CN214608058U

CN214608058U - Unattended system

Info

Publication number: CN214608058U
Application number: CN202120230195.4U
Authority: CN
Inventors: 陈诚; 李威; 尤冰冰; 冉德伟; 陈晨; 黄泽
Original assignee: Honeycomb Aerospace Tecnologies Beijing Co ltd
Current assignee: Honeycomb Aerospace Tecnologies Beijing Co ltd
Priority date: 2021-01-27
Filing date: 2021-01-27
Publication date: 2021-11-05
Anticipated expiration: 2031-01-27

Abstract

The utility model discloses an unmanned on duty system, stop cabin and special VTOL unmanned aerial vehicle including unmanned on duty, unmanned on duty stops the cabin and is used for accomodating special VTOL unmanned aerial vehicle charges to it, special VTOL unmanned aerial vehicle is VTOL unmanned aerial vehicle. The special vertical take-off and landing unmanned aerial vehicle comprises a body, a first wing, a second wing, a first connecting beam, a second connecting beam, a vertical propeller, a tail propeller, an undercarriage, a charging seat and a breaker, wherein the first wing and the second wing are respectively arranged on two sides of the body, and the first connecting beam is detachably connected to the first wing; the system is simple to operate, a task is executed by one key, the requirement on operators is reduced by adopting an instruction key type design in flight control, and the operator training can be completed within 2 h; the system is highly intelligent: accurate landing of unmanned aerial vehicle is realized through accurate landing technique, and the aircraft charges, goes up the electricity, the outage all shuts down the cabin through intelligence and independently accomplishes.

Description

Unattended system

Technical Field

The utility model relates to an unmanned air vehicle technique field, concretely relates to unmanned on duty system, this system are the brand-new application mode in unmanned aerial vehicle field, and this system possesses functions such as unmanned on duty, remote control, key operation, automatic charging, multimachine cooperative control and intelligent data processing, can satisfy the long distance of trades such as border inspection, forest fire prevention, pipeline are patrolled and examined, on a large scale, the unmanned aerial vehicle general survey monitoring demand of high frequency.

Background

Along with the development of unmanned aerial vehicle manufacturing technology and control technology, the application of unmanned aerial vehicle has been introduced in more and more fields, current unmanned aerial vehicle carries on cloud platform camera, carry out conventional observation, need fly to near target area control cloud platform position confirm the approximate position of target location and fix a position again when monitoring, enlarge, fix a position and continue to enlarge, the step is many, the operation complexity is little when the single-point is monitored, but lack the method that high-efficient location was patrolled and examined when needing unmanned aerial vehicle to carry out the multiple spot location to patrol and examine, need adjust repeatedly and do not have the memory function to the position of having patrolled and examined when the multiple spot location is patrolled and examined, need carry out secondary control and just can patrol and examine when patrolling and examining again, inefficiency. Many rotors unmanned on duty system belongs to emerging application mode, and through its application, reducible personnel drop into, improve the operating efficiency, for many rotors unmanned aerial vehicle promote by a large scale and provide powerful guarantee, provide a more convenient, intelligent solution for application environment such as highway, urban road, security protection warehouse, petroleum pipeline, coast patrol.

There is a lack of an unattended system comprising an unattended parking cabin and a dedicated vertical take-off and landing unmanned aerial vehicle.

SUMMERY OF THE UTILITY MODEL

Therefore, the utility model provides an unmanned on duty system to solve the above-mentioned problem among the prior art.

In order to achieve the above object, the present invention provides the following technical solutions:

according to the utility model discloses an aspect, an unmanned on duty system, stop cabin and special VTOL unmanned aerial vehicle including unmanned on duty, unmanned on duty stops the cabin and is used for accomodating special VTOL unmanned aerial vehicle charges to it, special VTOL unmanned aerial vehicle is VTOL unmanned aerial vehicle.

Furthermore, the special vertical take-off and landing unmanned aerial vehicle comprises a body, a first wing, a second wing, a first connecting beam, a second connecting beam, a vertical propeller, a tail propeller, an undercarriage, a charging seat and a circuit breaker, wherein the first wing and the second wing are respectively arranged on two sides of the body, the first connecting beam is detachably connected to the first wing, the second connecting beam is detachably connected to the second wing, the vertical propellers are respectively arranged at two ends of the first connecting beam and two ends of the second connecting beam, the tail propeller is arranged at the tail part of the body, the circuit breaker is arranged at the bottom of the body, the undercarriage is further arranged on the lower surface of the body, and the charging seat is arranged at the lower end of the undercarriage; the special vertical take-off and landing unmanned aerial vehicle also comprises an empennage, and the empennage is detachably connected to the rear ends of the first connecting beam and the second connecting beam; the first connecting beam is perpendicular to the extending direction of the first wing, and the second connecting beam is perpendicular to the extending direction of the second wing; the first connecting beam is connected to the middle of the first wing through a bolt, and the second connecting beam is connected to the middle of the second wing through a bolt.

Furthermore, wing spoilers are respectively arranged on the first wing and the second wing, the wing spoilers on the first wing are positioned on the outer side of the first connecting beam, the wing spoilers on the second wing are positioned on the outer side of the second connecting beam, and the first connecting beam and the second connecting beam are symmetrically arranged about the vertical central plane of the fuselage.

