CN218401013U

CN218401013U - Unmanned aerial vehicle takes off and land balanced and fixed locking platform

Info

Publication number: CN218401013U
Application number: CN202222601269.8U
Authority: CN
Inventors: 汤伟; 辛卓; 高亮亮; 马斌斌; 邢景峰
Original assignee: Individual
Current assignee: Individual
Priority date: 2022-09-30
Filing date: 2022-09-30
Publication date: 2023-01-31
Anticipated expiration: 2032-09-30

Abstract

The utility model discloses an unmanned aerial vehicle balance and fixed locking platform that takes off and land, including the deck of taking off and land, balanced support and support frame, the first pivot of both ends middle part fixed connection of the deck of taking off and land, first pivot is connected with the inner wall rotation of balanced support, the both ends middle part fixed connection of balanced support has the second pivot, the second pivot is rotated with the top of support frame and is connected, the solid fixed ring of bottom fixedly connected with of support frame, fixedly connected with floats the flotation pontoon in the fixation ring, the equal fixedly connected with fixing rope in the six angle departments in bottom on the deck of taking off and land, the isometric setting of fixing rope and one end fixedly connected with balancing weight, the bottom on the deck of taking off and land is provided with electro-magnet and U type locking hook structure, the utility model relates to a field. This kind of unmanned aerial vehicle take off and land balance and fixed locking platform has realized rocking the restriction with the place of taking off and land at the surface of water by the hull, and unmanned aerial vehicle can steady take off and land.

Description

Unmanned aerial vehicle takes off and land balanced and fixed locking platform

Technical Field

The utility model relates to an unmanned aerial vehicle application technology field specifically is an unmanned aerial vehicle balance and fixed locking platform of taking off and land.

Background

When the unmanned aerial vehicle takes off and lands, certain requirements are provided for the supporting surface of the unmanned aerial vehicle. The unmanned aerial vehicle is used on the ship and needs to be supported, if the ship is a large ship, the ship is provided with an open deck, the deck can be used as flat ground, and the unmanned aerial vehicle can take off and land after being placed, and if the ship is a speed boat or a sailing boat, the bow of the ship is narrow, and even a ship with a mast, a sail and dense ropes cannot find an empty ground to take off. Because the ship is small and shakes seriously, the balance of the ship and the take-off of the airplane are both kept, and the ship is easy to go out without paying attention to the airplane and brings potential safety hazards.

SUMMERY OF THE UTILITY MODEL

In order to solve the defects, the utility model provides an unmanned aerial vehicle takes off and land balanced and fixed locking platform has realized not rocking the restriction with the place of taking off and land by the hull at the surface of water, and unmanned aerial vehicle can steady take off and land.

In order to realize the above-mentioned purpose, the utility model provides a technical scheme does, an unmanned aerial vehicle balance and fixed locking platform that takes off and land, including the deck of taking off and land, balanced support and support frame, the deck of taking off and land is the hexagon structure, the first pivot of the both ends middle part fixedly connected with of the deck of taking off and land, first pivot is connected with the inner wall rotation of balanced support, the both ends middle part fixedly connected with second pivot of balanced support, the second pivot is rotated with the top of support frame and is connected, the solid fixed ring of bottom fixedly connected with of support frame, fixedly connected with floats the flotation pontoon in the fixation ring, float the support frame that the support frame both sides are connected to the flotation pontoon, the equal fixedly connected with fixed rope in bottom six angle departments of the deck of taking off and land, the isometric setting of fixed rope and one end fixedly connected with balancing weight, the balancing weight is located the below of the deck center of taking off and land, the surface symmetry of the deck of taking off and land is provided with the location sign and corresponds the position and is provided with electro-magnet and U type locking hook claw structure, the surface of the deck of taking off and land is provided with the perforation with U type locking hook claw structure adaptation.

Preferably, the bottom of the lifting deck is further provided with an electric telescopic rod and a fixed pulley, the working end of the electric telescopic rod is fixedly connected with a traction rope, and one end of the traction rope is wound around the surface of the fixed pulley and is fixedly connected with one end of the U-shaped locking claw structure.

Preferably, the electromagnets are arranged in pairs, the tops of the electromagnets extend to the surface of the lifting deck, and the U-shaped locking claw structure is located between the two electromagnets on the same side.

