CN111874250A - Unmanned aerial vehicle outdoor operations equipment - Google Patents

Unmanned aerial vehicle outdoor operations equipment Download PDF

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Publication number
CN111874250A
CN111874250A CN202010758404.2A CN202010758404A CN111874250A CN 111874250 A CN111874250 A CN 111874250A CN 202010758404 A CN202010758404 A CN 202010758404A CN 111874250 A CN111874250 A CN 111874250A
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CN
China
Prior art keywords
unmanned aerial
aerial vehicle
centering
lifting mechanism
drive
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Pending
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CN202010758404.2A
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Chinese (zh)
Inventor
芦志明
卫大为
曹亚兵
严凯
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Fuya Intelligent Technology Taicang Co ltd
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Fuya Intelligent Technology Taicang Co ltd
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Publication date
Application filed by Fuya Intelligent Technology Taicang Co ltd filed Critical Fuya Intelligent Technology Taicang Co ltd
Priority to CN202010758404.2A priority Critical patent/CN111874250A/en
Publication of CN111874250A publication Critical patent/CN111874250A/en
Pending legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND 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
    • B64F1/00Ground or aircraft-carrier-deck installations
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • B64C27/08Helicopters with two or more rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Forklifts And Lifting Vehicles (AREA)

Abstract

The invention belongs to the technical field of unmanned aerial vehicle use, and discloses an outdoor operation device of an unmanned aerial vehicle. This unmanned aerial vehicle outdoor operations equipment includes: the unmanned aerial vehicle comprises a frame and a carrying platform, wherein the carrying platform is arranged in the frame in a sliding manner and used for carrying the unmanned aerial vehicle; the lifting mechanism is arranged on the frame and is configured to bear the unmanned aerial vehicle and drive the unmanned aerial vehicle to move up and down along the vertical direction; dial oar mechanism, it sets up on elevating system, dials oar mechanism and is configured into the screw of stirring unmanned aerial vehicle for unmanned aerial vehicle's descending. This unmanned aerial vehicle outdoor operations equipment, microscope carrier form drawer type structure for unmanned aerial vehicle accomodate, realize the loading function. Elevating system can bear unmanned aerial vehicle and drive it along vertical direction elevating movement to fly required high altitude environment for unmanned aerial vehicle provides, thereby realize the function of flying. When unmanned aerial vehicle descends, dial oar mechanism and can stir unmanned aerial vehicle's screw to draw in the screw, the unmanned aerial vehicle's of being convenient for descending, convenience of use nature is good.

Description

Unmanned aerial vehicle outdoor operations equipment
Technical Field
The invention relates to the technical field of unmanned aerial vehicle use, in particular to an unmanned aerial vehicle outdoor operation device.
Background
The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle is applied to the fields of aerial photography, wild animal observation, mapping, news reporting, power inspection, disaster relief, film and television shooting and the like, and the application of the unmanned aerial vehicle is greatly expanded.
At present, in trades such as electric wire netting traffic forestry, when using unmanned aerial vehicle to carry out outdoor data collection, the user can face unmanned aerial vehicle safe transportation, outdoor charge and many equipment inconvenient carry and fly away management scheduling problem for the manual work scope is wide, and the degree of difficulty is big, and user's convenience is not good, is difficult to satisfy diversified demand.
Disclosure of Invention
The invention aims to provide outdoor operation equipment of an unmanned aerial vehicle, which realizes the functions of loading and flying of the unmanned aerial vehicle and has good use convenience.
In order to achieve the purpose, the invention adopts the following technical scheme:
an unmanned aerial vehicle outdoor operations equipment, includes:
the unmanned aerial vehicle comprises a frame and a carrying platform, wherein the carrying platform is arranged in the frame in a sliding manner and is used for carrying the unmanned aerial vehicle;
the lifting mechanism is arranged on the frame and is configured to bear the unmanned aerial vehicle and drive the unmanned aerial vehicle to move up and down along a vertical direction;
dial oar mechanism, it set up in on the elevating system, dial oar mechanism and be configured as and stir unmanned aerial vehicle's screw, be used for unmanned aerial vehicle's descending.
