CN220263145U - Survey and drawing unmanned aerial vehicle falls storage device - Google Patents

Abstract

Survey unmanned aerial vehicle falls storage device, includes: the utility model ensures that the surveying and mapping unmanned aerial vehicle cannot be interfered by environmental wind in the falling process through the wind shield and the wind guide strip, and avoids the influence of unstable air flow when the surveying and mapping unmanned aerial vehicle falls in a narrow and relatively closed space, and meanwhile, the air bag capable of being inflated and deflated is arranged below the surveying and mapping unmanned aerial vehicle, so that the surveying and mapping camera cannot be damaged due to jolt in the process of storing and transporting the surveying and mapping unmanned aerial vehicle.

Description

Survey and drawing unmanned aerial vehicle falls storage device

Technical Field

The utility model relates to the technical field of unmanned aerial vehicle auxiliary equipment, in particular to a surveying and mapping unmanned aerial vehicle landing storage device.

Background

The unmanned survey aircraft is an unmanned aircraft for geographic information acquisition, measurement and drawing. The high-precision sensor is carried, such as a GPS, a laser scanner, a high-resolution camera and the like, and high-efficiency and accurate measurement and drawing are realized through a flight control system. Unmanned aerial vehicle survey and drawing has characteristics fast, safe, high-efficient and the precision is high, can be applied to fields such as urban planning, land investigation, resource development, environmental monitoring. Under the condition that the unmanned aerial vehicle of survey and drawing does not fly, accomodate the transportation by corresponding descending storage equipment to unmanned aerial vehicle generally. The related art currently retrieved is listed below:

chinese patent 1; name: survey and drawing unmanned aerial vehicle landing platform; patent number: 202221320901.5; summary: the utility model relates to the technical field of unmanned aerial vehicle auxiliary equipment, and discloses a surveying and mapping unmanned aerial vehicle landing platform, which comprises a machine body, four groups of pulleys arranged at the bottom of the machine body, a placing block fastened at the top of the machine body, four groups of first springs fastened in the placing block and a buffer plate fastened at the top of the first springs, wherein a movable groove is formed in the machine body, two groups of sliding grooves are formed in the top of the movable groove, and a movable rod is connected in a sliding manner in the sliding grooves. This survey and drawing unmanned aerial vehicle platform that falls, through the cooperation between push pedal and the two sets of fly leaf, and then when the push pedal antedisplacement and the front side of two sets of fly leaf of top move, the rear side of fly leaf will drive the movable rod displacement through the mode that the spliced pole was moved to the top, and the removal of movable rod will drive the guard plate and remove the outside of placing the piece, makes two sets of guard plate protection place the piece and place the unmanned aerial vehicle in the piece, has prevented that unmanned aerial vehicle from being destroyed the condition in transit.

Chinese patent 2; name: survey and drawing unmanned aerial vehicle landing platform; patent number: 202121457897.2; summary: the utility model provides a mapping unmanned aerial vehicle landing platform, which belongs to the technical field of landing platforms and comprises: the device comprises a base, rollers, armrests, an electric push rod, a protective cover, a supporting part, a supporting rod, a supporting plate, a spring, a contact plate, a containing groove, a telescopic plate, a handle, a cover plate, a first connecting part, a second connecting part, a locking ring and a handle; in order to solve the problems that an unmanned aerial vehicle landing platform in the prior art cannot be suitable for a mapping field, the unmanned aerial vehicle is stored and transported stably, and the like, the utility model provides the mapping unmanned aerial vehicle landing platform which is more suitable for mapping complex large-area terrains, the device is convenient to move and store, the unmanned aerial vehicle can be stored after falling, and the purpose of protecting the unmanned aerial vehicle is achieved. Simultaneously, this device has greatly promoted unmanned aerial vehicle and has fallen behind the prerequisite of unmanned aerial vehicle stability under, and the convenience and the suitability of removal satisfy the demand of different transportation, promote and use experience.

