CN111572795A - Unmanned aerial vehicle takes off device and unmanned aerial vehicle conveyer - Google Patents
Unmanned aerial vehicle takes off device and unmanned aerial vehicle conveyer Download PDFInfo
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- CN111572795A CN111572795A CN202010451955.4A CN202010451955A CN111572795A CN 111572795 A CN111572795 A CN 111572795A CN 202010451955 A CN202010451955 A CN 202010451955A CN 111572795 A CN111572795 A CN 111572795A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60P—VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS
- B60P3/00—Vehicles adapted to transport, to carry or to comprise special loads or objects
- B60P3/06—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles
- B60P3/11—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles for carrying aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B35/00—Vessels or similar floating structures specially adapted for specific purposes and not otherwise provided for
- B63B35/50—Vessels or floating structures for aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
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- B64F1/005—Protective coverings for aircraft not in use
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
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Abstract
The application provides an unmanned aerial vehicle take-off device and an unmanned aerial vehicle transportation device, wherein the unmanned aerial vehicle take-off device comprises a support frame, a turnover containing body and a take-off plate; the overturning accommodating body is arranged on the supporting frame and used for accommodating the unmanned aerial vehicle; the take-off plate is arranged on the overturning accommodating body and used for fixing or unlocking the unmanned aerial vehicle; the overturning accommodating body can rotate relative to the supporting frame so as to realize the conversion of the unmanned aerial vehicle between a take-off position and an assembling position; when the unmanned aerial vehicle is in a take-off position, the take-off plate is horizontally placed; the central point of unmanned aerial vehicle when the equipment position is less than the central point of unmanned aerial vehicle at the position of taking off. This take-off device can provide a lower equipment position of height for unmanned aerial vehicle, makes things convenient for operating personnel to assemble unmanned aerial vehicle before unmanned aerial vehicle takes off, and then makes unmanned aerial vehicle can accomodate after dismantling or folding again, has reduced unmanned aerial vehicle's storage space, has reduced take-off device's volume for this unmanned aerial vehicle take-off device can be applicable to the limited region in space such as car, ship and use.
Description
Technical Field
The application relates to the technical field of unmanned aerial vehicles, particularly, relate to an unmanned aerial vehicle take-off device and unmanned aerial vehicle conveyer.
Background
Many rotor unmanned aerial vehicle obtains wide application in a plurality of fields rapidly with advantages such as the convenience of excellent performance and the vertical take-off and landing of controlling. Among the prior art, unmanned aerial vehicle's take-off device or small-size airport adopt elevating gear to realize that unmanned aerial vehicle accomodates the position and takes off the conversion of position more, and this type of unmanned aerial vehicle take-off device is owing to lack the space that can supply workman's operation equipment, consequently no matter accomodate inside the elevating platform box or when preparing to take off, and unmanned aerial vehicle is the state of having assembled already. This results in a very large take-off device volume, occupies a large amount of space, is only suitable for use in wide fixed places, and is very unfavorable for use in vehicles, ships or areas with limited space.
Disclosure of Invention
An object of the embodiment of the application provides an unmanned aerial vehicle takes off device and unmanned aerial vehicle conveyer, and this unmanned aerial vehicle takes off device can provide a high lower equipment position for unmanned aerial vehicle, makes things convenient for operating personnel to assemble unmanned aerial vehicle before unmanned aerial vehicle takes off.
The embodiment of the application provides an unmanned aerial vehicle take-off device, and this unmanned aerial vehicle take-off device includes support frame, upset receiver and takes-off board. The overturning storage body is installed on the supporting frame and comprises a storage cavity for storing the unmanned aerial vehicle. The take-off plate is installed on the overturning containing body and used for fixing or unlocking the unmanned aerial vehicle and driving the unmanned aerial vehicle to enter and exit the containing cavity. The overturning containing body can rotate relative to the supporting frame so as to realize the conversion of the unmanned aerial vehicle between a take-off position and an assembling position. When the unmanned aerial vehicle is in the takeoff position, the takeoff plate is horizontally placed. The central point of the unmanned aerial vehicle at the assembling position is lower than the central point of the unmanned aerial vehicle at the takeoff position.