Preferably, the elevating mechanism includes:
a lifting platform for carrying the drone;
and the output end of the lifting driving source is connected to the lifting platform, and the lifting driving source can drive the lifting platform to perform lifting motion.
Preferably, the paddle-pulling mechanism comprises:
a first paddle assembly configured to secure an inboard wing of the propeller;
a second paddle assembly configured to paddle an outboard wing of the propeller.
Preferably, the first paddle assembly includes:
the lifting mechanism is provided with a containing through groove, and the rotating shaft is arranged in the containing through groove;
the reset piece is sleeved on the rotating shaft, and two ends of the reset piece are abutted against the inner wall of the accommodating through groove;
the first deflector rod penetrates through the accommodating through groove and is sleeved on the rotating shaft;
and the first driving part can abut against the bottom of the first deflector rod, so that the first deflector rod rotates relative to the rotating shaft and is selectively arranged in the accommodating through groove for fixing the inner wing.
Preferably, the first driving part includes:
the turntable is arranged on the lifting mechanism, and a pressing block is arranged on the outer side surface of the turntable;
and the output end of the rotary driving source is connected to the turntable, and the rotary driving source can drive the turntable to rotate so that the pressing block abuts against the bottom of the first driving lever.
Preferably, the second paddle assembly includes:
the second deflector rod is arranged on the outer side of the lifting mechanism;
and the second driving component is connected to the second driving lever, and can drive the second driving lever to horizontally move so that the second driving lever can drive the outer wing to be driven.
Preferably, the second driving part includes:
the driving chain wheel is rotationally arranged on the lifting mechanism;
a driven sprocket rotatably provided on the lifting mechanism;
the chain is arranged around the lifting mechanism and connected to the second driving lever, and the chain is meshed with the driving chain wheel and the driven chain wheel respectively;
and the output end of the rotary driving piece is connected to the driving chain wheel, and the rotary driving piece can drive the driving chain wheel to rotate and drive the chain and the second driving lever to move.
Preferably, the unmanned aerial vehicle further comprises a centering mechanism, the centering mechanism is arranged on the lifting mechanism, and the centering mechanism is configured to abut against the outer side of the unmanned aerial vehicle, so that the unmanned aerial vehicle is located in the center of the lifting mechanism.
Preferably, the centering mechanism includes:
the two first centering rods are respectively arranged on one group of opposite sides of the lifting mechanism;
the two second centering rods are respectively arranged on the other opposite sides of the lifting mechanism, and the second centering rods are perpendicular to the first centering rods;
the middle returning driving source is in transmission connection with the first middle returning rod and the second middle returning rod respectively, and the middle returning driving source can drive the first middle returning rod and the second middle returning rod to move towards the direction close to or away from each other and can abut against the outer sides of the two adjacent sides of the unmanned aerial vehicle.
Preferably, the frame further comprises a shock absorbing member disposed outside the frame.
The invention has the beneficial effects that:
according to the outdoor operation equipment for the unmanned aerial vehicle, the carrying platform is arranged in the frame in a sliding mode, so that the carrying platform forms a drawer type structure, the unmanned aerial vehicle is carried on the carrying platform and used for accommodating the unmanned aerial vehicle, an operator pushes and pulls the carrying platform, the unmanned aerial vehicle can be conveniently taken and placed, and a loading function is achieved. When the unmanned aerial vehicle needs to fly away, the unmanned aerial vehicle on the microscope carrier is placed on the lifting mechanism by an operator, and the lifting mechanism can bear the unmanned aerial vehicle and drive the unmanned aerial vehicle to move up and down along the vertical direction, so that the unmanned aerial vehicle is provided with a high-altitude environment required for flying away, and the flying function is realized. When unmanned aerial vehicle descends, dial oar mechanism and can stir unmanned aerial vehicle's screw to draw in the screw, the unmanned aerial vehicle's of being convenient for descending, convenience of use nature is good.
