CN215361899U

CN215361899U - Unmanned aerial vehicle carrying, flying and recycling system for shelter

Info

Publication number: CN215361899U
Application number: CN202120099861.5U
Authority: CN
Inventors: 王志勤; 刘建博; 张博峰; 徐迪
Original assignee: Xi'an Tiancheng Yibang Electronic Technology Co ltd
Current assignee: Xi'an Tiancheng Yibang Electronic Technology Co ltd
Priority date: 2021-01-14
Filing date: 2021-01-14
Publication date: 2021-12-31
Anticipated expiration: 2031-01-14

Abstract

The utility model discloses an unmanned aerial vehicle carrying, flying and recycling system for a shelter, which comprises a flying platform and a cabin top platform, wherein a telescopic mechanism is fixedly arranged at the top of the flying platform, the top of the telescopic mechanism is fixedly connected with a clamping mechanism, the bottom of the flying platform is fixedly connected with a lifting mechanism, a correcting mechanism and a three-way mechanism are respectively and fixedly arranged at the top of the cabin top platform, the telescopic mechanism comprises an aluminum alloy platform, the left side of the bottom of the aluminum alloy platform is fixedly connected with a first supporting slide rail, and the right side of the bottom of the aluminum alloy platform is fixedly connected with a second supporting slide rail. The unmanned helicopter has the advantages of being convenient to recover and release, and solves the problems that the wing opening and landing posture correction of the unmanned helicopter is inconvenient, the vertical transportation and clamping fixation of the unmanned helicopter are inconvenient, and the release and recovery of the unmanned helicopter are easily influenced in the use process of the existing unmanned helicopter.

Description

Unmanned aerial vehicle carrying, flying and recycling system for shelter

Technical Field

The utility model relates to the technical field of engineering equipment, in particular to an unmanned aerial vehicle carrying, flying and recycling system for a shelter.

Background

Unmanned aerial vehicle, as the name suggests is unmanned aircraft, unmanned aerial vehicle system mainly includes aircraft body, flight control system, data link system, launching recovery system, power system, etc., flight control system is also called flight management and control system, and is equivalent to the heart part of unmanned aerial vehicle system, and has important influence on stability, reliability, accuracy, real-time property, etc. of unmanned aerial vehicle, and plays a decisive role in flight performance, data link system can ensure accurate transmission of remote control command, and real-time property and reliability of unmanned aerial vehicle receiving and sending information, so as to ensure timely effectiveness of information feedback, smoothness and accuracy to complete task, along with the development of unmanned aerial vehicle industry, the need of realizing automatic storage to automatic release of unmanned aerial vehicle is increasingly abundant, because unmanned helicopter is different from fixed wing unmanned aerial vehicle, in order to realize release and recovery of unmanned aerial vehicle helicopter into cabin, the wing is convenient to transport and store, and the wing needs to be folded; simultaneously because unmanned aerial vehicle need store in certain space, so position and gesture when unmanned aerial vehicle descends need go on according to predetermined state, nevertheless because environment and other factors, unmanned aerial vehicle can't descend according to predetermined state completely.

The existing unmanned helicopter is inconvenient to carry out wing opening and landing posture correction on the unmanned helicopter in the using process, is inconvenient to transport the unmanned helicopter in the vertical direction and clamp and fix the unmanned helicopter, is easy to influence flying and recovery of the unmanned helicopter, and reduces the convenience of the unmanned helicopter.

SUMMERY OF THE UTILITY MODEL

The utility model aims to provide an unmanned aerial vehicle carrying, flying and recovering system for a shelter, which has the advantages of convenience in recovery and flying, and solves the problems that the wing opening and landing posture correction of an unmanned helicopter is inconvenient, the vertical direction transportation and clamping fixation of the unmanned helicopter are inconvenient, the flying and recovery of the unmanned helicopter are easily influenced, and the convenience of the unmanned helicopter is reduced in the using process of the existing unmanned helicopter.

In order to achieve the purpose, the utility model provides the following technical scheme: the utility model provides an unmanned aerial vehicle delivery, free flight and recovery system for shelter, includes take-off platform and cabin roof platform, the top fixed mounting of the platform of taking off has telescopic machanism, telescopic machanism's top fixedly connected with clamping mechanism, the bottom fixedly connected with elevating system of the platform of taking off, the top of cabin roof platform is fixed mounting respectively has correction mechanism and three-way mechanism.