In the above-mentioned realization process, at general storage state, unmanned aerial vehicle accomodates in the storage cavity of the upset storage body after dismantling or folding. When needs start unmanned aerial vehicle and take off, at first drive unmanned aerial vehicle to accomodate the chamber through taking off the board outside. If take-off board drives unmanned aerial vehicle and accomodates external back to the upset, unmanned aerial vehicle's position is higher, and operating personnel assembles inconveniently, and rotatable upset storage body this moment rotates unmanned aerial vehicle to lower position and assembles the position promptly to operating personnel assembles. If take-off the board and drive unmanned aerial vehicle and accomodate external back to the upset, the position that unmanned aerial vehicle was located has been lower, convenient equipment, and operating personnel can directly assemble unmanned aerial vehicle on this position, and this position can regard as the equipment position. After the unmanned aerial vehicle equipment is complete, rotate the upset receiver and make unmanned aerial vehicle reach the position of taking off, take off the board level and place, unmanned aerial vehicle is in the state of being prepared for war, can take off at any time.
Another mode still can at first rotate the upset receiver to predetermined angle, then move unmanned aerial vehicle to the storage chamber outside this predetermined angle, unmanned aerial vehicle just is in the position of lower convenient equipment this moment, later operating personnel assembles unmanned aerial vehicle at this equipment position, and the back is accomplished in the equipment, rotates the upset receiver and makes unmanned aerial vehicle reach the position of taking off, and unmanned aerial vehicle can take off on taking off the board afterwards.
Therefore, the action of moving the unmanned aerial vehicle to the outside of the containing cavity and the action of rotating the turnover containing body to enable the unmanned aerial vehicle outside the containing cavity to be located at the assembling position are not in sequence, and a proper operation sequence can be selected according to the requirements and actual conditions of operators.
To sum up, above-mentioned unmanned aerial vehicle take-off device provides a lower equipment position of height for unmanned aerial vehicle, makes things convenient for operating personnel to assemble unmanned aerial vehicle before unmanned aerial vehicle takes off, and then makes unmanned aerial vehicle accomodate after dismantling or folding, has reduced unmanned aerial vehicle's storage space, has reduced take-off device's volume for this unmanned aerial vehicle take-off device can be applicable to the limited region in space such as car, ship and use.
In a possible implementation manner, the take-off plate is rotatably connected to the turnover storage body, and the take-off plate rotates relative to the turnover storage body so as to enable the unmanned aerial vehicle to enter and exit the storage body cavity.
In the above-mentioned realization process, the board of taking off realizes unmanned aerial vehicle business turn over through pivoted action and accomodates the chamber, compares and realizes unmanned aerial vehicle business turn over storage space through elevation structure among the prior art, rotates connection structure simple, convenient operation.
In a possible implementation manner, a storage window communicated with the storage cavity is formed in the turnover storage body, a rotating shaft is arranged at a window edge close to the storage window, and one side edge of the take-off plate is fixedly mounted on the rotating shaft.
In the implementation process, one side edge of the take-off plate is fixedly mounted on the rotating shaft, the rotating shaft rotates to drive the take-off plate to enter and exit the storage window, and when the take-off plate rotates to be parallel to the storage window, namely the take-off plate covers the storage window, the unmanned aerial vehicle reaches an assembly position; when taking off the board and rotate along the axis of rotation and receive in the window, unmanned aerial vehicle is accomodate to accomodating the intracavity.
In a possible implementation manner, a first locking device is further arranged on the turnover containing body; the first locking device is used for locking the takeoff plate after the takeoff plate rotates to a preset position.
