezoid connecting frame 1 having a short side 11 and a sloping side 12, wherein the short side 11 is an upper bottom edge of the trapezoid connecting frame 1, and the unmanned surface vehicle is characterized in that: the unmanned water surface vehicle further comprises an electric cabin 2 arranged above the short side 11 of the trapezoid connecting frame 1, a battery cabin 3 arranged below the short side 11 of the trapezoid connecting frame 1 and positioned on the inner side of the inclined side 12 of the trapezoid connecting frame 1, a propeller 4 fixed at the bottom end of the inclined side 12 of the trapezoid connecting frame 1, and a floating block 5 positioned above the propeller 4 and fixed in the middle of the inclined side 12 of the trapezoid connecting frame 1;
A first U-shaped frame 21 is arranged between the electric appliance cabin 2 and the trapezoid connecting frame 1, the outer shell of the electric appliance cabin 2 is fixedly connected to the inner wall of the first U-shaped frame 21, and the upper end face of the short side 11 of the trapezoid connecting frame 1 is fixedly connected to the outer wall of the first U-shaped frame 21;
The first U-shaped frame 21 is used for fixing the electric appliance cabin 2 in the upper direction, the lower direction, the left direction and the right direction and limiting the position of the electric appliance cabin 2 on the trapezoid connecting frame 1, so that dislocation of the electric appliance cabin 2 during movement of the aircraft is avoided, and meanwhile, the overall structural strength of the aircraft can be enhanced;
Alternatively, the first U-shaped frame 21 is hollow in order to reduce the weight and volume of the aircraft.
The upper end of the electric cabin 2 is fixedly connected with a picture transmission antenna 22 for enhancing signals, and a controller is arranged in the electric cabin 2 and used for controlling the motion state of the aircraft and transmitting back images; the bottom of the electric appliance cabin 2 is also provided with a side-scan sonar 6 for detecting underwater structures and objects in water.
The image transmission antenna 22 is arranged at the top of the electric appliance cabin 2, the image transmission antenna 22 is higher than the water surface, the side scan sonar 6 can image the water surface, the obtained image data is transmitted to the controller, and the controller transmits the image data to the shore operation terminal through the image transmission antenna 22, so that a technician can acquire underwater image information.
A second U-shaped frame 31 is arranged between the battery compartment 3 and the trapezoid connecting frame 1, the outer shell of the battery compartment 3 is fixedly connected to the inner wall of the second U-shaped frame 31, and the lower end face of the short side 11 of the trapezoid connecting frame 1 is fixedly connected to the outer wall of the second U-shaped frame 31;
The second U-shaped frame 31 is used for fixing the battery compartment 3 in the upper direction, the lower direction, the left direction and the right direction and limiting the position of the battery compartment 3 on the trapezoid connecting frame 1, so that dislocation of the battery compartment 3 during movement of the aircraft is avoided, and meanwhile, the overall structural strength of the aircraft can be enhanced;
through setting up electrical apparatus cabin 2 and battery cabin 3 respectively in trapezoidal link 1's upper and lower both ends, make the cabin spare part mutual independence in electrical apparatus cabin 2 and the battery cabin 3, when dismantling or changing the battery in the battery cabin 3, can not lead to the fact the destruction to the spare part in the electrical apparatus cabin 2, increase the life of aircraft.
Optionally, the second U-shaped frame 31 is hollow in order to reduce the weight and volume of the aircraft.
At least one battery is arranged in the battery compartment 3, and the battery is electrically connected with the motor, the controller and the side-scan sonar of the propeller and provides electric energy for the motor, the controller and the side-scan sonar of the propeller.
The battery is a 24V/40AH ternary lithium battery, a power line of the battery is connected to watertight connectors of the electric appliance cabin 2 and the propeller 4, and one end of the watertight connectors is connected with a controller and a motor of the propeller 4 through wires; the junction of watertight connector, power cord, wire belongs to quick detach knot structure, can realize the quick dismantlement and the installation of battery.