Furthermore, the special vertical take-off and landing unmanned aerial vehicle further comprises a tail spoiler, the tail wing is of an inverted V-shaped structure, and the end parts of the open ends of the inverted V-shaped structure of the tail wing are detachably arranged at the rear ends of the first connecting beam and the second connecting beam respectively; the tail fin is provided with two tail spoilers which are respectively arranged on two side plates of the inverted V-shaped structure.

Furthermore, the special vertical take-off and landing unmanned aerial vehicle further comprises two connecting rods, the lower part of the machine body is detachably connected with the two landing gears, the landing gears are of two-point supporting structures, and the two charging seats are sleeved at the two lower ends of each landing gear; two ends of the two landing gears are connected through the connecting rod respectively, and the connecting rod is positioned below the charging seat; the machine body is formed by die pressing of high-strength glass fiber and a foam interlayer.

Furthermore, the charging seat comprises a charging seat body and an electrode, the electrode is arranged on the lower surface of the charging seat body, and the charging seat body is provided with a mounting hole which is detachably connected to an undercarriage of the unmanned aerial vehicle; the lower surface of the charging seat body is provided with a groove, and the electrode is arranged in the groove; the groove is an open rectangular cross-section groove; the electrode is a rectangular columnar bulge and is arranged at the center of the groove; the charging seat is characterized by further comprising a clamping piece and fastening screws, wherein the clamping piece is mounted on the charging seat body through the fastening screws, and the mounting holes are formed in the connecting position of the clamping piece and the charging seat body; the mounting hole is a rectangular hole; the dihedral angle between the plane of the clamping piece and the plane of the charging seat body is an obtuse angle; the clamping piece is of a U-shaped structure, the mounting hole is formed between the open end of the U-shaped structure of the clamping piece and the charging seat body, four fixing holes are formed in the clamping piece, the fixing holes are stepped holes, and the fastening screws are connected in the fixing holes in a threaded mode; the nominal diameter of the fastening screw is 3mm-5 mm; still include the visor, be equipped with the locating hole on the visor, the charging seat body deviates from the mounting groove has been seted up on the surface of recess, the visor is established the open end of mounting groove, the mounting groove is used for installing the circuit board.

Furthermore, the unattended shutdown cabin comprises a cabin body, a lifting partition plate, a first cabin door, a second cabin door, a horizontal driving motor, a horizontal nut screw pair, a lifting driving motor, a lifting nut screw pair and a charging seat; the cabin body is provided with a machine body accommodating cavity with an open upper end, the length direction of the open end of the machine body accommodating cavity is connected with the first cabin door and the second cabin door in a sliding mode, and the horizontal driving motor is in transmission connection with the first cabin door and the second cabin door through the horizontal nut-screw pair respectively; the lifting partition plate is connected to the vertical side wall of the accommodating cavity of the machine body in a sliding manner, and the lifting driving motor is in transmission connection with the lifting partition plate through the lifting nut-screw pair; a charging seat is arranged at the bottom of the accommodating cavity of the machine body and used for charging the special vertical take-off and landing unmanned aerial vehicle; the machine body accommodating cavity is divided into a first cavity and a second cavity by the lifting partition plate, and the second cavity is located below the lifting partition plate.

Furthermore, the unmanned on duty shutdown cabin also comprises a wing accommodating cavity and a side cover, wherein the two length edges of the open end of the cabin body are respectively provided with the wing accommodating cavity, and the wing accommodating cavity extends to the outside of the cabin body; the side covers are arranged on two side edges of the first cabin door parallel to the sliding direction of the first cabin door and used for plugging the wing accommodating cavity.

Furthermore, the unmanned on duty parking cabin further comprises an access door, the access door is arranged on the vertical side wall of the cabin body, and the access door is communicated with the second chamber; the unattended operation parking cabin further comprises rollers, a plurality of rollers are arranged at the bottom of the cabin body, and the rollers are universal wheels; the unmanned on duty stops cabin still includes braced frame, the lower surface of lift division board is provided with braced frame, braced frame is the frame construction that flat shaped steel welding formed.

Furthermore, the unattended operation parking cabin also comprises a cabin controller, a cabin wireless module and a command terminal, wherein the lifting driving motor and the horizontal driving motor are electrically connected with the cabin controller, the cabin controller is electrically connected with the cabin wireless module, the command terminal is wirelessly connected with the cabin wireless module, and a horizontal cabin door opening key, a horizontal cabin door closing key, a lifting plate ascending key and a lifting plate descending key are arranged in the command terminal; when the horizontal cabin door opening key is pressed, the first cabin door and the second cabin door are opened in a way of deviating from opposite directions; when the horizontal cabin door closing key is pressed, the first cabin door and the second cabin door are close to each other and closed; when the lifting plate lifting key is pressed, the lifting separation plate is lifted to an upper limit position; when the lifting plate descending key is pressed, the lifting separation plate descends to a lower limit position; the unattended operation parking cabin also comprises an integrated environment sensor, the integrated environment sensor is electrically connected with the cabin controller, and the integrated environment sensor comprises an air speed sensor, a wind direction sensor, an air temperature sensor, a temperature and humidity sensor and a rain and snow sensor which are integrated together; the unattended operation parking cabin further comprises a GPS positioning module, a monitoring camera and a memory, wherein the GPS positioning module, the monitoring camera and the memory are all electrically connected with the cabin controller, and the memory is used for storing a monitoring video recorded by the monitoring camera.