Drawings
FIG. 1 is a schematic structural diagram of an unmanned aerial vehicle outdoor operation device of the present invention;
FIG. 2 is a schematic structural view of the hidden lifting mechanism of the outdoor unmanned aerial vehicle operation equipment;
FIG. 3 is a schematic structural diagram of a lifting mechanism in the outdoor working equipment of the unmanned aerial vehicle of the present invention;
FIG. 4 is a schematic structural view of a view angle of a lifting platform in the unmanned aerial vehicle outdoor work equipment of the present invention;
fig. 5 is a schematic structural view of another view angle of the elevating platform in the unmanned aerial vehicle outdoor operation equipment;
fig. 6 is a schematic structural view of the display centering mechanism of the unmanned aerial vehicle outdoor operation equipment.
In the figure:
100. an unmanned aerial vehicle;
1. a frame; 2. a stage; 3. a lifting mechanism; 4. a paddle shifting mechanism; 5. an operation panel; 6. a safety grating; 7. an electric appliance cabinet; 8. a shock absorbing member; 9. a centering mechanism;
31. a lifting platform; 311. an accommodating through groove; 32. a lifting drive source; 33. a guide member; 34. a guide bar;
41. a first paddle assembly; 42. a second paddle assembly;
411. a first shift lever; 412. a first drive member; 4121. a turntable; 4122. a pressing block; 4123. a rotary drive source;
421. a second deflector rod; 422. a second drive member; 4221. a drive sprocket; 4222. a driven sprocket; 4223. a chain; 4224. a rotary drive member;
91. a first centering rod; 92. a second centering rod; 93. a middle returning driving source; 94. a drive rope; 95. a driving wheel.
Detailed Description
In order to make the technical problems solved, technical solutions adopted and technical effects achieved by the present invention clearer, the technical solutions of the embodiments of the present invention will be described in further detail below with reference to the accompanying drawings, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all 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.
In the description of the present invention, unless expressly stated or limited otherwise, the terms "connected," "connected," and "fixed" are to be construed broadly, e.g., as meaning permanently connected, removably connected, or integral to one another; can be mechanically or electrically connected; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
In the present invention, unless otherwise expressly stated or limited, "above" or "below" a first feature means that the first and second features are in direct contact, or that the first and second features are not in direct contact but are in contact with each other via another feature therebetween. Also, the first feature being "on," "above" and "over" the second feature includes the first feature being directly on and obliquely above the second feature, or merely indicating that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature includes the first feature being directly under and obliquely below the second feature, or simply meaning that the first feature is at a lesser elevation than the second feature.
The technical scheme of the invention is further explained by the specific implementation mode in combination with the attached drawings.
The embodiment provides unmanned aerial vehicle outdoor operations equipment for the transportation and use process of unmanned aerial vehicle 100. Unmanned aerial vehicle outdoor operations equipment is preferred to be set up on the car, forms on-vehicle unmanned aerial vehicle outdoor operations equipment, realizes charging and remote monitoring in the car, and the unmanned aerial vehicle 100 of being convenient for uses in the open air. As shown in fig. 1-2, this unmanned aerial vehicle outdoor operations equipment includes frame 1, microscope carrier 2, elevating system 3 and dials oar mechanism 4, and frame 1 has played the effect of whole support, and it is provided with microscope carrier 2 to slide in frame 1, and microscope carrier 2 is used for bearing unmanned aerial vehicle 100. A lifting mechanism 3 is provided on the frame 1, the lifting mechanism 3 being configured to carry the drone 100 and drive it to move up and down in a vertical direction. Dial oar mechanism 4 and set up on elevating system 3, dial oar mechanism 4 and be configured as the screw of stirring unmanned aerial vehicle 100 for unmanned aerial vehicle 100's descending.