According to the search results, the fact that a certain problem exists in the actual use process of the existing mapping unmanned aerial vehicle landing device on the market can be seen, on one hand, most of the existing mapping unmanned aerial vehicle landing devices basically provide a landing platform for the mapping unmanned aerial vehicle, and wind shielding structures are lacked around the existing mapping unmanned aerial vehicle landing devices, so that the mapping unmanned aerial vehicle can be influenced in the landing process due to the influence of environmental wind, the mapping equipment such as a precision sensor and a mapping cradle head mounted on the mapping unmanned aerial vehicle can be damaged due to overlarge landing impact, and although part of the mapping unmanned aerial vehicle landing devices are provided with the wind shielding structures, a narrow and relatively closed space can be formed between the wind shielding structures and the landing platform of the mapping unmanned aerial vehicle landing device, and air in the landing platform can flow too fast in the landing process of the mapping unmanned aerial vehicle; the air flow is unstable; the air flow is uneven; the condition such as air current intensity is too big, influences unmanned aerial vehicle's steady landing, and on the other hand, current survey unmanned aerial vehicle landing gear is provided with fixing device, however, is used for carrying on survey and drawing camera's survey and drawing cloud platform not corresponding protection to survey and drawing unmanned aerial vehicle, probably leads to survey and drawing unmanned aerial vehicle in the in-process of accomodating the transportation, and survey and drawing cloud platform damages because jolt or strike.

Disclosure of Invention

The utility model aims to provide a surveying and mapping unmanned aerial vehicle landing storage device, which solves the problem that the existing surveying and mapping unmanned aerial vehicle landing device lacks a wind shielding device to influence the normal landing of an unmanned aerial vehicle, and the existing wind shielding device can form a narrow and relatively closed space, so that air in a landing platform is excessively fast; the air flow is unstable; the air flow is uneven; the condition such as air current intensity is too big to and current survey and drawing unmanned aerial vehicle landing gear is in accomodating the in-process of transportation, lacks the problem of corresponding protection to the survey and drawing cloud platform, adopts the scheme as follows for realizing above-mentioned purpose:

survey unmanned aerial vehicle falls storage device, includes: the air guide device comprises an outer box body, universal wheels, a power supply, a controller, a handle, a box cover, an inner box body, an electric sliding table, a windshield, air guide strips, electric push rods, an air pump, a landing table, fixing straps, an air bag, an electric air valve and an air guide hose.

Further, the power supply sets a charging interface.

Further, the controller is a singlechip controller.

Further, the wind shield and the wind guide strip are made of transparent acrylic

Further, an anti-slip rubber is arranged on one side, in contact with the landing gear of the unmanned aerial vehicle, of the fixing strap.

The using method comprises the following steps:

the staff opens the case lid, start electric putter through the controller, lift the landing platform, then start electric slipway, lift the windshield, just can let the unmanned aerial vehicle flying hand drop this moment, at the in-process of dropping, the air current that unmanned aerial vehicle rotor produced is through the bar opening of windshield, the air guide mouth of following the wind-guiding strip bottom is discharged, make the air current in the windshield stable relatively, evenly, simultaneously, because the wind guide mouth of wind-guiding strip is located the bottom, make the environmental wind can not get into the windshield by the wind guide mouth, can not cause the influence to unmanned aerial vehicle's landing, after unmanned aerial vehicle steadily drops, the staff fixes unmanned aerial vehicle's undercarriage on the landing platform through the fixed bandage, then start the air pump through the controller, open the electric air valve with the air pump intercommunication, close the electric air valve that does not communicate with the air pump, charge into a quantitative gas to the gasbag, guarantee that the survey and drawing cloud platform can not be damaged because of jolt or strike the swing of showing a large margin in the transportation process, then control electric shrink, with survey and drawing unmanned aerial vehicle accomodates in the interior box, close the case lid, the handle shifts to the survey and drawing place, reach other places through the fixed air pump, the landing platform can be opened through the electric air pump, the landing platform is opened when the landing platform, the landing platform is not charge, can be opened with the air pump, the landing device is charged with the landing platform, the landing platform is not is opened, the landing device is can be charged with the landing air pump, and can be had.