In the above-mentioned realization in-process, when taking off the board and driving unmanned aerial vehicle and rotate and accomodate the intracavity, when unmanned aerial vehicle reachd the position of accomodating promptly, the board of taking off is locked to first locking device, with unmanned aerial vehicle fixed mounting in accomodating the chamber to make unmanned aerial vehicle accomodate in accomodating the chamber firmly, prevent that unmanned aerial vehicle from taking place to rock in the transportation, with protection unmanned aerial vehicle's structure. When taking off the board and driving unmanned aerial vehicle and rotate to the equipment position or accomodate window department, first locking device will take off the board locking for take off board and upset storage body fixed connection make things convenient for operating personnel to assemble unmanned aerial vehicle on the one hand, and on the other hand also makes the board of taking off immovable, provides a firm platform of taking off for taking off of follow-up unmanned aerial vehicle.
In a possible implementation manner, a first driving device is arranged on the turnover containing body; the first driving device is used for driving the take-off plate to rotate relative to the overturning containing body.
In the implementation process, the first driving device is arranged to realize automatic rotation of the take-off plate, manpower is liberated, and automation is improved.
In a possible implementation manner, the supporting frame comprises a turning shaft, and the turning storage body is rotatably connected to the supporting frame through the turning shaft.
In the implementation process, the turnover containing body is connected with the support frame in a rotating mode through the turnover shaft, and the turnover containing body is simple in structure and convenient to operate.
Specifically, the overturning shaft comprises a first rotating shaft and a second rotating shaft, the axis of the first rotating shaft and the axis of the second rotating shaft are on the same straight line, the first rotating shaft and the second rotating shaft are respectively arranged on two sides of the overturning containing body, and one end of the first rotating shaft and one end of the second rotating shaft are fixedly installed on the overturning containing body. The support frame also comprises a base, the first rotating shaft and the second rotating shaft are respectively arranged on two sides of the base, and the first rotating shaft and the second rotating shaft are rotatably arranged on the base. The first rotating shaft and the second rotating shaft rotate on the base so as to drive the turnover containing body to rotate relative to the base.
In a possible implementation manner, the second driving device is arranged on the supporting frame and is used for driving the turnover containing body to rotate relative to the supporting frame.
In the implementation process, the second driving device is arranged, so that the turnover containing body can be automatically turned over, manpower is liberated, and automation is realized.
In a possible implementation manner, a second locking device is arranged on the support frame, and the second locking device is used for locking the turnover storage body when the unmanned aerial vehicle reaches the takeoff position or the assembly position.
In the above-mentioned realization process, when unmanned aerial vehicle reachd the equipment position, adopt second locking device locking upset storage body, can provide a stable operation platform for operating personnel, make things convenient for operating personnel to assemble unmanned aerial vehicle. When unmanned aerial vehicle reachd the position of taking off, adopt second locking device locking upset receiver, can be so that the upset receiver is fixed motionless, and then provide firm platform of taking off for unmanned aerial vehicle's taking off.
In one possible implementation, the flip angle of the flip-up receptacle from the takeoff position to the assembly position is 90 °.
In the implementation process, the turnover containing body is turned over by 90 degrees from the takeoff position to reach the assembly position, and when the unmanned aerial vehicle is at the takeoff position, the takeoff plate is horizontally placed; when the drone is in the assembly position, the takeoff board is placed vertically. When the equipment position, unmanned aerial vehicle is located the side of upset storage body, can provide bigger operating space for operating personnel, and the operating personnel of being convenient for assembles unmanned aerial vehicle.
In a second aspect, an embodiment of the present application further provides an unmanned aerial vehicle transportation device, where the unmanned aerial vehicle takeoff device of one or more of the first aspects is configured on the unmanned aerial vehicle transportation device.
In the above embodiment, the takeoff device is configured on the unmanned aerial vehicle transportation device, so that the takeoff place of the unmanned aerial vehicle can be flexibly changed, and the transportation of the unmanned aerial vehicle is facilitated.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present application, the drawings that are required to be used in the embodiments of the present application will be briefly described below, it should be understood that the following drawings only illustrate some embodiments of the present application and therefore should not be considered as limiting the scope, and that those skilled in the art can also obtain other related drawings based on the drawings without inventive efforts.