Preferably, telescopic machanism includes the aluminum alloy platform, the first support slide rail of left side fixedly connected with of aluminum alloy platform bottom, the right side fixedly connected with second support slide rail of aluminum alloy platform bottom, the first lead screw module of left side fixedly connected with of slide rail is supported to the second, the top swing joint of aluminum alloy platform has fixed slide rail and second lead screw module, the top of fixed slide rail and second lead screw module and clamping mechanism's bottom fixed connection.

Preferably, the clamping mechanism comprises a rack, a first motor is fixedly connected to the top of the rack, a belt pulley is movably connected to the bottom of the inner wall of the rack through a bearing, a transmission belt is connected to the surface of the belt pulley and an output shaft of the first motor in a transmission manner, a fixing hook is fixedly connected to the surface of the transmission belt, and a limiter is fixedly connected to the top of the rack.

Preferably, the correcting mechanism comprises a connecting slide rail, a push rod is movably connected to the top of the connecting slide rail, a second motor is fixedly connected to the left side of the push rod, a root line belt is arranged on the second motor, a first gear is sleeved on an output shaft of the second motor, a first rack is meshed on the surface of the first gear, and the bottom of the first rack is fixedly connected with the top of the cabin top platform.

Preferably, the three-way mechanism includes a third lead screw module, the bottom swing joint of third lead screw module has movable slide rail, the top fixedly connected with fixed plate of third lead screw module, the bottom fixedly connected with third motor of fixed plate, the output shaft of third motor extends to the top and the fixedly connected with revolving stage of fixed plate, the fixed surface of third lead screw module installs the fourth motor, the output shaft cover of fourth motor is equipped with the second gear, the top fixedly connected with second rack of cabin top platform, the surface of second gear respectively with the surface meshing of first rack and second rack.

Compared with the prior art, the utility model has the following beneficial effects:

1. the unmanned helicopter disclosed by the utility model solves the problems that the wings of the unmanned helicopter are inconvenient to open and correct landing postures, the unmanned helicopter is inconvenient to transport and clamp and fix in the vertical direction, the flying and recovery of the unmanned helicopter are easily influenced, and the convenience of the unmanned helicopter is reduced by matching the take-off platform, the clamping mechanism, the telescopic mechanism, the lifting mechanism, the cabin top platform, the correction mechanism and the three-way mechanism.

Drawings

FIG. 1 is a schematic view of a takeoff platform of the present invention;

FIG. 2 is a schematic view of the telescoping mechanism of the present invention;

FIG. 3 is a schematic view of a clamping mechanism of the present invention;

FIG. 4 is a schematic view of a ceiling platform of the present invention;

FIG. 5 is a schematic view of a corrective mechanism of the present invention;

FIG. 6 is a schematic view of a three-way mechanism of the present invention;

fig. 7 is a schematic bottom view of the three-way mechanism of the present invention.

In the figure: 1 take-off platform, 2 clamping mechanisms, 3 telescopic mechanisms, 4 lifting mechanisms, 5 first supporting slide rails, 6 aluminum alloy platforms, 7 cabin top platforms, 8 second screw rod modules, 9 first screw rod modules, 10 second supporting slide rails, 11 fixed slide rails, 12 racks, 13 limiters, 14 first motors, 15 third motors, 16 transmission belts, 17 belt pulleys, 18 fixed hooks, 19 correction mechanisms, 20 three-way mechanisms, 21 first gears, 22 connecting slide rails, 23 push rods, 24 second motors, 25 first racks, 26 wire belts, 27 fixed plates, 28 rotary tables, 29 second gears, 30 fourth motors, 31 second racks, 32 movable slide rails and 33 third screw rod modules.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

The takeoff platform 1, the clamping mechanism 2, the telescopic mechanism 3, the lifting mechanism 4, the first supporting slide rail 5, the aluminum alloy platform 6, the cabin roof platform 7, the second screw rod module 8, the first screw rod module 9, the second supporting slide rail 10, the fixed slide rail 11, the frame 12, the limiter 13, the first motor 14, the third motor 15, the transmission belt 16, the belt pulley 17, the fixed hook 18, the correcting mechanism 19, the three-way mechanism 20, the first gear 21, the connecting slide rail 22, the push rod 23, the second motor 24, the first rack 25, the root line belt 26, the fixed plate 27, the rotary table 28, the second gear 29, the fourth motor 30, the second rack 31, the movable slide rail 32, the third screw rod module 33 and other components of the utility model are all common standard components or components known by technicians in the field, the structure and principle are known to those skilled in the art through technical manuals or through routine experimentation.