The utility model has the advantages of as follows:

1. the system realizes remote control: the network is used for data transmission, the transmission distance is not limited, the data transmission is not shielded by barriers, and operators do not need to go to the site for operation;

2. the system is simple to operate: one key is used for executing tasks, autonomous landing is realized, the flight control adopts an instruction key type design to reduce the requirement on operators, and the operator training can be completed within 2 h;

3. the system is highly intelligent: accurate landing of unmanned aerial vehicle is realized through accurate landing technique, and the aircraft charges, goes up the electricity, the outage all shuts down the cabin through intelligence and independently accomplishes.

Drawings

In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below. It should be apparent that the drawings in the following description are merely exemplary, and that other embodiments can be derived from the drawings provided by those of ordinary skill in the art without inventive effort.

The structure, ratio, size and the like shown in the present specification are only used for matching with the content disclosed in the specification, so as to be known and read by people familiar with the technology, and are not used for limiting the limit conditions which can be implemented by the present invention, so that the present invention has no technical essential significance, and any structure modification, ratio relationship change or size adjustment should still fall within the scope which can be covered by the technical content disclosed by the present invention without affecting the efficacy and the achievable purpose of the present invention.

Fig. 1 is a perspective view of an unattended system according to some embodiments of the present invention.

Fig. 2 is a front view of an unattended system according to some embodiments of the invention.

Fig. 3 is a special vertical take-off and landing unmanned aerial vehicle top view of the unmanned system provided by some embodiments of the present invention.

Fig. 4 is a view of the utility model discloses some embodiments provide a special VTOL unmanned aerial vehicle of unmanned on duty system from a bottom view.

Fig. 5 is a front view of the dedicated vertical take-off and landing unmanned aerial vehicle of the unattended system provided by some embodiments of the present invention.

Fig. 6 is a rear view of the dedicated vertical take-off and landing unmanned aerial vehicle of the unattended system provided by some embodiments of the present invention.

Fig. 7 is a perspective view of the charging seat of the dedicated vertical take-off and landing unmanned aerial vehicle of the unattended system provided by some embodiments of the present invention.

Fig. 8 is a plan view of the charging seat of the unmanned aerial vehicle for vertical take-off and landing according to some embodiments of the present invention.

Fig. 9 is a perspective view of an unattended operation shutdown cabin of an unattended system according to some embodiments of the present invention.

Fig. 10 is a front view of an unmanned parking space of an unmanned system according to some embodiments of the present invention.

Fig. 11 is a top view of an unmanned shutdown cabin of an unmanned system according to some embodiments of the present invention.

Fig. 12 is a left view of an unattended parking space of an unattended system according to some embodiments of the present invention.

Fig. 13 is an exploded view of an unmanned shutdown cabin of an unmanned system according to some embodiments of the present invention.

Fig. 14 is an exploded view of an unmanned shutdown cabin of an unmanned system according to some embodiments of the present invention.

In the figure: 1. fuselage, 2, first wing, 3, second wing, 4, first tie-beam, 5, second tie-beam, 6, perpendicular screw, 7, tail screw, 8, fin, 9, undercarriage, 10, connecting rod, 11, the outage ware, 12, the charging seat, 13, the charging seat body, 14, joint spare, 15, visor, 16, the locating hole, 17, the mounting hole, 18, the fixed orifices, 19, fastening screw, 20, the recess, 21, the electrode, 22, the cabin body, 23, the lift division board, 24, first hatch door, 25, the second hatch door, 26, the wing holds the chamber, 27, the side cap, 28, access door, 29, the gyro wheel, 30, organism holds the chamber, 31, the reinforcing frame.

Detailed Description

The present invention is described in terms of specific embodiments, and other advantages and benefits of the present invention will become apparent to those skilled in the art from the following disclosure. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

As shown in fig. 1 to 8, the utility model discloses an unmanned on duty system in the embodiment of the first aspect, stop cabin and special VTOL unmanned aerial vehicle including unmanned on duty, unmanned on duty stops the cabin and is used for accomodating special VTOL unmanned aerial vehicle and charges it, and special VTOL unmanned aerial vehicle is VTOL unmanned aerial vehicle.

The precise landing of the special vertical take-off and landing unmanned aerial vehicle is realized through a precise landing technology, and the charging, the electrifying and the power-off of the unmanned aerial vehicle are all automatically completed through an unattended shutdown cabin; the special vertical take-off and landing unmanned aerial vehicle only needs one key for operation, after the unattended shutdown cabin is automatically opened, the special vertical take-off and landing unmanned aerial vehicle slowly rises along with the lifting platform, and when the special vertical take-off and landing unmanned aerial vehicle rises to a proper position, the special vertical take-off and landing unmanned aerial vehicle is automatically started to prepare for flying; after the special vertical take-off and landing unmanned aerial vehicle finishes working and flies back to the cabin, the position centering mechanism of the unmanned on duty stopped the cabin adjusts the special vertical take-off and landing unmanned aerial vehicle to the intermediate position, and the unmanned aerial vehicle intelligent propeller collecting system of the unmanned on duty stopped the cabin adjusts the propeller of the unmanned aerial vehicle to the proper position. After adjustment is finished, the special vertical take-off and landing unmanned aerial vehicle slowly lands along with the lifting platform, and when the unmanned aerial vehicle lands in the cabin, the cabin cover is automatically closed to start charging the airplane.

