CN111717408A - Marine launching platform capable of bearing multiple unmanned aerial vehicles - Google Patents
Marine launching platform capable of bearing multiple unmanned aerial vehicles Download PDFInfo
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- CN111717408A CN111717408A CN202010603102.8A CN202010603102A CN111717408A CN 111717408 A CN111717408 A CN 111717408A CN 202010603102 A CN202010603102 A CN 202010603102A CN 111717408 A CN111717408 A CN 111717408A
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- aerial vehicle
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/007—Helicopter portable landing pads
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Abstract
The utility model provides a can bear marine transmission platform of a plurality of unmanned aerial vehicle, belongs to unmanned aerial vehicle work platform technical field. Can bear a plurality of unmanned aerial vehicle's marine launching platform includes the base and sets up in safety cover, multistage stop device and the unmanned aerial vehicle transmission runway of base, and the safety cover is provided with emission window for launch unmanned aerial vehicle, multistage stop device loop through revolution mechanic and elevating system with the base is connected, multistage stop device includes the fixed axle and sets firmly in a plurality of machine halt positions of fixed axle for park unmanned aerial vehicle, unmanned aerial vehicle transmission runway pass through angle adjusting structure with the base is connected, angle adjusting structure is used for adjusting unmanned aerial vehicle transmission runway inclination. The marine launching platform capable of bearing the plurality of unmanned aerial vehicles can provide space for parking of the plurality of unmanned aerial vehicles, the number of the unmanned aerial vehicles borne by the unmanned aerial vehicle launching platform is effectively increased, the cost is reduced, and resources are saved.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle working platforms, in particular to an offshore launching platform capable of bearing a plurality of unmanned aerial vehicles.
Background
The territorial sea area is vast in China, the coastline is long, a large number of resources are owned by the wide sea, and the cost is high, the period is long, and the feasibility is lacked when ocean resources are searched by means of manual cruising. The research of ocean resource utilizes artificial mode to be not enough far away, still need adopt unmanned aerial vehicle to explore ocean resource, but current most unmanned aerial vehicle launching platform only can launch single unmanned aerial vehicle at every turn, and this makes the detection efficiency of ocean resource receive very big restriction. Therefore, there is an urgent need for a launch platform that can carry multiple drones for use by enterprises, colleges, research institutions, and the military.
Disclosure of Invention
In order to solve the technical problems in the prior art, the invention provides an offshore launching platform capable of bearing a plurality of unmanned aerial vehicles, which can provide space for parking of the unmanned aerial vehicles, effectively increases the number of the unmanned aerial vehicles borne by the unmanned aerial vehicle launching platform, reduces the cost and saves resources.
In order to achieve the purpose, the technical scheme of the invention is as follows:
a marine launching platform capable of bearing a plurality of unmanned aerial vehicles comprises a base, a protective cover arranged on the base, a multi-stage stopping device and an unmanned aerial vehicle launching runway;
the protective cover is provided with a transmitting window for transmitting the unmanned aerial vehicle;
the multi-stage stopping device is connected with the base through a rotating structure and a lifting mechanism in sequence, and comprises a fixed shaft and a plurality of stopping positions fixedly arranged on the fixed shaft and used for stopping the unmanned aerial vehicle;
the unmanned aerial vehicle launches the runway pass through angle modulation structure with the base is connected, angle modulation structure is used for adjusting unmanned aerial vehicle launches runway inclination.
Furthermore, the base and the protective cover are of an integrally formed flying saucer-shaped structure and are used for enabling the marine launching platform to stably float on the sea, and control on the sea is facilitated.
Further, the rotating structure comprises a motor and a rotating shaft which are connected with each other, and the rotating shaft is fixedly connected with the fixed shaft.
Furthermore, the lifting mechanism adopts an electric push rod, the electric push rod is fixedly connected with the base, and the extending end of the electric push rod is fixedly connected with the motor.
Further, the specific arrangement mode that a plurality of machine stopping positions are fixedly arranged on the fixed shaft is as follows: a plurality of shutdown layers are arranged along the longitudinal direction of the fixed shaft, and a plurality of shutdown positions are arranged on each shutdown layer along the circumferential direction of the fixed shaft.
Preferably, a plurality of the stand positions are uniformly arranged along the circumferential direction of the fixed shaft.
Furthermore, the angle adjusting structure adopts a pulley block, and the unmanned aerial vehicle launching runway is connected with a base fixedly arranged on the base through the pulley block.