Among them, the watertight connector, which is an electrical connector for waterproofing, is generally used in the environment such as outdoor and diving equipment, has a special design and material, and can effectively prevent water and moisture from entering the inside of the connector, thereby protecting the safe operation of the electronic equipment.
Embodiment two:
referring to fig. 1 and 2, the horizontal central axis of the electric compartment 2 and the horizontal central axis of the battery compartment 3 are located on the same vertical plane.
The horizontal central axis of the electric cabin 2 and the horizontal central axis of the battery cabin 3 are arranged on the same vertical plane, so that the left and right weight distribution of the aircraft is ensured to be uniform, and the stability of movement is improved.
The propeller 4 includes two groups, each group of the propeller 4 including a propeller shaft 41 and a propeller 42, and the direction of propulsion of the propeller 4 is changed by adjusting the angle of the propeller 42.
The motor of the propeller 4 is connected with the propeller shaft 41, the motor drives the propeller shaft 41 to rotate, and the propeller shaft 41 drives the propeller 42 to rotate.
The bevel edges 12 are divided into two groups, the two groups of bevel edges 12 are symmetrically arranged by taking the vertical central line of the short edge 11 as a symmetrical axis, and the two groups of propellers 4 are respectively fixed at the bottom ends of the two groups of bevel edges 12.
The two groups of propellers 4 are symmetrically arranged, and the bottom ends of the two groups of propellers 4 are positioned on the same horizontal plane, so that the left and right weight distribution of the aircraft is uniform, and the stability of movement is improved.
The floating block 5 comprises two groups, which are respectively fixed at the middle parts of the two groups of bevel edges 12 and are used for providing buoyancy for the aircraft.
Alternatively, the floating block 5 is made of polyurethane foam material, and the surface of the polyurethane foam material is completely wrapped by plastic film so as to be isolated from water.
Alternatively, the float 5 is made of a copolymer foam material, and the copolymer foam cross-linked copolymer foam is a rigid closed cell foam, and when this material is used, the float 5 is provided in a block shape or a sheet shape.
Alternatively, the floating blocks 5 are made of a composite foam material, which is the latest generation of floating block materials, and has the advantage of maintaining sufficient strength at very low density, and having the characteristics of high compression strength to weight ratio, low creep and low water absorption.
Alternatively, the shape of the floating block 5 may be a block shape or a cylinder shape.
The unmanned water surface vehicle further comprises an onshore operation terminal, the controller is a mobile communication terminal with 4G communication, and the mobile communication terminal is in wireless connection with the onshore operation terminal;
The on-shore operation terminal is an independent power supply mobile communication terminal similar to the controller, and is in wireless connection with the controller through a 4G network so as to remotely control and transmit data to the aircraft.
The integrated functional module of controller includes control panel, magnetic compass, propeller drive plate, picture pass module, side scan sonar module and wireless mobile communication unit.
Optionally, the shore operation terminal and the controller can be in wireless connection through wifi, and a wifi communication unit is additionally arranged in the controller at the moment.
The control flow of the electric appliance cabin 2 is as follows: the shore operation terminal carries out remote control on a control board of the controller through 4G mobile communication, the control board further controls the side scan sonar 6 to detect surrounding water areas, image data of the side scan sonar 6 is transmitted back to a picture transmission module of the controller, and the picture transmission module transmits the image data to the shore operation terminal through a picture transmission antenna 22.
The on-shore operation terminal remotely controls the control panel through 4G mobile communication, the control panel controls the magnetic compass to calculate the heading, and when the magnetic compass finishes the heading calculation operation, calculation data of the magnetic compass is transmitted to the on-shore operation terminal through 4G mobile communication.
The control panel of controller is carried out remote control to the operation terminal on shore through 4G mobile communication, the control panel sends the instruction to the propeller drive plate, the motor output of propeller 4 and the angle of screw 42 are controlled to propeller drive plate to control the control of propeller 4 turn left and right, the back and forth, and the speed of a ship, in this control process, the control of propeller 4 receives the influence of course calculation data, according to course calculation data with the angle of adjustment screw 42, thereby adjust the navigation gesture of aircraft, in the whole control process, control signal's emission is accomplished by operation terminal on shore, after the controller received the signal, the operation of control side scan sonar 6, propeller 4 and magnetic compass again.