The unmanned aerial vehicle outdoor operations equipment that this embodiment provided is provided with microscope carrier 2 through sliding in frame 1 for microscope carrier 2 forms drawer type structure, bears unmanned aerial vehicle 100 on the microscope carrier 2, is used for taking of unmanned aerial vehicle 100, and operating personnel push-and-pull microscope carrier 2, unmanned aerial vehicle 100 of being convenient for take and place, realize the loading function. When unmanned aerial vehicle 100 need fly, operating personnel places unmanned aerial vehicle 100 on microscope carrier 2 on elevating system 3, and elevating system 3 can bear unmanned aerial vehicle 100 and drive it along vertical direction elevating movement to provide the required high altitude environment of flying for unmanned aerial vehicle 100, thereby realize the function of flying. When unmanned aerial vehicle 100 descends, dial oar mechanism 4 and can stir unmanned aerial vehicle 100's screw to draw in the screw in, the descending of unmanned aerial vehicle 100 of being convenient for, the convenience in use is good.
It can be understood that the number of microscope carrier 2 can be provided with a plurality ofly, and every microscope carrier 2 is used for bearing an unmanned aerial vehicle 100, accomodates effectually. The quantity of the preferred microscope carrier 2 of this embodiment is four, and four microscope carriers 2 become the rectangular matrix and distribute, form two rows and two column structures for hold four unmanned aerial vehicle 100, accomodate neatly, pleasing to the eye, conveniently carry. Optionally, be provided with the fixed slot on microscope carrier 2, the fixed slot is used for holding and fixed unmanned aerial vehicle 100's undercarriage, avoids unmanned aerial vehicle 100 to appear the position removal in the transportation, and is fixed effectual, the unmanned aerial vehicle 100's of being convenient for safe transportation.
Further, this unmanned aerial vehicle outdoor operations equipment still includes operating panel 5, safety grating 6 and electric appliance cabinet 7, and electric appliance cabinet 7 sets up in the inside of frame 1, and electric appliance cabinet 7 is used for electronic components's installation, and electric appliance cabinet 7 electricity respectively connects in operating panel 5 and safety grating 6, and electric appliance cabinet 7 has played the effect of intermediate control. An operation panel 5 is arranged on the top surface of the frame 1, and the function of man-machine interaction is realized by arranging the operation panel 5. The safety grating 6 is arranged on one side of the top surface of the frame 1, and the safety grating 6 plays a role of an infrared sensor. When an operator and an object enter the range of the safety grating 6, the safety grating 6 can transmit a position signal to the electric appliance cabinet 7, and the electric appliance cabinet 7 controls the alarm to give an alarm, so that safety accidents are avoided.
Optionally, this unmanned aerial vehicle outdoor operations equipment still includes damper 8, and damper 8 sets up in the outside of frame 1, and damper 8 has played the cushioning effect, avoids appearing the condition of damage because of the collision at on-vehicle removal in-process.
This unmanned aerial vehicle outdoor operations equipment accomodate and fly to two relatively independent processes, in order to guarantee flying of unmanned aerial vehicle 100, as shown in fig. 3-4, elevating system 3 includes elevating platform 31 and lift driving source 32, and elevating platform 31 is similar cuboid structure, and elevating platform 31 is used for bearing unmanned aerial vehicle 100. The lift driving source 32 specifically is the lift electric cylinder, and the output of lift driving source 32 is connected in elevating platform 31, and lift driving source 32 can drive elevating platform 31 and drive unmanned aerial vehicle 100 and carry out the elevating movement, for unmanned aerial vehicle 100 provides the high altitude environment that lets go, is convenient for letting go of unmanned aerial vehicle 100.
Optionally, the lifting mechanism 3 further comprises a guide 33 (shown in fig. 3) and a guide rod 34 (shown in fig. 6), the guide 33 is preferably a linear bearing, the guide 33 is disposed on the frame 1, and the guide rod 34 is disposed at the bottom of the lifting table 31 and slidably engaged with the guide 33. Through the sliding fit of guide bar 34 and guide 33, the guide effect has been played, when guaranteeing elevating platform 31 at lift in-process stability, has guaranteed the smoothness nature of lift process.
After the drone 100 flies, in order to facilitate landing of the drone 100, as shown in fig. 4-5, the paddle poking mechanism 4 includes a first paddle poking component 41 and a second paddle poking component 42, the first paddle poking component 41 is configured to fix an inner wing of the propeller, and the second paddle poking component 42 is configured to poke an outer wing of the propeller, which plays a role in assisting rotation of the propeller. Because the screw can rotate for unmanned aerial vehicle 100 body, when inboard wing is fixed the back, stir the outside wing for the direction of adjustment screw draws in with the screw.