Further, the base still is provided with the protection pad, the protection pad is located the base upper surface in the terminal outside of unmanned aerial vehicle transmission runway.
The invention has the beneficial effects that:
1) according to the invention, a plurality of parking positions are connected through a fixed shaft to form a multi-stage parking device, the multi-stage parking device is used for providing parking positions for a plurality of unmanned aerial vehicles, so that the multi-stage parking of the unmanned aerial vehicles is realized, the number of the unmanned aerial vehicles which can be borne by an unmanned aerial vehicle launching platform is effectively increased, the number of the unmanned aerial vehicle launching platforms is reduced, a plurality of unmanned aerial vehicles are launched by using the same platform, the cost of an ocean resource exploration application process is reduced, the search radius of ocean resource development and exploration work is increased, the monitoring radius of the ocean monitoring work process is enlarged, a guarantee is provided for further exploring the ocean resources, and the pace of ocean resource development and utilization is accelerated;
2) the multi-stage stopping device is lifted by utilizing the expansion of the electric push rod, so that the unmanned aerial vehicle at each level can be launched;
3) the motor drives the rotating shaft to rotate so as to realize the rotation of the multi-stage stopping device, and the unmanned aerial vehicle on each surface of the multi-stage stopping device can be ensured to realize normal launching;
4) the inclination angle of the launching runway of the unmanned aerial vehicle is adjusted through rotation of the pulley block, so that the launching inclination angle of the unmanned aerial vehicle is adjusted;
5) the unmanned aerial vehicle launching platform is protected by the protective cover, the protective cover can block the external severe conditions, the damage to equipment on the launching platform and the interference to the operation of the unmanned aerial vehicle launching platform caused by the external severe conditions are prevented, the launching window arranged on the protective cover can ensure the normal launching of the unmanned aerial vehicle, the window is opened, the unmanned aerial vehicle launching operation is realized, and when the unmanned aerial vehicle launching is not needed, the window is closed, and the protection operation of the unmanned aerial vehicle launching platform is realized;
6) the protection pad can bear the impact of falling of the unmanned aerial vehicle, and the unmanned aerial vehicle and the launching platform are not damaged.
Additional features and advantages of the invention will be set forth in part in the detailed description which follows.
Drawings
Fig. 1 is a front view of an offshore launching platform capable of carrying a plurality of drones according to an embodiment of the present invention;
fig. 2 is a left side view of an offshore launching platform capable of carrying a plurality of drones according to an embodiment of the present invention;
fig. 3 is a top view of an offshore launching platform capable of carrying multiple drones according to an embodiment of the present invention.
Reference numerals in the drawings of the specification include:
1-fixed shaft, 2-protective cover, 3-base, 4-protective pad, 5-base, 6-unmanned aerial vehicle launching runway, 7-pulley block, 8-multistage stopping device, 9-electric push rod, 10-extending end, 11-motor, 12-rotating shaft, 13-launching window, and 14-stopping position.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments.
In the description of the present invention, it is to be understood that the terms "longitudinal", "lateral", "vertical", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", etc., indicate orientations or positional relationships based on those shown in the drawings, and are used only for convenience in describing the present invention and for simplicity in description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention.
In the description of the present invention, unless otherwise specified and limited, it is to be noted that the terms "mounted," "connected," and "connected" are to be interpreted broadly, and may be, for example, a mechanical connection or an electrical connection, a communication between two elements, a direct connection, or an indirect connection via an intermediate medium, and specific meanings of the terms may be understood by those skilled in the art according to specific situations.
As shown in fig. 1 to 3, the invention provides an offshore launching platform capable of bearing a plurality of unmanned aerial vehicles, which comprises a base 3, a protective cover 2 arranged on the base 3, a multi-stage stopping device 8 and an unmanned aerial vehicle launching runway 6;
the protective cover 2 is provided with a launching window 13 for launching the unmanned aerial vehicle;
the multi-stage stopping device 8 is connected with the base 3 sequentially through the rotating structure and the lifting mechanism, and the multi-stage stopping device 8 comprises a fixed shaft 1 and a plurality of stopping positions 14 fixedly arranged on the fixed shaft 1 and used for stopping the unmanned aerial vehicle;
unmanned aerial vehicle launching runway 6 is connected with base 3 through angle modulation structure, and angle modulation structure is used for adjusting 6 inclination of unmanned aerial vehicle launching runway.