Fig. 1 is a structural diagram of an unmanned aerial vehicle located at a takeoff position according to an embodiment of the present application;
fig. 2 is an unassembled structure view of an unmanned aerial vehicle in an assembled position according to an embodiment of the present disclosure;
fig. 3 is a structural diagram of an unmanned aerial vehicle provided in an embodiment of the present application after being assembled at an assembly position;
fig. 4 is a structural diagram of another unmanned aerial vehicle accommodated in an overturning accommodating body according to the embodiment of the present application;
FIG. 5 is a block diagram of a take-off plate according to an embodiment of the present disclosure;
fig. 6 is a structure diagram of an unmanned aerial vehicle conveyer that this application embodiment provided.
Icon: 100-a support frame; 200-turning over the containing body; 210-a receiving window; 220-a rotating shaft; 230-a receiving cavity; 300-take-off plate; 310-a briquette structure; 320-a landing rack groove; 110-a turning shaft; 400-a second drive; 500-a first locking device; 600-unmanned aerial vehicle.
Detailed Description
The technical solutions in the embodiments of the present application will be described below with reference to the drawings in the embodiments of the present application.
It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, it need not be further defined and explained in subsequent figures. Meanwhile, in the description of the present application, the terms "first", "second", and the like are used only for distinguishing the description, and are not to be construed as indicating or implying relative importance.
Referring to fig. 1, fig. 2, fig. 3 and fig. 4, an unmanned aerial vehicle takeoff device provided in an embodiment of the present application includes a support frame 100, a turning storage body 200 and a takeoff plate 300. The turnover storage body 200 is installed on the support frame 100, and the turnover storage body 200 includes a storage cavity 230 for storing the unmanned aerial vehicle 600. The take-off plate 300 is installed on the roll-over storage body 200, and is used to fix or unlock the drone 600. The flip receiving body 200 can rotate relative to the support frame 100 to realize the conversion of the drone 600 between the takeoff position and the assembly position. When the drone 600 is in the takeoff position, the takeoff board 300 is placed horizontally. The center point of drone 600 when in the assembly position is lower than the center point of drone 600 in the takeoff position.
In the above implementation process, in a general storage state, the drone 600 is stored in the storage cavity 230 of the turnover storage body 200 after being detached or folded. When the unmanned aerial vehicle 600 needs to be started to take off, the unmanned aerial vehicle 600 is firstly driven to the outside of the storage cavity 230 through the take-off plate 300. If take-off board 300 drives unmanned aerial vehicle 600 and accomodates body 200 outer back to the upset, unmanned aerial vehicle 600's position is higher, and operating personnel assembles inconveniently, and rotatable upset accomodate body 200 this moment rotates unmanned aerial vehicle 600 to lower position and assembles the position promptly to operating personnel assembles. If take-off board 300 drives unmanned aerial vehicle 600 and accomodates the body 200 outer back to the upset, the position that unmanned aerial vehicle 600 was located has been lower, convenient equipment, and operating personnel can directly assemble unmanned aerial vehicle 600 on this position, and this position can regard as the equipment position. After the unmanned aerial vehicle 600 equipment is complete, rotate upset storage body 200 and make unmanned aerial vehicle 600 reach the position of taking off, take off board 300 level and place, unmanned aerial vehicle 600 is in the state of being prepared for war, can take off at any time.
Another mode, still can first rotate the upset receiver 200 to predetermined angle, then move unmanned aerial vehicle 600 outside storage chamber 230 at this predetermined angle, unmanned aerial vehicle 600 just is in the position of lower convenient equipment this moment, later operating personnel assembles unmanned aerial vehicle 600 at this equipment position, and after the equipment is accomplished, rotate upset receiver 200 and make unmanned aerial vehicle 600 reach the position of taking off, unmanned aerial vehicle 600 can take off on the board 300 of taking off afterwards.
Therefore, the action of moving the unmanned aerial vehicle 600 out of the storage cavity 230 and the action of rotating the turnover storage body 200 to enable the unmanned aerial vehicle 600 out of the storage cavity 230 to be in the assembly position are not in sequence, and a proper operation sequence can be selected according to the requirements and actual conditions of operators.