Referring to fig. 1-7, an unmanned aerial vehicle carrying, flying and recycling system for a shelter comprises a flying platform 1 and a cabin top platform 7, wherein a telescopic mechanism 3 is fixedly installed at the top of the flying platform 1, a clamping mechanism 2 is fixedly connected at the top of the telescopic mechanism 3, a lifting mechanism 4 is fixedly connected at the bottom of the flying platform 1, a correcting mechanism 19 and a three-way mechanism 20 are respectively and fixedly installed at the top of the cabin top platform 7, the telescopic mechanism 3 comprises an aluminum alloy platform 6, a first supporting slide rail 5 is fixedly connected at the left side of the bottom of the aluminum alloy platform 6, a second supporting slide rail 10 is fixedly connected at the right side of the bottom of the aluminum alloy platform 6, a first screw rod module 9 is fixedly connected at the left side of the second supporting slide rail 10, a fixed slide rail 11 and a second screw rod module 8 are movably connected at the top of the aluminum alloy platform 6, the tops of the fixed slide rail 11 and the second screw rod module 8 are fixedly connected with the bottom of the clamping mechanism 2, the clamping mechanism 2 comprises a rack 12, a first motor 14 is fixedly connected to the top of the rack 12, a belt pulley 17 is movably connected to the bottom of the inner wall of the rack 12 through a bearing, a transmission belt 16 is connected to the surface of the belt pulley 17 and an output shaft of the first motor 14 in a transmission manner, a fixing hook 18 is fixedly connected to the surface of the transmission belt 16, a stopper 13 is fixedly connected to the top of the rack 12, a correcting mechanism 19 comprises a connecting slide rail 22, a push rod 23 is movably connected to the top of the connecting slide rail 22, a second motor 24 is fixedly connected to the left side of the push rod 23, a root line belt 26 is arranged on the second motor 24, a first gear 21 is sleeved on the output shaft of the second motor 24, a first rack 25 is meshed to the surface of the first gear 21, the bottom of the first rack 25 is fixedly connected to the top of the cabin top platform 7, a three-way mechanism 20 comprises a third lead screw module 33, a movable slide rail 32 is movably connected to the bottom of the third lead screw module 33, the top fixedly connected with fixed plate 27 of third lead screw module 33, the bottom fixedly connected with third motor 15 of fixed plate 27, the output shaft of third motor 15 extends to the top of fixed plate 27 and fixedly connected with revolving stage 28, the fixed surface of third lead screw module 33 installs fourth motor 30, the output shaft cover of fourth motor 30 is equipped with second gear 29, the top fixedly connected with second rack 31 of cabin top platform 7, the surface of second gear 29 meshes with the surface of first rack 25 and second rack 31 respectively.

When the unmanned aerial vehicle skid clamping device is used, when the clamping mechanism 2 clamps an unmanned aerial vehicle, the output shaft of the first motor 14 drives the transmission belt 16 to rotate, the transmission belt 16 drives the belt pulley 17 to rotate, the transmission belt 16 drives the fixed hooks 18 to slide on the

rack

12, and 2 fixed hooks 18 on each transmission belt 16 can move in opposite directions or opposite directions, so that the clamping and loosening of the skid of the unmanned aerial vehicle are realized;

when the telescopic mechanism 3 transports the unmanned aerial vehicle, the aluminum alloy platform 6 can move on the first support slide rail 5 and the second support slide rail 10 under the driving of the first lead screw module 9, the clamping mechanism 2 can move on the fixed slide rail 11 under the driving of the second lead screw module 8, the transportation of the unmanned aerial vehicle can be realized, the vertical movement of the take-off platform 1 can be realized by the lifting mechanism 4, the unmanned aerial vehicle is transported to the cabin roof platform 7, the transportation of the unmanned aerial vehicle from the inside of the cabin to the outside of the cabin is realized, and the functions of fastening and the like in the transportation process are realized;

when the unmanned aerial vehicle leaves the cabin, the three-way mechanism 20 performs fitting motion, the fourth motor 30 drives the second gear 29 to rotate and can reciprocate on the second rack 31, so that the third lead screw module 33 can slide on the movable slide rail 32 in a reciprocating manner, the motion of an X axis is realized, the third lead screw module 33 stretches and retracts, the motion of a Y axis is realized, the third motor 15 drives the rotary table 28 to rotate, the rotation of a Z axis is realized, and the unmanned aerial vehicle can hook the wing to unfold to a specified angle;