In the invention, a fixed shaft 1 is fixedly connected with each stand 14 to form an integral multi-stage stop device 8; the rotating structure comprises a motor 11 and a rotating shaft 12 which are connected with each other, and the rotating shaft 12 is fixedly connected with the fixed shaft 1; the lifting mechanism adopts an electric push rod 9, the electric push rod 9 is fixedly connected with the base 3, and an extending end 10 of the electric push rod 9 is fixedly connected with a motor 11. The multi-stage stopping device 8 can provide space for the stopping of the unmanned aerial vehicles, and marine launching of the unmanned aerial vehicles is realized through the functions of a rotating structure and a lifting mechanism, wherein the lifting process is controlled through the electric push rod 9, the electric push rod 9 is driven by electricity, the thrust provided by the electric push rod 9 can meet the lifting work of the multi-stage stopping device 8, and the stopping position 14 where the unmanned aerial vehicle to be launched is located and the unmanned aerial vehicle launching runway 6 are located at the same height; the end 10 that stretches out of electric putter 9 is provided with motor 11, and motor 11 is the power supply of rotation axis 12, and drive rotation axis 12 rotates, and rotation axis 12 drives fixed axle 1 that has linked firmly a plurality of shut-off positions 14 and rotates, makes the shut-off position 14 at transmission unmanned aerial vehicle place correspond the butt joint with unmanned aerial vehicle transmission runway 6 positions, ensures that the unmanned aerial vehicle homoenergetic on 8 each face shut-off positions of multistage stop device 14 can realize normal transmission.
The base 3 and the protective cover 2 are of an integrally formed flying saucer-shaped structure and are used for enabling the launching platform on the sea to stably float on the sea and facilitating control on the sea, wherein the base 3 is used as a carrier of other equipment on the launching platform of the unmanned aerial vehicle and placed in the sea to ensure that the launching platform of the unmanned aerial vehicle floats on the sea; the protective cover 2 can prevent equipment on the platform from being damaged due to complex sea surface conditions, the protective cover 2 is provided with the launching window 13, and when the launching platform does not carry out unmanned aerial vehicle launching work, the launching window 13 is closed to protect the unmanned aerial vehicle launching platform; when needing to carry out unmanned aerial vehicle transmission work, transmission window 13 is opened, guarantees unmanned aerial vehicle normal transmission. In this embodiment, the protective cover 2 is an outdoor spherical safety protective cover, and may be an aluminum material or a steel plate with a coating, so that the protective cover does not suffer from strength reduction or cracking under the condition of ultraviolet irradiation, and in order to ensure the safety of the protective cover 2, the protective cover may be further enhanced in its ability to resist external adverse environments by using a polyurethane baking varnish, anodic oxidation, and anodic oxidation plus painting methods.
The specific arrangement mode that a plurality of stands 14 are fixed on the fixed shaft 1 is as follows: a plurality of parking levels are arranged along the longitudinal direction of the fixed shaft 1, and each parking level is provided with a plurality of parking positions 14 along the circumferential direction of the fixed shaft 1. In this embodiment, the fixed shaft 1 is provided with two shutdown layers, each shutdown layer is provided with four shutdown positions 14, and the shutdown layers are uniformly arranged on four surfaces of the fixed shaft 1. Preferably, the plurality of stands 14 are uniformly arranged along the circumferential direction of the stationary shaft 1.
The angle modulation structure adopts assembly pulley 7, and unmanned aerial vehicle launching runway 6 is connected through assembly pulley 7 with the base 5 that sets firmly in base 3. Multistage arrester (-tor) 8 need utilize unmanned aerial vehicle transmission runway 6 to provide the place for the unmanned aerial vehicle transmission process in the unmanned aerial vehicle transmission process, ensure that unmanned aerial vehicle can realize normal transmission, unmanned aerial vehicle transmission runway 6 is located one side of multistage arrester (-tor) 8, it links to each other with base 5 through rotatory assembly pulley 7, base 5 links firmly with base 3 and keeps relative static, rotate the regulation that realizes unmanned aerial vehicle transmission runway 6 angle through assembly pulley 7, and then realize unmanned aerial vehicle transmission angle's regulation, unmanned aerial vehicle transmission runway 6's length sets up according to actual conditions, its length is enough unmanned aerial vehicle to take off.