Optionally, as shown in fig. 1 to 8, in some embodiments, the dedicated vertical take-off and landing unmanned aerial vehicle includes a body 1, a first wing 2, a second wing 3, a first connecting beam 4, a second connecting beam 5, a vertical propeller 6, a tail propeller 7, an undercarriage 9, a charging seat 12, and a charging seat 11, where the first wing 2 and the second wing 3 are respectively disposed on two sides of the body 1, the first connecting beam 4 is detachably connected to the first wing 2, the second connecting beam 5 is detachably connected to the second wing 3, the vertical propeller 6 is respectively disposed at two ends of the first connecting beam 4 and at two ends of the second connecting beam 5, the tail propeller 7 is disposed at a tail of the body 1, the disconnector 11 is disposed at a bottom of the body 1, the undercarriage 9 is further disposed on a lower surface of the body 1, and the charging seat 12 is disposed at a lower end of the undercarriage 9; the special vertical take-off and landing unmanned aerial vehicle also comprises a tail wing 8, wherein the tail wing 8 is detachably connected to the rear ends of the first connecting beam 4 and the second connecting beam 5; the first connecting beam 4 is perpendicular to the extending direction of the first wing 2, and the second connecting beam 5 is perpendicular to the extending direction of the second wing 3; the first connecting beam 4 is connected to the middle of the first wing 2 through a bolt, and the second connecting beam 5 is connected to the middle of the second wing 3 through a bolt.

In the above embodiment, it should be noted that the vertical propeller 6 realizes vertical take-off and landing of the vertical take-off and landing fixed-wing drone, and the tail propeller 7 realizes horizontal flight of the vertical take-off and landing fixed-wing drone.

The technical effects achieved by the above embodiment are as follows: the unmanned aerial vehicle can vertically take off and land in the mode of a rotor unmanned aerial vehicle, and can cruise in the mode of a fixed-wing unmanned aerial vehicle; in the vertical takeoff and landing process, the unmanned aerial vehicle vertically takes off or lands by utilizing rotors distributed on the unmanned aerial vehicle, when the unmanned aerial vehicle needs to fly in a fixed wing mode, the unmanned aerial vehicle is accelerated to a certain speed in a multi-rotor flight mode, the flight mode is switched, and the unmanned aerial vehicle is propelled by horizontal propulsion power to keep horizontal flight; the folding type air-conditioning unit has the characteristics of portability, long endurance, high reliability, simple and convenient operation, modularization, light structural weight and high strength, and can be placed in an air transport box after being folded for convenient transportation; by arranging the charging seat 12, the unmanned aerial vehicle can be charged quickly; the power breaker 11 is arranged to power off the unmanned aerial vehicle, and after the unmanned aerial vehicle flies back into the cabin, the power breaker 11 on the body 1 is automatically powered off after being contacted with the power breaker part in the cabin; can dismantle the rear end of connection at first tie-beam 4 and second tie-beam 5 through setting up fin 8, realized dismantling fin 8 and accomodate, can put into convenient transportation in the air transportation case after being convenient for folding, improved the convenience of transportation, reduced the space size that occupies.

Alternatively, as shown in fig. 1 to 8, in some embodiments, each of the first wing 2 and the second wing 3 is provided with a wing spoiler, the wing spoilers on the first wing 2 are located outside the first connecting beam 4, the wing spoilers on the second wing 3 are located outside the second connecting beam 5, and the first connecting beam 4 and the second connecting beam 5 are symmetrically arranged about the vertical central plane of the fuselage 1.

The beneficial effects of the above alternative embodiment are: the first connecting beam 4 is perpendicular to the extending direction of the first wing 2, and the second connecting beam 5 is perpendicular to the extending direction of the second wing 3, so that the unmanned aerial vehicle can take off and land vertically, the uniformity of lift force is improved, and good flight power is achieved; the wing spoilers are arranged, so that the flight stability is adjusted.

Optionally, as shown in fig. 1 to 8, in some embodiments, the dedicated vertical take-off and landing unmanned aerial vehicle further includes a tail spoiler, the tail wing 8 is of an inverted V-shaped structure, and end portions of an open end of the inverted V-shaped structure of the tail wing 8 are detachably disposed at rear ends of the first connecting beam 4 and the second connecting beam 5, respectively; two tail spoilers are arranged on the tail wing 8 and are respectively arranged on two side plates of the inverted V-shaped structure.

Optionally, as shown in fig. 1 to 8, in some embodiments, the dedicated vertical take-off and landing unmanned aerial vehicle further includes two connecting rods 10, two landing gears 9 are detachably connected to the lower portion of the airframe 1, the landing gears 9 are two-point supporting structures, and a charging seat 12 is installed at two lower ends of each landing gear 9 in a sleeved manner; two ends of the two landing gears 9 are respectively connected through a connecting rod 10, and the connecting rod 10 is positioned below the charging seat 12; the machine body 1 is formed by die pressing of high-strength glass fiber and a foam interlayer.

In the above optional embodiment, it should be noted that the undercarriage 9 is an inverted "V" shaped structure, and the undercarriage 9 is inserted into the charging seat 12 and fastened by bolts; still include three way connection, three way connection's upper end is connected at the lower extreme of undercarriage 9, and connecting rod 10 wears to establish at three way connection's downside both ends.