THE ADVANTAGES OF THE PRESENT INVENTION

(1) According to the utility model, the strip-shaped opening is arranged on the wind shield, and the wind guide strip with the strip-shaped wind guide opening at the bottom is arranged on the strip-shaped opening, so that the wind shield can isolate ambient wind, the influence of the ambient wind on the take-off and landing of the unmanned aerial vehicle is avoided, air flow generated by the rotation of the rotor wing of the unmanned aerial vehicle is discharged out of the wind shield through the wind guide strip, the ambient wind cannot enter the wind shield through the wind guide strip, and the air in the wind shield is prevented from being excessively fast due to the high-speed rotation of the rotor wing when the unmanned aerial vehicle takes off or lands; the air flow is unstable; the air flow is uneven; and under the conditions of overlarge air flow intensity and the like, the safety of the precision sensor and the surveying equipment such as a surveying and mapping cradle head and the like carried on the unmanned aerial vehicle is ensured.

(2) According to the utility model, the inflatable and deflatable air bag and the fixing binding belt are arranged on the landing platform, so that the mapping cradle head is ensured not to be damaged due to large swing caused by jolt or impact in the process of storage and transportation by the inflatable air bag.

Drawings

FIG. 1 is a front view of the present utility model;

FIG. 2 is a schematic view of the structure of the inner case without the windshield;

FIG. 3 is a schematic view of the structure of the inner box with a windshield;

FIG. 4 is a schematic structural view of the wind guiding strip;

fig. 5 is a schematic diagram of the internal structure of the inner box when the mapping unmanned aerial vehicle is dropped to the landing platform;

fig. 6 is a schematic diagram of an internal structure of the inner box when the unmanned aerial vehicle is stored in the inner box

The meaning of each mark in the figure is as follows:

1-an outer box body; 2-universal wheels; 3-power supply; 4-a controller; 5-handle; 6, a box cover; 7-an inner box body; 8-an electric sliding table; 9-a windshield; 10-wind guiding strips; 11-an electric push rod; 12-an air pump; 13-landing stage; 14-fixing the binding band; 15-an air bag; 16-an electric air valve; 17-an air guide hose.

Detailed Description

The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.

Survey unmanned aerial vehicle falls storage device, includes: the outer box body 1, the universal wheel 2, the power supply 3, the controller 4, the handle 5, the box cover 6, the inner box body 7, the electric sliding table 8, the windshield 9, the air guide strip 10, the electric push rod 11, the air pump 12, the landing table 13, the fixing strap 14, the air bag 15, the electric air valve 16 and the air guide hose 17, wherein the universal wheel 2 is fixedly arranged at four corners of the outer bottom surface of the outer box body 1, the power supply 3 is fixedly arranged in the middle of the outer bottom surface, the controller 4 is fixedly arranged at the front surface of the outer side surface, the handle 5 is fixedly arranged at the right side surface of the outer side surface, the box cover 6 is positioned at the top of the outer box body 1 and is hinged with the outer box body 1, the inner box body 7 is fixedly arranged at the inner bottom surface of the outer box body 1, the electric sliding table 8 is fixedly arranged at the four outer side surfaces of the inner box body 7, the electric sliding table 8 is vertically arranged, the windshield 9 is of a cuboid hollow structure, the upper surface and the lower surface are opened, a plurality of transverse strip-shaped openings are respectively arranged at the four side surfaces, the lower parts of four inner side surfaces are respectively fixed on the sliding tables of the four electric sliding tables 8, a plurality of air guide strips 10 are respectively and fixedly arranged on the outer side surfaces of strip-shaped openings on the side surfaces of the windshield 9, the air guide strips 10 are communicated with the strip-shaped openings, strip-shaped air guide openings are formed in the bottoms of the air guide strips 10, four electric push rods 11 are respectively and vertically arranged at four corners of the inner bottom surface of the inner box 7, an air pump 12 is fixedly arranged at the middle part of the inner bottom surface of the inner box 7, a landing table 13 is positioned in the inner box 7, four corners of the bottom surface are respectively and fixedly connected with the telescopic ends of the four electric push rods 11, fixing straps 14 are arranged at two sides of the top surface of the landing table 13, an air bag 15 is arranged in the middle part, two electric air valves 16 are arranged at the center of the bottom surface of the landing table 13, the two electric air valves 16 are communicated with the air bag 15, the air outlet end of the air pump 12 is connected with any one electric air valve 16 through an air guide hose 17, and the power supply 3 is respectively connected with the controller 4, the electric sliding tables 8, the electric push rod 11, the air pump 12 and the electric air valve 16 are connected, and the controller 4 is respectively and electrically connected with the electric sliding table 8, the electric push rod 11, the air pump 12 and the electric air valve 16.