The invention relates to a working process of an offshore launching platform capable of bearing a plurality of unmanned aerial vehicles, which comprises the following steps:
starting an electric push rod 9, and adjusting a stand 14 where the unmanned aerial vehicle to be launched is located to be at the same height as the unmanned aerial vehicle launching runway 6; starting a motor 11, driving a rotating shaft 12 to rotate, and adjusting a stand 14 where the unmanned aerial vehicle to be launched is located to a position corresponding to the unmanned aerial vehicle launching runway 6; adjusting the inclination angle of the unmanned aerial vehicle launching runway 6 to a set angle through a rotating pulley block 7 according to the launching angle of the unmanned aerial vehicle; opening an emission window 13 of the protective cover 2 and emitting the unmanned aerial vehicle; and entering the next unmanned aerial vehicle launching process according to the set searching or monitoring radius.
When the device is actually used, the opening and closing of the emission window 13 of the protective cover 2, the lifting and rotating of the multi-stage stopping device 8 and the inclination angle of the unmanned aerial vehicle emission runway 6 can be automatically controlled by the single chip microcomputer; unmanned aerial vehicle transmitting process is controlled by the computer, and the computer can control unmanned aerial vehicle's transmission, retrieve and motion state, and the computer can give an instruction to unmanned aerial vehicle after unmanned aerial vehicle transmission succeeds, controls unmanned aerial vehicle and does all kinds of movements such as straight line, circumference and acceleration and deceleration.
While embodiments of the invention have been shown and described, it will be understood by those of ordinary skill in the art that: various changes, modifications, substitutions and alterations can be made to the embodiments without departing from the principles and spirit of the invention, the scope of which is defined by the claims and their equivalents.
Claims (8)
1. A marine launching platform capable of bearing a plurality of unmanned aerial vehicles is characterized by comprising a base, a protective cover arranged on the base, a multi-stage stopping device and an unmanned aerial vehicle launching runway;
the protective cover is provided with a transmitting window for transmitting the unmanned aerial vehicle;
the multi-stage stopping device is connected with the base through a rotating structure and a lifting mechanism in sequence, and comprises a fixed shaft and a plurality of stopping positions fixedly arranged on the fixed shaft and used for stopping the unmanned aerial vehicle;
the unmanned aerial vehicle launches the runway pass through angle modulation structure with the base is connected, angle modulation structure is used for adjusting unmanned aerial vehicle launches runway inclination.
2. The marine launch platform of claim 1, wherein the base and the protective cover are of an integrally formed flying saucer shaped configuration.
3. The marine launch platform capable of carrying a plurality of drones according to claim 1, wherein said rotating structure comprises an interconnected motor and a rotating shaft, said rotating shaft being secured to said fixed shaft.
4. The offshore launching platform capable of carrying a plurality of unmanned aerial vehicles according to claim 3, wherein the lifting mechanism employs an electric push rod, the electric push rod is fixedly connected with the base, and an extending end of the electric push rod is fixedly connected with the motor.
5. The offshore launching platform capable of carrying multiple drones according to claim 1, wherein the specific arrangement of the plurality of parking places fixed on the fixed shaft is as follows: a plurality of shutdown layers are arranged along the longitudinal direction of the fixed shaft, and a plurality of shutdown positions are arranged on each shutdown layer along the circumferential direction of the fixed shaft.
6. The offshore launch platform capable of carrying a plurality of drones according to claim 5, wherein a plurality of said stands are uniformly disposed along the circumference of the stationary shaft.
7. The offshore launching platform capable of carrying a plurality of unmanned aerial vehicles according to claim 1, wherein the angle adjustment structure employs a pulley block, and the unmanned aerial vehicle launching runway is connected with a base fixed on the base through the pulley block.
8. The offshore launch platform capable of carrying a plurality of drones according to claim 1, wherein said base is further provided with a protective pad located on the upper surface of the base outside the end of the drone launch runway.
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| Application Number | Priority Date | Filing Date | Title |
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| CN202010603102.8A CN111717408A (en) | 2020-06-29 | 2020-06-29 | Marine launching platform capable of bearing multiple unmanned aerial vehicles |
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| CN202010603102.8A CN111717408A (en) | 2020-06-29 | 2020-06-29 | Marine launching platform capable of bearing multiple unmanned aerial vehicles |
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| CN111717408A true CN111717408A (en) | 2020-09-29 |
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| CN202010603102.8A Pending CN111717408A (en) | 2020-06-29 | 2020-06-29 | Marine launching platform capable of bearing multiple unmanned aerial vehicles |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112623132A (en) * | 2020-12-25 | 2021-04-09 | 山东科技大学 | Offshore platform capable of recycling unmanned aerial vehicle |
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| CN112623132A (en) * | 2020-12-25 | 2021-04-09 | 山东科技大学 | Offshore platform capable of recycling unmanned aerial vehicle |
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Application publication date: 20200929 |