Further, first group's oar subassembly 41 includes the pivot, resets, first driving lever 411 and first driver part 412, is provided with on elevating system 3's elevating platform 31 and holds logical groove 311, is holding logical inslot 311 and is provided with the pivot, and the piece that resets is worn to locate by the pivot, resets specifically for the torsional spring, resets the both ends butt of piece in holding the inner wall that leads to groove 311, resets and has played the effect that the rotation resets. The first driving lever 411 is disposed through the receiving slot 311 and sleeved on the rotating shaft, and the first driving member 412 can abut against the bottom of the first driving lever 411, so that the first driving lever 411 rotates relative to the rotating shaft and is selectively disposed in the receiving slot 311. The first toggle lever 411 is used for fixing the inner wing through stretching and retracting relative to the lifting platform 31.
The first driving part 412 moves towards the direction close to the first driving lever 411, the first driving part 412 abuts against the bottom of the first driving lever 411 and drives the first driving lever 411 to rotate relative to the rotating shaft towards the direction close to the accommodating through groove 311, the reset part is in a compressed state, and the first driving lever 411 can press the inner wing against the lifting platform 31, so that the inner wing is fixed. If the unmanned aerial vehicle 100 is not arranged on the lifting platform 31, the first driving lever 411 can be directly accommodated in the accommodating through groove 311, the first driving lever 411 can be accommodated, the occupied space is small, and the space utilization rate is high. When the first driving element 412 moves away from the first driving lever 411, the first driving element 412 leaves the bottom of the first driving lever 411, and under the self-restoring force of the compressed restoring element, the first driving lever 411 rotates relative to the rotating shaft in the direction away from the accommodating through slot 311 until the first driving lever 411 is in a vertical state.
It can be understood that, because unmanned aerial vehicle 100's screw has four, can both be drawn in order to guarantee every screw, the quantity of first driving lever 411 is four, and four first driving levers 411 encircle and locate the setting of elevating platform 31, form the accommodation space that is used for holding unmanned aerial vehicle 100.
In order to ensure that the four propellers can be accommodated simultaneously by using one first driving part 412, the first driving part 412 comprises a rotary table 4121 and a rotary driving source 4123, the rotary table 4121 is arranged at the bottom of the lifting platform 31 of the lifting mechanism 3, a pressing block 4122 is arranged on the outer side surface of the rotary table 4121, and the pressing block 4122 extends out of the rotary table 4121, so that a cantilever effect is realized. The rotary driving source 4123 is specifically a rotary motor, an output end of the rotary driving source 4123 is connected to the turntable 4121, the rotary driving source 4123 can drive the turntable 4121 to rotate, so that the pressing block 4122 abuts against the bottom of the first shift lever 411, and the pressing block 4122 plays a role in shifting the first shift lever 411. Because each pressing block 4122 can shift one first shifting lever 411 along with the rotation of the rotating disc 4121, the rotation of the first shifting lever 411 can be realized simultaneously by adopting one rotary driving source 4123, the synchronization consistency is good, and the production cost is saved.
Further, as shown in fig. 4-5, the second paddle assembly 42 includes a second paddle 421 and a second driving component 422, the second paddle 421 is disposed outside the lifting platform 31 of the lifting mechanism 3, the second driving component 422 is connected to the second paddle 421, the second driving component 422 can drive the second paddle 421 to move horizontally, and the second paddle 421 completes the process of toggling the outer wing along with the movement of the second paddle 421.