To sum up, above-mentioned unmanned aerial vehicle take-off device provides a lower equipment position of height for unmanned aerial vehicle 600, makes things convenient for operating personnel to assemble unmanned aerial vehicle 600 before unmanned aerial vehicle 600 takes off, and then makes unmanned aerial vehicle 600 accomodate after dismantling or folding, has reduced unmanned aerial vehicle 600's storage space, has reduced the volume of the device of taking off for this unmanned aerial vehicle take-off device can be applicable to the limited region in space such as car, ship and use.
It should be understood that above-mentioned unmanned aerial vehicle take-off device not only can be applicable to the limited region in space such as car, ship, also can be applicable to region such as roof, ground.
It should be noted that, the above-mentioned assembly position does not refer to a specific position, and all positions or orientations that are lower than the takeoff position and that are convenient for the operator to assemble the drone 600 all belong to the above-mentioned assembly position, and this is not limited in the embodiment of the present application.
It should be understood that the takeoff position of the drone 600 described above refers to the takeoff board 300 being placed horizontally, so that the takeoff board can provide a horizontal takeoff platform for the drone 600.
The turning direction of the turnover receiving body 200 with respect to the supporting frame 100 may be clockwise or counterclockwise. The flip receiving body 200 may be in the form of a box, a cantilever, a frame, and the like, which is not limited in the embodiment of the present application.
Referring to fig. 4, in a possible implementation manner, the takeoff plate 300 is rotatably connected to the turning storage body 200, and the takeoff plate 300 rotates relative to the turning storage body 200 to enable the unmanned aerial vehicle 600 to enter and exit the storage cavity 230.
In the above-mentioned realization process, take-off board 300 realizes that unmanned aerial vehicle 600 passes in and out through the pivoted action and accomodates chamber 230, compares and realizes that unmanned aerial vehicle 600 passes in and out through elevation structure and accomodates the chamber among the prior art, rotates connection structure simple, convenient operation.
It should be noted that the manner of rotationally connecting the takeoff plate 300 and the turnover storage body 200 is various, and the takeoff plate 300 may be rotationally connected to the turnover storage body 200 through a hinge, or may be rotationally connected to the turnover storage body 200 through a rotation shaft 220, which is not limited in the embodiment of the present application.
In a possible implementation manner, please refer to fig. 5, a plurality of press block structures 310 and two landing gear slots 320 are disposed on the takeoff plate 300, and the size, depth and position of the landing gear slots 320 are matched with the span and diameter of the landing gear of the unmanned aerial vehicle 600 for installing the landing gear of the unmanned aerial vehicle 600. The press block structure 310 is used to fix the landing gear of the drone 600 on the takeoff plate 300. The mass structure 310 may both hold down the landing gear from rocking and unlock the landing gear during takeoff.
In a possible implementation manner, the turnover receiving body 200 is provided with a receiving window 210 communicated with the receiving cavity 230, a rotating shaft 220 is arranged at a window edge close to the receiving window 210, and one side of the take-off plate 300 is fixedly mounted on the rotating shaft 220.
In the implementation process, one side of the take-off plate 300 is fixedly mounted on the rotating shaft 220, the rotating shaft 220 rotates to drive the take-off plate 300 to enter or exit the storage window 210, and when the take-off plate 300 rotates to be parallel to the storage window 210, that is, when the take-off plate 300 covers the storage window 210, the unmanned aerial vehicle 600 reaches the assembly position; when the takeoff plate 300 rotates along the rotation shaft 220 into the receiving window 210, the drone 600 is received into the receiving cavity 230.
In a possible implementation, the turnover container 200 is further provided with a first locking device 500; the first locking device 500 is used for locking the take-off plate 300 after the take-off plate 300 is rotated to a predetermined position.