when the unmanned aerial vehicle enters the cabin, the correcting mechanism 19 needs to align the unmanned aerial vehicle after the unmanned aerial vehicle falls, an output shaft of the second motor 24 drives the first gear 21 to rotate and can reciprocate on the first rack 25, so that the front push rod 23 and the rear push rod 23 can slide on the connecting slide rail 22 in a reciprocating manner, the unmanned aerial vehicle which has fallen in the falling area is pushed to correct the unmanned aerial vehicle, the three-way mechanism 20 performs fitting motion, so that wings can be hooked to recover to an appointed angle, and after the wing flap is finished, the lifting mechanism 4 and the telescopic mechanism 3 convey the unmanned aerial vehicle to a hangar in the cabin;

through the cooperation use of platform 1 that takes off, clamping mechanism 2, telescopic machanism 3, elevating system 4, cabin roof platform 7, guiding mechanism 19 and three-dimensional mechanism 20, solved current unmanned helicopter in the in-process that uses, be not convenient for carry out the wing to unmanned helicopter and open and descend the gesture and correct, be not convenient for carry out the vertical direction transportation to unmanned helicopter and press from both sides tight fixedly, influence the problem of flying and retrieving of unmanned helicopter easily, reduced the unmanned helicopter convenience.

In summary, the following steps: this unmanned aerial vehicle delivery is let to fly in cabin, recovery system, through the platform 1 that takes off, clamping mechanism 2, telescopic machanism 3, elevating system 4, cabin roof platform 7, the cooperation of guiding mechanism 19 and three-way mechanism 20 is used, the in-process of current unmanned helicopter in use has been solved, be not convenient for carry out the wing to unmanned helicopter and open and descend the gesture correction, be not convenient for carry out the vertical direction transportation and press from both sides tightly fixed to unmanned helicopter, influence the letting of unmanned helicopter and fly and retrieve easily, the problem of unmanned helicopter convenience has been reduced.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides an unmanned aerial vehicle delivery is let to fly, recovery system for shelter, includes take-off platform (1) and cabin roof platform (7), its characterized in that: the aircraft is characterized in that a telescopic mechanism (3) is fixedly mounted at the top of the takeoff platform (1), a clamping mechanism (2) is fixedly connected to the top of the telescopic mechanism (3), a lifting mechanism (4) is fixedly connected to the bottom of the takeoff platform (1), and a correcting mechanism (19) and a three-way mechanism (20) are fixedly mounted at the top of the cabin roof platform (7) respectively.

2. The system of claim 1, wherein the system comprises: telescopic machanism (3) include aluminum alloy platform (6), the first support slide rail of left side fixedly connected with (5) of aluminum alloy platform (6) bottom, the right side fixedly connected with second support slide rail (10) of aluminum alloy platform (6) bottom, the first lead screw module of left side fixedly connected with (9) of second support slide rail (10), the top swing joint of aluminum alloy platform (6) has fixed slide rail (11) and second lead screw module (8), the top of fixed slide rail (11) and second lead screw module (8) and the bottom fixed connection of clamping mechanism (2).

3. The system of claim 1, wherein the system comprises: clamping mechanism (2) include frame (12), the first motor of top fixedly connected with (14) of frame (12), there are belt pulley (17) bottom of frame (12) inner wall through bearing swing joint, the surface of belt pulley (17) and the output shaft transmission of first motor (14) are connected with drive belt (16), the fixed surface of drive belt (16) is connected with fixed hook (18), the top fixedly connected with stopper (13) of frame (12).

4. The system of claim 1, wherein the system comprises: the correcting mechanism (19) comprises a connecting slide rail (22), a push rod (23) is movably connected to the top of the connecting slide rail (22), a second motor (24) is fixedly connected to the left side of the push rod (23), a root line belt (26) is arranged on the second motor (24), a first gear (21) is sleeved on an output shaft of the second motor (24), a first rack (25) is meshed on the surface of the first gear (21), and the bottom of the first rack (25) is fixedly connected with the top of the cabin top platform (7).

5. The system of claim 1, wherein the system comprises: three-way mechanism (20) includes third lead screw module (33), the bottom swing joint of third lead screw module (33) has movable slide rail (32), the top fixedly connected with fixed plate (27) of third lead screw module (33), the bottom fixedly connected with third motor (15) of fixed plate (27), the output shaft of third motor (15) extends to the top and fixedly connected with revolving stage (28) of fixed plate (27), the fixed surface of third lead screw module (33) installs fourth motor (30), the output shaft cover of fourth motor (30) is equipped with second gear (29), the top fixedly connected with second rack (31) of cabin top platform (7), the surface of second gear (29) meshes with the surface of first rack (25) and second rack (31) respectively.