The magnetic compass measures the space attitude angle by utilizing the inherent directivity of the geomagnetic field, and can measure the three-dimensional attitude data of the carrier: horizontal heading, pitch and roll.
The side-scan sonar 6 has high imaging resolution, can realize full-coverage side-scan on a target area water area, and can perform qualitative analysis on underwater topography, and the like.
The outer shell of the electric appliance cabin 2 is provided with a handle 23.
The rapid transfer task of the aircraft is realized by moving the aircraft through the handle 23.
A supporting rod 13 is arranged between the inclined edge 12 and the battery compartment 3, one end of the supporting rod 13 is fixedly connected with the inclined edge 12 of the trapezoid connecting frame 1, and the other end is fixedly connected with the shell of the battery compartment 3.
The supporting rods 13 are divided into two groups, are symmetrically arranged on two sides of the battery compartment 3, are used for limiting the position of the battery compartment 3 and giving a certain supporting force to the bevel edge 12, and are of hollow structures for reducing the weight of the aircraft.
The head and the tail of the electric appliance cabin 2 are in a round head shape.
When the round head modeling is adopted, the internal volume of the electric appliance cabin 2 is effectively increased, so that more parts can be conveniently installed, and the functions of the electric appliance cabin are expanded.
Embodiment III:
Referring to fig. 3 and 4, the head and tail of the electric cabin 2 may also be designed in a pointed shape to reduce movement resistance, thereby saving electric energy and increasing the endurance time of the battery.
The control board of the controller is arranged in the middle of the electric appliance cabin 2, and the magnetic compass is arranged at the front end of the electric appliance cabin 2 so as to prevent electromagnetic interference; the propeller driving plate, the image transmission module and the side scan sonar module are all arranged at the tail section of the electric appliance cabin 2.
The control panel reads the current heading and deflection angle of the water surface aircraft measured by the magnetic compass, transmits the current heading and deflection angle to the on-shore operation terminal through 4G mobile communication, and sends a target instruction to the propeller driving plate according to the measurement data of the magnetic compass so as to adjust the propeller angle of the propeller 4, thereby controlling the direction of the left and right propellers 4 and further realizing the steering, advancing and retreating functions of the heading machine; the shore operation terminal sends a target instruction to the control panel to control the side sonar 6 to detect the surrounding water area, real-time image data detected by the side sonar 6 is transmitted to the image transmission module, and the image transmission module transmits the data to the shore terminal through the image transmission antenna 22 to realize remote image transmission, so that the water area remote detection function is completed.
According to the application, the electric appliance cabin 2, the battery cabin 3, the propeller 4 and the floating block 5 are fixedly arranged on the trapezoid connecting frame 1, and the electric appliance cabin 2 and the battery cabin 3 are respectively arranged at the upper end and the lower end of the trapezoid connecting frame 1, so that parts in the electric appliance cabin 2 and the battery cabin 3 are mutually independent, and when a battery in the battery cabin 3 is dismounted or replaced, the parts in the electric appliance cabin 2 are not damaged, and the service life of the aircraft is prolonged; the controller is installed in electrical cabin 2, controls and data transmission to the aircraft through controller and on-shore operation terminal to this realizes the underwater detection operation, and this device simple structure and the connected mode between the cabin body are simple, and the component layout of aircraft is reasonable, easily makes.
Finally, it is noted that the above-mentioned preferred embodiments illustrate rather than limit the application, and that, although the application has been described in detail with reference to the above-mentioned preferred embodiments, it will be understood by those skilled in the art that various changes in form and details may be made therein without departing from the scope of the application as defined by the appended claims; the size of the drawing is irrelevant to the specific real object, and the real object size can be changed arbitrarily.