In the above-mentioned realization process, when taking off board 300 and driving unmanned aerial vehicle 600 and rotate to storage chamber 230 in, when unmanned aerial vehicle 600 reachd the storage position promptly, first locking device 500 locks taking off board 300, with unmanned aerial vehicle 600 fixed mounting at storage chamber 230 to make unmanned aerial vehicle 600 accomodate at storage chamber 230 firmly, prevent that unmanned aerial vehicle 600 from taking place to rock in the transportation, with the structure of protection unmanned aerial vehicle 600. When taking off board 300 and driving unmanned aerial vehicle 600 and rotate to the assembly position or accomodate window 210 department, first locking device 500 will take off board 300 locking for take off board 300 and upset storage body 200 fixed connection make things convenient for operating personnel to assemble unmanned aerial vehicle 600 on the one hand, and on the other hand also makes take off board 300 fixed motionless, provides a firm platform of taking off for taking off of follow-up unmanned aerial vehicle 600.
Specifically, the first locking device 500 may include a first set of locks mounted at the receiving cavity 230 to lock the take-off plate 300 at the receiving cavity 230, and a second set of locks mounted at the receiving window 210 to lock the take-off plate 300 at the receiving window 210. Further, the first set of locking members or the second set of locking members each comprise a plurality of mortise locks. The mortise lock comprises a movable plug-in unit and a locking hole matched with the movable plug-in unit. The mobile plug-in unit can be installed on the take-off plate 300, and the corresponding locking hole is installed on the turnover receiving body 200; the mobile plug-in may also be mounted on the roll-over receptacle 200, with the corresponding locking hole provided on the take-off plate 300. When the mobile plug-in is installed on the takeoff board 300, the mobile plug-in can slide relative to the takeoff board 300 and extend into or out of the locking hole on the turnover storage body 200, so as to realize locking and unlocking of the takeoff board 300.
In a possible implementation manner, a first driving device is arranged on the turnover containing body 200; the first driving device is used for driving the take-off plate 300 to rotate relative to the overturning receiving body 200.
In the implementation process, the first driving device is arranged to realize automatic rotation of the take-off plate 300, manpower is liberated, and automation is improved. The first driving device may be used for the rotation connection structure between the take-off plate 300 and the flip receiving body 200, for example, the rotation shaft 220, or may be used for the take-off plate 300.
It should be understood that the first driving device may be a motor-driven, hydraulic, cylinder-driven, or gear-driven driving device. In addition, the takeoff plate 300 can be driven to rotate by manual driving.
In combination with the above embodiments, when the unmanned aerial vehicle 600 needs to be started to operate, the takeoff plate 300 is rotated by the first driving device, so that the unmanned aerial vehicle 600 rotates from the storage cavity 230 (shown in fig. 4) to the outside of the turnover storage body 200 to the assembly position (shown in fig. 2), and the takeoff plate 300 is locked by the first locking device 500. The operating personnel assembles unmanned aerial vehicle 600, and the equipment back is shown in fig. 3, then drives upset receiver 200 through second drive arrangement 400 and rotates for unmanned aerial vehicle 600 rotates to the position of taking off (as shown in fig. 1), and at this moment, unmanned aerial vehicle 600 gets into the state of being prepared for war, reaches when and takes off after the instruction, and unmanned aerial vehicle 600 starts, and unmanned aerial vehicle 600's screw rotates, gets into the idle state. The briquetting mechanism of the take-off plate 300 is unlocked and opened, and the unmanned aerial vehicle 600 is no longer limited in vertical degree of freedom. The operating personnel continues to send signals to the unmanned aerial vehicle 600, and the unmanned aerial vehicle 600 refuels take off and lift off.
In an embodiment, the takeoff plate 300 is rotatably connected to the turning storage body 200 through the rotating shaft 220, the first driving device is a motor, and an output shaft of the motor is fixedly connected to the rotating shaft 220 to drive the rotating shaft 220 to rotate.
In a possible implementation manner, the supporting stand 100 includes a turning shaft 110, and the turning storage body 200 is rotatably connected to the supporting stand 100 through the turning shaft 110.
In the implementation process, the turnover containing body 200 is rotatably connected with the support frame 100 through the turnover shaft 110, and the turnover containing body is simple in structure and convenient to operate.