Preferably, the first rotating shaft is rotatably connected with the balance support through a bearing, and the second rotating shaft is rotatably connected with the support frame through a bearing.

Preferably, the top of the lifting deck and the positions close to the first rotating shaft and the second rotating shaft are provided with monitoring lenses.

Preferably, U type locking hook structure includes the barrel, the barrel is provided with two and fixes the bottom at the deck of taking off and land, be provided with the direction baffle in the barrel, the direction baffle is provided with two and middle part sliding connection has the connecting rod, the top fixedly connected with U type mount of connecting rod, the flexible electromagnetic lock of one side fixedly connected with of U type mount, the bottom fixedly connected with limiting plate of connecting rod, fixedly connected with dead lever between two limiting plates of both sides, the one end of haulage rope and the middle part fixed connection of dead lever, be provided with the spring between the top of limiting plate and the direction baffle.

Preferably, the fixed pulley is positioned right above the fixed rod.

The utility model adopts the above technical scheme, beneficial effect includes: float the flotation pontoon and the support frame has guaranteed through setting up that the device can float at the surface of water, has guaranteed the steady of deck of taking off and landing through balanced support, first pivot, second pivot and balancing weight, has further improved the fixed to unmanned aerial vehicle through electro-magnet and U type locking hook claw structure simultaneously, effectual solution unmanned aerial vehicle is because the hull rocks and takes off and land the limited problem in place, thereby guarantee unmanned aerial vehicle and operating personnel's safety, thereby avoid bringing the unnecessary loss.

Drawings

FIG. 1 is a first schematic structural diagram of the present invention;

FIG. 2 is a second schematic structural view of the present invention;

FIG. 3 is a side view of the structure of the present invention;

fig. 4 is a schematic structural view of the U-shaped locking claw structure of the present invention;

fig. 5 is the working state schematic diagram of the U-shaped locking claw structure of the present invention.

In the figure: 1-lifting deck, 2-balance support, 3-first rotating shaft, 4-support frame, 5-second rotating shaft, 6-fixing ring, 7-floating buoy, 8-fixing rope, 9-balancing weight, 10-electromagnet, 11-U-shaped locking claw structure, 111-cylinder, 112-guide partition plate, 113-connecting rod, 114-U-shaped fixing frame, 115-telescopic electromagnetic lock, 116-limiting plate, 117-fixing rod, 118-spring, 12-perforation, 13-electric telescopic rod, 14-fixed pulley, 15-traction rope, 16-lifting location mark and 17-monitoring lens.

Detailed Description

The present invention will be further described with reference to the accompanying drawings.

The first embodiment is as follows: referring to fig. 1-5, the present invention provides a technical solution: the utility model provides an unmanned aerial vehicle balance and fixed locking platform that takes off and land, including deck 1 that takes off and land, balance support 2 and support frame 4, be applicable to the unmanned aerial vehicle that has the ironbar on the undercarriage, deck 1 that takes off and land is the hexagon structure, the first pivot 3 of both ends middle part fixedly connected with of deck 1 that takes off and land, first pivot 3 rotates with the inner wall of balance support 2 to be connected, the both ends middle part fixedly connected with second pivot 5 of balance support 2, second pivot 5 rotates with the top of support frame 4 to be connected, rotate through the bearing between first pivot 3 and the balance support 2 to be connected, rotate through the bearing between second pivot 5 and the support frame 4 and be connected, the equal fixedly connected with fixed rope 8 in the bottom six angle departments of deck 1 that takes off and land, the isometric setting of fixed rope 8 and one end fixedly connected with balancing weight 9, balancing weight 9 is located the below at deck 1 center that takes off and land, the principle that utilizes the spirit level has guaranteed that deck 1 that takes off and land all the time keeps the horizontal position, balancing weight 9 adopts solid iron ball or lead ball, utilize the central downward centrobaric principle of deck 1 that takes off and land to offset the balanced all the water surface factor all the gravity of the platform that takes off and land under the circumstances that the platform rocks.