The beneficial effects of the above alternative embodiment are: by arranging the two undercarriage 9, the stable support of the unmanned aerial vehicle body 2 is realized, and the stability is high; by arranging the connecting rod 10, the stability of the undercarriage is enhanced, and meanwhile, the charging seat 12 is prevented from falling off; the flying weight is reduced by arranging the machine body 1 formed by molding the high-strength glass fiber and foam interlayer; the first connecting beam 4 and the second connecting beam 5 are symmetrically arranged about the vertical central plane of the aircraft body 1, so that the stability of the flight power is realized.

Optionally, as shown in fig. 1 to 8, in some embodiments, the charging dock includes a charging dock body 13 and an electrode 21, the electrode 21 is disposed on a lower surface of the charging dock body 13, and the charging dock body 13 is provided with a mounting hole 17 for detachably connecting to an undercarriage of the unmanned aerial vehicle; the lower surface of the charging seat body 13 is provided with a groove 20, and an electrode 21 is arranged in the groove 20; the groove 20 is an open rectangular cross-section groove; the electrode 21 is a rectangular columnar bulge, and the electrode 21 is arranged at the center of the groove 20; the charging base further comprises a clamping piece 14 and fastening screws 19, wherein the clamping piece 14 is installed on the charging base body 13 through the fastening screws 19, and installation holes 17 are formed in the connection position of the clamping piece 14 and the charging base body 13; the mounting hole 17 is a rectangular hole; a dihedral angle between the plane of the clamping piece 14 and the plane of the charging seat body 13 is an obtuse angle; the clamping piece 14 is of a U-shaped structure, a mounting hole 17 is formed between the open end of the U-shaped structure of the clamping piece 14 and the charging seat body 13, four fixing holes 18 are formed in the clamping piece 14, the fixing holes 18 are stepped holes, and fastening screws 19 are connected with the fixing holes 18 in a threaded manner; the nominal diameter of the fastening screw 19 is between 3mm and 5 mm; still include visor 15, be equipped with locating hole 16 on the visor 15, the charging seat body 13 has seted up the mounting groove on deviating from the surface of recess 20, and visor 15 is established at the open end of mounting groove, and the mounting groove is used for installing the circuit board.

In the above optional embodiment, it should be noted that the connection mode between the electrode 21 and the charging seat body 13 may be fixed connection or detachable connection; the mounting holes 17 can be arranged into different shapes according to different unmanned aerial vehicle landing gears; the electrode 21 is a rectangular columnar bulge, and the electrode 21 is arranged at the center of the groove 20; the mounting hole 17 is a rectangular hole, and a dihedral angle between a plane where the clamping piece 14 is located and a plane where the charging seat body 13 is located is an obtuse angle.

The beneficial effects of the above alternative embodiment are: by arranging the charging seat body 13 and the electrodes 21, the unattended system is more automatic and intelligent, and the labor input is reduced; different connection modes of the electrodes 21 and the charging seat body 13 are set, and the mounting holes 17 are set into different shapes according to different unmanned aerial vehicle undercarriages, so that the unmanned aerial vehicle charging seat can adapt to various working environments and different types of unmanned aerial vehicles; by arranging the groove 20 and arranging the electrode 21 as a rectangular columnar bulge, the unmanned aerial vehicle can be accurately positioned in the charging process, and the charging process is more accurate and convenient; the charging seat body 13 can be conveniently installed and replaced through the clamping piece 14 and the fastening screw 19; by setting the dihedral angle between the plane where the clamping piece 14 is located and the plane where the charging seat body 13 is located to be an obtuse angle, the front surface of the electrode 21 faces downwards, so that the charging operation can be conveniently carried out by contacting a charging electrode in the unmanned airplane cabin; the clamping piece 14 is arranged to be of a U-shaped structure, so that the charging seat body 13 can be conveniently fixed and installed; by arranging the fixing hole 18 as a stepped hole, the problem of unattractive appearance and inconvenience in use caused by the protrusion of the screw head after the fixing screw 7 is installed can be avoided; by arranging the mounting groove, the mounting and the storage of the charging line can be facilitated; the protective cover 15 is provided with a positioning hole 16, and the protective cover 15 is mounted on the mounting groove in a buckling mode, so that the protective cover can be conveniently detached and mounted.

Optionally, as shown in fig. 1 to 14, in some embodiments, the unmanned parking cabin includes a cabin body 22, a lifting partition plate 23, a first cabin door 24, a second cabin door 25, a horizontal driving motor, a horizontal nut screw pair, a lifting driving motor, a lifting nut screw pair, and a charging seat; the cabin body 22 is provided with a body accommodating cavity 30 with an open upper end, the length direction of the open end of the body accommodating cavity 30 is connected with a first cabin door 24 and a second cabin door 25 in a sliding manner, and a horizontal driving motor is in transmission connection with the first cabin door 24 and the second cabin door 25 through a horizontal nut-screw pair respectively; the lifting partition plate 23 is connected to the vertical side wall of the machine body accommodating cavity 30 in a sliding manner, and the lifting driving motor is in transmission connection with the lifting partition plate 23 through a lifting nut-screw pair; a charging seat is arranged at the bottom of the body accommodating cavity 30 and used for charging the special vertical take-off and landing unmanned aerial vehicle; the body accommodating chamber 30 is partitioned into a first chamber and a second chamber by the elevation partition plate 23, and the second chamber is located below the elevation partition plate 23.