Specifically, the turning shaft 110 includes a first rotating shaft and a second rotating shaft, the axis of the first rotating shaft and the axis of the second rotating shaft are on the same straight line, the first rotating shaft and the second rotating shaft are respectively disposed at two sides of the turning storage body 200, and one end of the first rotating shaft and one end of the second rotating shaft are fixedly mounted on and turn the storage body 200. The supporting frame 100 further includes a base, and the first rotating shaft and the second rotating shaft are respectively disposed on two sides of the base, and both the first rotating shaft and the second rotating shaft are rotatably mounted on the base. The first rotating shaft and the second rotating shaft rotate on the base to drive the turnover containing body 200 to rotate relative to the base.
In a possible implementation manner, the second driving device 400 is disposed on the supporting frame 100, and the second driving device 400 is configured to drive the turnover receiving body 200 to rotate relative to the supporting frame 100.
In the implementation process, the second driving device 400 is arranged, so that the turnover containing body 200 can be automatically turned over, manpower is liberated, and automation is achieved. It should be understood that the second driving device 400 may be a motor-driven, hydraulic, cylinder-driven, or gear-driven driving device. In addition, the turnover container 200 can be driven to turn over manually by manpower.
In a possible implementation, a second locking device is provided on the support frame 100, and the second locking device is used for locking the turnover receiving body 200 when the unmanned aerial vehicle 600 reaches the takeoff position or the assembly position.
In the above-mentioned realization process, when unmanned aerial vehicle 600 reachd the equipment position, adopt second locking device locking upset receiver 200, can provide a stable operation platform for operating personnel, make things convenient for operating personnel to assemble unmanned aerial vehicle 600. When unmanned aerial vehicle 600 arrived the position of taking off, adopt second locking device locking upset storage body 200, can make upset storage body 200 fixed motionless, and then provide firm platform of taking off for unmanned aerial vehicle 600 takes off.
The locking of the flip storage body 200 means that the flip storage body 200 is fixed to the stand 100. In addition, the turnover containing body 200 can be locked by the second driving device 400, that is, the turnover containing body 200 is automatically locked after the second driving device 400 drives the turnover containing body 200 to rotate to a predetermined position. For example, the second driving device 400 is a motor, and an output shaft of the motor is fixedly connected to the first rotating shaft or the second rotating shaft. After the turnover containing body 200 rotates to a preset angle, the motor is turned off, and the output shaft of the motor does not rotate any more, so that the turnover containing body 200 is locked.
The turning angle of the turning storage body 200 from the take-off position to the assembly position may be 30 °, 45 °, 60 °, 90 °, 110 °, and the like, which is not limited in the embodiment of the present application.
In one possible implementation, the flip angle of the flip container 200 from the takeoff position to the assembly position is 90 °.
In the implementation process, the turnover containing body 200 is turned 90 degrees from the takeoff position to reach the assembly position, and when the unmanned aerial vehicle 600 is at the takeoff position, the takeoff plate 300 is horizontally placed; when the drone 600 is in the assembled position, the takeoff board 300 is placed vertically. When the equipment position, unmanned aerial vehicle 600 is located the side of upset storage body 200, can provide bigger operating space for operating personnel, and the operating personnel of being convenient for assembles unmanned aerial vehicle 600.
Referring to fig. 6, an embodiment of the present application further provides an unmanned aerial vehicle transportation device, and one or more unmanned aerial vehicle take-off devices described in any of the above embodiments are configured on the unmanned aerial vehicle transportation device.
In the above embodiment, the takeoff device is configured on the unmanned aerial vehicle transportation device, so that the takeoff place of the unmanned aerial vehicle 600 can be flexibly changed, and the transportation of the unmanned aerial vehicle 600 is facilitated.
It should be understood that the above-mentioned unmanned aerial vehicle conveyer can be vehicles such as vehicles, boats and ships, and this application embodiment does not limit this.