The solid fixed ring 6 of bottom fixedly connected with of support frame 4, gu fixed ring 6 is connected with the support frame 4 is detachable, gu fixed ring 6 internal fixation connected with floats flotation pontoon 7, support frame 4 of 2 both sides of balanced support is connected to a float section of thick bamboo 7, the buoyancy of a float section of thick bamboo 7 is enough to support whole platform, guaranteed through a float section of thick bamboo 7 that the device can float at the surface of water, be applicable to the surface of water operation, guaranteed rock at the hull and still can provide stable platform of taking off and land for unmanned aerial vehicle under the limited circumstances in place of taking off and land.

The surperficial symmetry of deck 1 that takes off and land is provided with location sign 16 that rises and lands, distance between two location signs 16 that rise and land equals with the distance between the unmanned aerial vehicle foot, the bottom of deck 1 that takes off and land and be located the location sign 16 that rises and lands and correspond the position and be provided with electro-magnet 10 and U type locking hook structure 11, the surface of deck 1 that takes off and land is provided with the perforation 12 with U type locking hook structure 11 adaptation, electro-magnet 10 sets up in pairs, the top of electro-magnet 10 extends to the surface of deck 1 that takes off and land, U type locking hook structure 11 is located between two electro-magnets 10 of homonymy, when unmanned aerial vehicle descends to deck 1 that takes off and land, electro-magnet 10 circular telegram produces magnetic force, adsorb iron's unmanned aerial vehicle foot firmly, accessible U type locking hook structure 11 carries out the locking to the unmanned aerial vehicle foot afterwards and fixes, guarantee unmanned aerial vehicle's safety.

An electric telescopic rod 13 and a fixed pulley 14 are further arranged at the bottom of the lifting deck 1, a traction rope 15 is fixedly connected to the working end of the electric telescopic rod 13, and one end of the traction rope 15 bypasses the surface of the fixed pulley 14 and is fixedly connected with one end of the U-shaped locking claw structure 11; the U-shaped locking claw structure 11 comprises a cylinder 111, the cylinder 111 is provided with two parts and fixed at the bottom of the lifting deck 1, a guide partition plate 112 is arranged in the cylinder 111, the guide partition plate 112 is provided with two parts, the middle part of the guide partition plate is slidably connected with a connecting rod 113, the top end of the connecting rod 113 is fixedly connected with a U-shaped fixing frame 114, one side of the U-shaped fixing frame 114 is fixedly connected with a telescopic electromagnetic lock 115, the bottom end of the connecting rod 113 is fixedly connected with a limiting plate 116, a fixing rod 117 is fixedly connected between the two limiting plates 116 on the two sides, a fixed pulley 14 is positioned right above the fixing rod 117, one end of a traction rope 15 is fixedly connected with the middle part of the fixing rod 117, a spring 118 is arranged between the top of the limiting plate 116 and the guide partition plate 112, when the unmanned aerial vehicle foot is locked and fixed, the U-shaped locking claw structure 11 is firstly contracted through an electric telescopic rod 13, the fixing rod 117 is driven to move upwards through the traction rope 15, then the U-shaped fixing frame 114 is driven to move upwards through the limiting plate 116 and the connecting rod 113, the unmanned aerial vehicle foot is positioned in the U-shaped fixing frame 114, finally, the telescopic electromagnetic lock 115 is electrified to work, the telescopic end of the telescopic electromagnetic lock 115 is extended, so that the top of the unmanned aerial vehicle foot is fixed at the secondary telescopic electromagnetic lock to press the unmanned aerial vehicle fixing frame 115;

unmanned aerial vehicle is when needs take off, flexible end of flexible electromagnetic lock 115 is withdrawed earlier, electro-magnet 10 outage loses magnetic adsorption after unmanned aerial vehicle receives the instruction that takes off and rises, guarantee that unmanned aerial vehicle can normally work and lift off, unmanned aerial vehicle takes off after finishing, electric telescopic handle 13 extension, U type mount 114 is downstream under the spring 118 effect to the completion is withdrawed, guarantee taking off and landing deck 1 level and smooth, make unmanned aerial vehicle object surface obstacle-free when descending.

The top of deck 1 that takes off and land and be close to first pivot 3 and the 5 positions of second pivot and be provided with monitoring camera 17, monitoring camera 17 is located the top condition of taking off and land deck 1, be convenient for control unmanned aerial vehicle descending condition, monitoring camera 17's pencil and electro-magnet 10, electric telescopic handle 13 and flexible electromagnetic lock 115's pencil extend to the ship on, through the equipment control behavior on the ship, the rope has been tied up to one side of support frame 4 and the ship is connected, the removal of assurance ship can drag the platform at the horizontally removal.