Preferably, the power supply 3 is provided with a charging interface.

Preferably, the controller 4 is a single-chip microcomputer controller.

Preferably, the wind shield 9 and the wind guiding strip 10 are made of transparent acrylic.

Preferably, the side of the securing strap 14 that contacts the landing gear of the unmanned aerial vehicle is provided with anti-slip rubber.

Claims (5)

1. Survey and drawing unmanned aerial vehicle falls storage device, a serial communication port includes: the utility model comprises an outer box body (1), universal wheels (2), a power supply (3), a controller (4), a handle (5), a box cover (6), an inner box body (7), an electric sliding table (8), a wind shield cover (9), an air guide strip (10), an electric push rod (11), an air pump (12), a landing table (13), a fixing strap (14), an air bag (15), an electric air valve (16) and an air guide hose (17), the universal wheels (2) are fixedly arranged at four corners of the outer bottom surface of the outer box body (1), the power supply (3) is fixedly arranged in the middle of the outer bottom surface, the controller (4) is fixedly arranged on the front surface of the outer side, the handle (5) is fixedly arranged on the right side surface of the outer side surface, the box cover (6) is positioned at the top of the outer box body (1) and is hinged with the outer box body (1), the inner box body (7) is fixedly arranged on the inner bottom surface of the outer box body (1), the electric sliding table (8) is fixedly arranged on four outer side surfaces of the inner box body (7), the electric sliding table (8) are vertically arranged, the wind shield cover (9) is of a cuboid hollow structure, the upper side surface and the lower side surface are respectively provided with four lateral side surfaces which are respectively provided with four lateral inner side surfaces, the four lateral side surfaces respectively, the electric sliding table (8) are fixedly arranged on the strip-shaped wind guide strips respectively, air guide strip (10) and bar opening intercommunication, and the bottom of air guide strip (10) sets up the wind guide mouth of bar, bottom surface four corners in box (7) are including four electric putter (11) respectively vertical installation, bottom surface middle part in box (7) are including air pump (12) fixed mounting, descending platform (13) are located in box (7), and bottom surface four corners respectively with the flexible end rigid coupling of four electric putter (11), descending platform (13) top surface both sides set up fixed bandage (14), the middle part sets up gasbag (15), descending platform (13) bottom surface center sets up two electric air valves (16), and two electric air valves (16) and gasbag (15) intercommunication, the end of giving vent to anger of air pump (12) is connected with arbitrary electric air valve (16) through air guide hose (17), power (3) are connected with controller (4) respectively, electric slipway (8), electric putter (11), air pump (12) and electric air valve (16), controller (4) are with electric slipway (8), electric putter (11), air pump (12) and electric air valve (16) electric connection respectively.

2. The survey unmanned aerial vehicle landing receptacle of claim 1, wherein: the power supply (3) is provided with a charging interface.

3. The survey unmanned aerial vehicle landing receptacle of claim 1, wherein: the controller (4) is a singlechip controller.

4. The survey unmanned aerial vehicle landing receptacle of claim 1, wherein: the wind shield (9) and the wind guide strip (10) are made of transparent acrylic.

5. The survey unmanned aerial vehicle landing receptacle of claim 1, wherein: one side of the fixing strap (14) contacted with the landing gear of the unmanned aerial vehicle is provided with anti-slip rubber.