In the above embodiment, it should be noted that the cabin 22 may be formed by welding stainless steel plates, and sealing strips are disposed at the joints between the first and

second doors

24 and 25 and the cabin 22, so as to prevent rain from wetting electronic components inside the cabin 22; when the unmanned aerial vehicle enters the unattended shutdown cabin, the unmanned aerial vehicle can be descended along with the lifting partition plate 23, so that a charging port on the unmanned aerial vehicle is abutted against a charging seat under the action of gravity; can be provided with the stopper on the inside wall of the cabin body 22, when the cabin body 22 moves down, but the butt is on the stopper, and first cavity is used for depositing unmanned aerial vehicle, and the second cavity is used for storing the required electronic components of unmanned on duty shut down cabin.

The technical effects achieved by the above embodiment are as follows: the system can be remotely controlled, autonomously charged, autonomously lifted and landed, clustered and autonomously operated and the like, and can be widely applied to the industries of environment monitoring, power inspection, pipeline inspection, forest fire prevention, emergency detection and the like; the machine body accommodating cavity 30 is divided into a first cavity and a second cavity by the lifting partition plate 23, so that the unmanned aerial vehicle can be accommodated, and the upper and lower cabin separation designs are adopted for protecting the required electric components, thereby facilitating transportation and reducing weight; possess the high accuracy module that resets, can reset unmanned aerial vehicle to the assigned position.

Optionally, as shown in fig. 1 to 14, in some embodiments, the unmanned aerial vehicle further includes wing receiving cavities 26 and side covers 27, the two length edges of the open end of the nacelle 22 are respectively provided with the wing receiving cavities 26, and the wing receiving cavities 26 extend to the outside of the nacelle 22; two side edges of the first door 24 parallel to the sliding direction of the first door 24 are provided with side covers 27, and the side covers 27 are used for sealing the wing accommodating cavities 26.

Optionally, as shown in fig. 1 to 14, in some embodiments, the unmanned parking cabin further includes an access door 28, the access door 28 is disposed on a vertical side wall of the cabin 22, and the access door 28 is communicated with the second chamber; the unattended operation parking cabin also comprises rollers 29, the bottom of the cabin body 22 is provided with a plurality of rollers 29, and the rollers 29 are universal wheels; the unmanned on duty stops the cabin and still includes braced frame 31, and the lower surface of lift division board 23 is provided with braced frame 31, and braced frame 31 is the frame construction that flat shaped steel welding formed.

In the above alternative embodiment, it should be noted that the wing receiving cavity 26 is communicated with the body receiving cavity 30; the access door 28 is rotatably connected to the side wall of the cabin 22 through a hinge, in addition, a handle is arranged on the outer side wall of the access door 28, and a lockset is also arranged on the access door 28, so that the safety of devices inside the cabin 22 is protected; rollers are arranged at four bottom corners of the cabin 22; for example, a flat stainless steel is welded into a frame structure which is staggered transversely and longitudinally.

The beneficial effects of the above alternative embodiment are: the wing accommodating cavity 26 is arranged, so that the wings of the unmanned aerial vehicle can be placed; the maintenance of the electronic components in the cabin 22 is realized by arranging the access door 28; by arranging the rollers 29, the mobility of the cabin 22 is improved; through setting up strengthening frame 31, can play the supporting role to lift division board 23, can also play the enhancement to the mechanical strength of lift division board 23.

Optionally, as shown in fig. 1 to 14, in some embodiments, the unattended operation stopped cabin further includes a cabin controller, a cabin wireless module, and a command terminal, the lifting drive motor and the horizontal drive motor are both electrically connected to the cabin controller, the cabin controller is electrically connected to the cabin wireless module, the command terminal is electrically connected to the cabin wireless module in a wireless manner, and a horizontal cabin door opening key, a horizontal cabin door closing key, a lifting plate lifting key, and a lifting plate lowering key are provided in the command terminal; when the horizontal cabin door opening key is pressed, the first cabin door 24 and the second cabin door 25 are opened in a way of deviating from opposite directions; when the horizontal door close key is pressed, the first door 24 and the second door 25 are closed close to each other; when the lifter plate up key is pressed, the lifter partition plate 23 is raised to the upper limit position; when the lifter plate lowering key is pressed, the lifter partition plate 23 is lowered to the lower limit position; the unattended operation stopped cabin also comprises an integrated environment sensor, the integrated environment sensor is electrically connected with the cabin controller, and the integrated environment sensor comprises an air speed sensor, a wind direction sensor, an air temperature sensor, a temperature and humidity sensor and a rain and snow sensor which are integrated together; the unattended operation parking cabin further comprises a GPS positioning module, a monitoring camera and a memory, wherein the GPS positioning module, the monitoring camera and the memory are all electrically connected with the cabin controller, and the memory is used for storing a monitoring video recorded by the monitoring camera.

In the above optional embodiment, it should be noted that the aircraft cabin controller further includes a cloud server, the cabin controller is electrically connected to a command terminal through the cloud server, the command terminal is a computer, a tablet, a mobile phone terminal or a specially-made control terminal, and the control circuit can be implemented by using a circuit connection relationship in the prior art.