In addition, still can demolish solid fixed ring 6 and a section of thick bamboo 7 that floats, but support frame 4 adopts scalable mount, realizes working in the operation area of land unevenness, guarantees unmanned aerial vehicle and operating personnel's safety to avoid bringing the unnecessary loss.

It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. The term "comprising", without further limitation, means that the element so defined is not excluded from the group consisting of additional identical elements in the process, method, article, or apparatus that comprises the element.

The above description is only a preferred embodiment of the present invention, and is not intended to limit the present invention, and modifications and variations may be made by those skilled in the art. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims

1. The utility model provides an unmanned aerial vehicle balance and fixed locking platform that takes off and land, includes deck (1) that takes off and land, balanced support (2) and support frame (4), its characterized in that, deck (1) that takes off and land is the hexagon structure, the both ends middle part position fixedly connected with first pivot (3) of deck (1) that takes off and land, first pivot (3) are connected with the inner wall rotation of balanced support (2), the both ends middle part position fixedly connected with second pivot (5) of balanced support (2), second pivot (5) are connected with the top rotation of support frame (4), the bottom fixedly connected with solid fixed ring (6) of support frame (4), gu fixed ring (6) internal fixation connected with floats flotation pontoon (7), float flotation pontoon (7) connect support frame (4) both sides of balanced support (2), the equal fixedly connected with fixing rope (8) of the bottom six angles department of deck (1) that takes off and land, the isometric setting of fixing rope (8) and one end fixedly connected with balancing weight (9), balancing weight (9) are located the below of the center of deck (1) that takes off and land, the symmetrical surface location of deck (1) that takes off and the locking is provided with the sign (16) and the corresponding electromagnet (11) and location of the lifting claw (11), the surface of the lifting deck (1) is provided with a through hole (12) matched with the U-shaped locking claw structure (11).

2. The unmanned aerial vehicle take-off and landing balance and fixed locking platform of claim 1, wherein: the bottom of the lifting deck (1) is further provided with an electric telescopic rod (13) and a fixed pulley (14), the working end of the electric telescopic rod (13) is fixedly connected with a traction rope (15), and one end of the traction rope (15) bypasses the surface of the fixed pulley (14) and is fixedly connected with one end of a U-shaped locking claw structure (11).

3. The balance and fixed locking platform for taking off and landing of the unmanned aerial vehicle as claimed in claim 1, wherein: the lifting device is characterized in that the electromagnets (10) are arranged in pairs, the tops of the electromagnets (10) extend to the surface of the lifting deck (1), and the U-shaped locking claw structures (11) are located between the two electromagnets (10) on the same side.

4. The unmanned aerial vehicle take-off and landing balance and fixed locking platform of claim 1, wherein: the first rotating shaft (3) is rotatably connected with the balance support (2) through a bearing, and the second rotating shaft (5) is rotatably connected with the support frame (4) through a bearing.

5. The balance and fixed locking platform for taking off and landing of the unmanned aerial vehicle as claimed in claim 1, wherein: and a monitoring lens (17) is arranged at the top of the lifting deck (1) and close to the first rotating shaft (3) and the second rotating shaft (5).

6. The unmanned aerial vehicle take-off and landing balance and fixed locking platform of claim 2, wherein: u type locking hook structure (11) include barrel (111), barrel (111) are provided with two and fix the bottom at take-off and landing deck (1), be provided with direction baffle (112) in barrel (111), direction baffle (112) are provided with two and middle part sliding connection has connecting rod (113), the top fixedly connected with U type mount (114) of connecting rod (113), the flexible electromagnetic lock (115) of one side fixedly connected with of U type mount (114), the bottom fixedly connected with limiting plate (116) of connecting rod (113), fixedly connected with dead lever (117) between two limiting plates (116) of both sides, the middle part fixed connection of the one end of haulage rope (15) and dead lever (117), be provided with spring (118) between the top of limiting plate (116) and direction baffle (112).

7. The balance and fixed locking platform for taking off and landing of the unmanned aerial vehicle as claimed in claim 6, wherein: the fixed pulley (14) is positioned right above the fixed rod (117).