Claims (9)
1. The utility model provides an unmanned vehicles of surface of water, includes the controller, has the trapezoidal link of minor face and hypotenuse, the minor face is the last base of trapezoidal link, its characterized in that: the unmanned water surface vehicle further comprises an electric appliance cabin arranged above the short side of the trapezoid connecting frame, a battery cabin arranged below the short side of the trapezoid connecting frame and positioned on the inner side of the bevel edge of the connecting frame, a propeller fixed at the bottom end of the bevel edge of the trapezoid connecting frame, and a floating block positioned above the propeller and fixed in the middle of the bevel edge of the trapezoid connecting frame;
A first U-shaped frame is arranged between the electric appliance cabin and the trapezoid connecting frame, an outer shell of the electric appliance cabin is fixedly connected to the inner wall of the first U-shaped frame, and the upper end face of the short side of the trapezoid connecting frame is fixedly connected with the outer wall of the first U-shaped frame;
The upper end of the electric appliance cabin is fixedly connected with a graphic transmission antenna for enhancing signals, and a controller is arranged in the electric appliance cabin and used for controlling the motion state of the aircraft and returning images; the bottom of the electric appliance cabin is also provided with a side-scan sonar for detecting underwater structures and objects in water;
A second U-shaped frame is arranged between the battery compartment and the trapezoid connecting frame, the outer shell of the battery compartment is fixedly connected to the inner wall of the second U-shaped frame, and the lower end face of the short side of the trapezoid connecting frame is fixedly connected with the outer wall of the second U-shaped frame;
At least one battery is arranged in the battery compartment, and the battery is electrically connected with the motor of the propeller and the controller.
2. The unmanned surface vehicle of claim 1, wherein: the horizontal central axis of the electric appliance cabin and the horizontal central axis of the battery cabin are positioned on the same vertical plane.
3. The unmanned surface vehicle of claim 1, wherein: the propeller comprises two groups, each group of the propeller comprises a propeller shaft and a propeller, and the propelling direction of the propeller is changed by adjusting the angle of the propeller.
4. The unmanned surface vehicle of claim 1, wherein: the bevel edges are divided into two groups, the two groups of bevel edges are symmetrically arranged by taking the vertical central line of the short edge as a symmetrical axis, and the two groups of propellers are respectively fixed at the bottom ends of the two groups of bevel edges.
5. The unmanned surface vehicle of claim 1, wherein: the floating blocks comprise two groups, and are respectively fixed in the middle parts of the two groups of inclined edges and used for providing buoyancy for the aircraft.
6. The unmanned surface vehicle of claim 1, wherein: the unmanned water surface vehicle further comprises an onshore operation terminal, the controller is a mobile communication terminal with 4G communication, and the mobile communication terminal is in wireless connection with the onshore operation terminal;
The integrated functional module of controller includes control panel, magnetic compass, propeller drive plate, picture pass module, side scan sonar module and wireless mobile communication unit.
7. The unmanned surface vehicle of claim 1, wherein: a handle is arranged on the shell of the electric appliance cabin.
8. The unmanned surface vehicle of claim 1, wherein: a supporting rod is arranged between the bevel edge and the battery compartment, one end of the supporting rod is fixedly connected with the bevel edge of the trapezoid connecting frame, and the other end of the supporting rod is fixedly connected with the shell of the battery compartment.
9. The unmanned surface vehicle of claim 1, wherein: the head and the tail of the electric appliance cabin are in round head shapes.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323426291.4U CN221251732U (en) | 2023-12-15 | 2023-12-15 | Unmanned vehicle on water surface |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323426291.4U CN221251732U (en) | 2023-12-15 | 2023-12-15 | Unmanned vehicle on water surface |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN221251732U true CN221251732U (en) | 2024-07-02 |
Family
ID=91653050
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202323426291.4U Active CN221251732U (en) | 2023-12-15 | 2023-12-15 | Unmanned vehicle on water surface |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN221251732U (en) |
-
2023
- 2023-12-15 CN CN202323426291.4U patent/CN221251732U/en active Active
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