The beneficial effects of the above alternative embodiment are: by arranging the cabin controller, the cabin wireless module and the command terminal, the intelligent control of the unmanned on-duty cabin stopping is realized, and the intelligent control can be cooperatively controlled with the unmanned aerial vehicle to realize automatic opening, closing and charging; the charging adopts commercial power supply, so that a storage taking-off and landing place is provided for the unmanned aerial vehicle, and the all-weather operation capability of the unmanned aerial vehicle is ensured; and the command terminal is internally provided with command center software: and the command center software is designed in a command button type, so that the operation is convenient and simple. The flight path of the unmanned aerial vehicle can be planned, the flight of the unmanned aerial vehicle is controlled, and the states of the unmanned aerial vehicle and the shutdown cabin are observed in real time; the meteorological environment around the shutdown cabin can be sensed in real time; the GPS positioning module is arranged, so that the unmanned on-duty shutdown cabin can be accurately positioned, the monitoring of the environment around the unmanned on-duty shutdown cabin is realized by arranging the monitoring camera, and the flying condition of the unmanned aerial vehicle near the unmanned on-duty shutdown cabin can be monitored in real time; through setting up the light, realized the illumination to unmanned on duty shut down cabin surrounding environment.

In the specific implementation process, the parameters of the drooping fixed-wing unmanned aerial vehicle are as follows: wingspan: 3200 mm; machine length: 1780 mm; the machine height is as follows: 465mm without landing gear; standard load: 2 kg; during voyage: not less than 100min1000 m; working radius: not less than 50Km1000 m; measuring and controlling the distance: the microwave link is 50Km/30 Km; working altitude: more than or equal to 3000 m; wind resistance: grade 5 or more; and (3) landing precision: is better than 30 cm; the safety mechanism is as follows: self-checking of the system, chain breakage protection, low-power return and autonomous standby landing; the parameters of the unattended operation stopped cabin are as follows: and (3) cabin size collection: 2800 x 2300 x 1400 (length x width x height); the unfolding size is as follows: 5170 × 3300 × 1400 (length × width × height); weight: less than or equal to 750 kg; ambient temperature: -20 ℃ to 45 ℃ and-40 ℃ to 55 ℃ (including temperature control); protection grade: IP 55; the communication mode is as follows: 4G/5G/optical fiber/Weitong.

Although the invention has been described in detail with respect to the general description and the specific embodiments, it will be apparent to those skilled in the art that modifications and improvements can be made based on the invention. Therefore, such modifications and improvements are intended to be within the scope of the invention as claimed.

In the present specification, the terms "upper", "lower", "left", "right", "middle", and the like are used for the sake of clarity only, and are not intended to limit the scope of the present invention, and changes or adjustments of the relative relationship thereof are also considered to be the scope of the present invention without substantial changes in the technical content.

Claims

1. An unattended system is characterized by comprising an unattended parking cabin and a special vertical take-off and landing unmanned aerial vehicle, wherein the unattended parking cabin is used for accommodating and charging the special vertical take-off and landing unmanned aerial vehicle, and the special vertical take-off and landing unmanned aerial vehicle is a vertical take-off and landing unmanned aerial vehicle; the special vertical take-off and landing unmanned aerial vehicle comprises a fuselage (1), a first wing (2), a second wing (3), a first connecting beam (4), a second connecting beam (5), a vertical propeller (6), a tail propeller (7), an undercarriage (9), a charging seat (12) and a circuit breaker (11), wherein the first wing (2) and the second wing (3) are respectively arranged on two sides of the fuselage (1), the first connecting beam (4) is detachably connected on the first wing (2), the second connecting beam (5) is detachably connected on the second wing (3), the vertical propeller (6) is respectively arranged at two ends of the first connecting beam (4) and two ends of the second connecting beam (5), the tail propeller (7) is arranged at the tail part of the fuselage (1), the circuit breaker (11) is arranged at the bottom of the fuselage (1), the lower surface of the machine body (1) is also provided with the undercarriage (9), and the lower end of the undercarriage (9) is provided with the charging seat (12); the special vertical take-off and landing unmanned aerial vehicle further comprises an empennage (8), and the empennage (8) is detachably connected to the rear ends of the first connecting beam (4) and the second connecting beam (5); the first connecting beam (4) is perpendicular to the extending direction of the first wing (2), and the second connecting beam (5) is perpendicular to the extending direction of the second wing (3); the first connecting beam (4) is connected to the middle of the first wing (2) through a bolt, and the second connecting beam (5) is connected to the middle of the second wing (3) through a bolt.

2. An unmanned system according to claim 1, wherein each of the first wing (2) and the second wing (3) is provided with a wing spoiler, the wing spoilers on the first wing (2) are located outside the first connecting beam (4), the wing spoilers on the second wing (3) are located outside the second connecting beam (5), and the first connecting beam (4) and the second connecting beam (5) are symmetrically arranged about a vertical central plane of the fuselage (1).

3. The unmanned system of claim 2, wherein the dedicated VTOL UAV further comprises a tail spoiler, the tail wing (8) is of an inverted V-shaped structure, and the ends of the open ends of the inverted V-shaped structure of the tail wing (8) are respectively and detachably arranged at the rear ends of the first connecting beam (4) and the second connecting beam (5); the tail wing (8) is provided with two tail spoilers which are respectively arranged on two side plates of the inverted V-shaped structure.

4. The unmanned system according to claim 3, wherein the dedicated VTOL unmanned aerial vehicle further comprises two connecting rods (10), the number of the landing gears (9) is two, the two landing gears (9) are detachably connected to the lower part of the vehicle body (1), the landing gears (9) are two-point supporting structures, and the charging seats (12) are sleeved on the two lower ends of each landing gear (9); two ends of the two landing gears (9) are respectively connected through the connecting rod (10), and the connecting rod (10) is positioned below the charging seat (12); the machine body (1) is formed by die pressing of high-strength glass fiber and a foam interlayer.