The above description is only an example of the present application and is not intended to limit the scope of the present application, and various modifications and changes may be made by those skilled in the art. Any modification, equivalent replacement, improvement and the like made within the spirit and principle of the present application shall be included in the protection scope of the present application. It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, it need not be further defined and explained in subsequent figures.
The above description is only for the specific embodiments of the present application, but the scope of the present application is not limited thereto, and any person skilled in the art can easily conceive of the changes or substitutions within the technical scope of the present application, and shall be covered by the scope of the present application. Therefore, the protection scope of the present application shall be subject to the protection scope of the claims.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.
Claims (10)
1. An unmanned aerial vehicle take-off device, its characterized in that includes:
a support frame;
the overturning accommodating body is arranged on the supporting frame and comprises an accommodating cavity for accommodating the unmanned aerial vehicle;
the take-off plate is arranged on the overturning accommodating body and used for fixing or unlocking the unmanned aerial vehicle and driving the unmanned aerial vehicle to enter or exit the accommodating cavity;
the overturning accommodating body can rotate relative to the supporting frame so as to realize the conversion of the unmanned aerial vehicle between a take-off position and an assembling position;
when the unmanned aerial vehicle is at a take-off position, the take-off plate is horizontally placed; the central point of the unmanned aerial vehicle at the assembling position is lower than the central point of the unmanned aerial vehicle at the takeoff position.
2. The takeoff device of the unmanned aerial vehicle of claim 1, wherein the takeoff plate is rotatably connected to the overturning receiving body, and the takeoff plate rotates relative to the overturning receiving body to enable the unmanned aerial vehicle to enter and exit the receiving cavity.
3. The takeoff device of the unmanned aerial vehicle as claimed in claim 2, wherein the overturning accommodating body is provided with an accommodating window communicated with the accommodating cavity, a rotating shaft is arranged at a position close to the window edge of the accommodating window, and one side edge of the takeoff plate is fixedly mounted on the rotating shaft.
4. The unmanned aerial vehicle take-off device of claim 2, wherein a first locking device is further disposed on the roll-over receptacle;
the first locking device is used for locking the takeoff plate after the takeoff plate rotates to a preset position.
5. The unmanned aerial vehicle take-off device of claim 2, wherein a first drive device is disposed on the roll-over receptacle;
the first driving device is used for driving the take-off plate to rotate relative to the overturning containing body.
6. The unmanned aerial vehicle take-off device of any one of claims 1 to 5, wherein the support frame comprises a turning shaft, and the turning storage body is rotatably connected to the support frame through the turning shaft.
7. An unmanned aerial vehicle takeoff device as claimed in any one of claims 1 to 5, wherein a second drive means on the support frame;
the second driving device is used for driving the turnover containing body to rotate relative to the supporting frame.
8. An unmanned aerial vehicle take-off device as claimed in any one of claims 1 to 5, wherein a second locking device is provided on the support frame;
the second locking device is used for locking the overturning containing body when the unmanned aerial vehicle reaches the take-off position or the assembling position.
9. An unmanned aerial vehicle takeoff device as claimed in any one of claims 1 to 5, wherein a flip angle at which the flip-up receptacle is flipped from the takeoff position to the assembly position is 90 °.
10. An unmanned aerial vehicle transportation device, wherein one or more unmanned aerial vehicle take-off devices of any one of claims 1-9 are configured on the unmanned aerial vehicle transportation device.
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| CN202010451955.4A CN111572795B (en) | 2020-05-25 | 2020-05-25 | Unmanned aerial vehicle takes off device and unmanned aerial vehicle conveyer |
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| Application Number | Priority Date | Filing Date | Title |
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| CN202010451955.4A CN111572795B (en) | 2020-05-25 | 2020-05-25 | Unmanned aerial vehicle takes off device and unmanned aerial vehicle conveyer |
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| CN111572795B CN111572795B (en) | 2022-04-22 |
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| WO2024033582A1 (en) * | 2022-08-09 | 2024-02-15 | Atechsys Engineering (Ate) | Docking system for a flying delivery drone and improved delivery vehicle |
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| CN111572795B (en) | 2022-04-22 |
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