5. The unmanned system of claim 4, wherein the charging dock comprises a charging dock body (13) and an electrode (21), the electrode (21) is disposed on a lower surface of the charging dock body (13), the charging dock body (13) is provided with a mounting hole (17) for detachable connection to an undercarriage of the unmanned aerial vehicle; a groove (20) is formed in the lower surface of the charging seat body (13), and the electrode (21) is arranged in the groove (20); the groove (20) is an open rectangular cross-section groove; the electrode (21) is a rectangular columnar bulge, and the electrode (21) is arranged at the center of the groove (20); the charging seat is characterized by further comprising a clamping piece (14) and fastening screws (19), wherein the clamping piece (14) is installed on the charging seat body (13) through the fastening screws (19), and the installation hole (17) is formed in the connection position of the clamping piece (14) and the charging seat body (13); the mounting hole (17) is a rectangular hole; a dihedral angle between the plane of the clamping piece (14) and the plane of the charging seat body (13) is an obtuse angle; the clamping piece (14) is of a U-shaped structure, the mounting hole (17) is formed between the open end of the U-shaped structure of the clamping piece (14) and the charging seat body (13), four fixing holes (18) are formed in the clamping piece (14), the fixing holes (18) are stepped holes, and fastening screws (19) are connected to the fixing holes (18) in an internal thread mode; the nominal diameter of the fastening screw (19) is between 3mm and 5 mm; still include visor (15), be equipped with locating hole (16) on visor (15), charging seat body (13) deviate from the mounting groove has been seted up on the surface of recess (20), visor (15) are established the open end of mounting groove, the mounting groove is used for installing circuit board.

6. The unattended system according to claim 1, wherein the unattended parking cabin comprises a cabin body (22), a lifting partition plate (23), a first cabin door (24), a second cabin door (25), a horizontal driving motor, a horizontal nut screw pair, a lifting driving motor, a lifting nut screw pair and a charging seat; the cabin body (22) is provided with a machine body accommodating cavity (30) with an open upper end, the open end of the machine body accommodating cavity (30) is connected with the first cabin door (24) and the second cabin door (25) in a sliding mode in the length direction, and the horizontal driving motor is in transmission connection with the first cabin door (24) and the second cabin door (25) through the horizontal nut-screw pair respectively; the lifting partition plate (23) is connected to the vertical side wall of the machine body accommodating cavity (30) in a sliding mode, and the lifting driving motor is in transmission connection with the lifting partition plate (23) through the lifting nut-screw pair; a charging seat is arranged at the bottom of the body accommodating cavity (30), and the charging seat is used for charging the special vertical take-off and landing unmanned aerial vehicle; the machine body accommodating cavity (30) is divided into a first cavity and a second cavity by the lifting partition plate (23), and the second cavity is located below the lifting partition plate (23).

7. An unmanned system according to claim 6, wherein the unmanned aerial vehicle further comprises wing receiving cavities (26) and side covers (27), wherein the wing receiving cavities (26) are respectively arranged at two length edges of the open end of the nacelle body (22), and the wing receiving cavities (26) extend to the outside of the nacelle body (22); the side covers (27) are arranged on two side edges of the first door (24) parallel to the sliding direction of the first door (24), and the side covers (27) are used for sealing the wing accommodating cavity (26).

8. An unmanned system according to claim 7, wherein the unmanned parked nacelle further comprises an access door (28), the access door (28) being provided on a vertical side wall of the nacelle (22), the access door (28) being in communication with the second chamber; the unmanned parking cabin further comprises rollers (29), a plurality of rollers (29) are arranged at the bottom of the cabin body (22), and the rollers (29) are universal wheels; unmanned on duty stops cabin still includes braced frame (31), the lower surface of lift division board (23) is provided with braced frame (31), braced frame (31) are the frame construction that flat shaped steel welding formed.

9. The unattended system according to claim 8, wherein the unattended parking cabin further comprises a cabin controller, a cabin wireless module and a command terminal, the lifting driving motor and the horizontal driving motor are electrically connected with the cabin controller, the cabin controller is electrically connected with the cabin wireless module, the command terminal is electrically connected with the cabin wireless module in a wireless manner, and a horizontal cabin door opening key, a horizontal cabin door closing key, a lifting plate ascending key and a lifting plate descending key are arranged in the command terminal; when the horizontal cabin door opening key is pressed, the first cabin door (24) and the second cabin door (25) are opened in a way of deviating from opposite directions; -when said horizontal door closing key is pressed, said first door (24) and said second door (25) close to each other; when the lifting plate lifting key is pressed, the lifting separation plate (23) is lifted to an upper limit position; when the lifting plate descending key is pressed, the lifting separation plate (23) descends to a lower limit position; the unattended operation parking cabin also comprises an integrated environment sensor, the integrated environment sensor is electrically connected with the cabin controller, and the integrated environment sensor comprises an air speed sensor, a wind direction sensor, an air temperature sensor, a temperature and humidity sensor and a rain and snow sensor which are integrated together; the unattended operation parking cabin further comprises a GPS positioning module, a monitoring camera and a memory, wherein the GPS positioning module, the monitoring camera and the memory are all electrically connected with the cabin controller, and the memory is used for storing a monitoring video recorded by the monitoring camera.