Further, the second driving component 422 includes a driving sprocket 4221, a driven sprocket 4222, a chain 4223 and a rotary driving element 4224, the driving sprocket 4221 is rotatably disposed on the lifting mechanism 3, the driven sprocket 4222 is rotatably disposed on the lifting mechanism 3, the chain 4223 is disposed around the lifting platform 31 of the lifting mechanism 3 and connected to the second shift lever 421, the chain 4223 is respectively engaged with the driving sprocket 4221 and the driven sprocket 4222, an output end of the rotary driving element 4224 is connected to the driving sprocket 4221, and the rotary driving element 4224 can drive the driving sprocket 4221 to rotate and drive the chain 4223 and the second shift lever 421 to move. The rotary driving member 4224 is specifically a motor, the rotary driving member 4224 drives the driving sprocket 4221 to rotate, and the chain 4223 and the driven sprocket 4222 are driven to move along with the rotation of the driving sprocket 4221, so that the second shift lever 421 moves, and an effect of shifting the outer wing is achieved.
Optionally, the number of the driven sprockets 4222 is three, one driving sprocket 4221 and three driven sprockets 4222 are respectively arranged at four corners of the lifting platform 31, and the chain 4223 is of a closed rectangular annular structure, so that the storage of four propellers can be simultaneously realized by one second driving part 422, the synchronization consistency is good, and the production cost is saved.
Owing to be convenient for accomodate unmanned aerial vehicle 100, this unmanned aerial vehicle outdoor operations equipment is still including returning to the middle mechanism 9, and the mechanism 9 sets up on elevating system 3 in returning to the middle, and the mechanism 9 of returning to the middle is configured to the butt in unmanned aerial vehicle 100's the outside for unmanned aerial vehicle 100 is located the central point of elevating system 3's elevating platform 31 and puts together to unmanned aerial vehicle 100 that descends.
Specifically, as shown in fig. 6, the centering mechanism 9 includes two first centering rods 91, two second centering rods 92 and a centering driving source 93, the two first centering rods 91 are respectively disposed on one set of opposite sides of the lifting mechanism 3, the two second centering rods 92 are respectively disposed on the other set of opposite sides of the lifting mechanism 3, the second centering rods 92 are perpendicular to the first centering rods 91, and the two first centering rods 91 and the two second centering rods 92 form a rectangular structure. Pole 91 and the second pole 92 of returning to the center in first returning can the butt in two adjacent side outsides of unmanned aerial vehicle 100, the driving source 93 specifically is driving motor in returning to the center, the driving source 93 is connected in pole 91 and the second pole 92 of returning to the center in first returning to the center in the transmission respectively, the driving source 93 can drive first pole 91 and the second pole 92 of returning to the center in returning to the center and to being close to each other or the direction removal of keeping away from and can the butt in two adjacent side outsides of unmanned aerial vehicle 100, make unmanned aerial vehicle 100 to the central point of elevating platform 31 and put together, accomplish putting together of unmanned aerial vehicle 100.
Preferably, the centering mechanism 9 further includes a transmission rope 94 and a transmission wheel 95, the transmission rope 94 is preferably a steel wire rope, the centering driving source 93 is specifically a driving cylinder, the centering driving source 93 is disposed along one of the side edges of the lifting platform 31, the output end of the centering driving source 93 is connected to the transmission rope 94, and the transmission rope 94 is slidably disposed on the lifting platform 31. The plurality of driving wheels 95 are wound on the lifting table 31, and the driving rope 94 is wound on the plurality of driving wheels 95 in a tensioned manner, so that the driving rope 94 is a closed rectangular ring structure. Four sides of the driving rope 94 are respectively connected to the two first centering rods 91 and the two second centering rods 92, the centering driving source 93 drives one side of the driving rope 94 to move, and due to the fact that the driving rope 94 is of an annular structure, the driving rope 94 rotates relative to the lifting table 31 in the moving process, and therefore each first centering rod 91 and each second centering rod 92 respectively move along the corresponding side face. The rotation direction of the driving rope 94 is fixed to realize the simultaneous concentration and diffusion of the four centering rods, so as to ensure the synchronous gathering effect of the unmanned aerial vehicle 100.
In the description herein, it is to be understood that the terms "upper", "lower", "right", and the like are based on the orientations and positional relationships shown in the drawings and are used for convenience in description and simplicity in operation, but do not indicate or imply that the referenced devices or elements must have a particular orientation, be constructed in a particular orientation, and be constructed in a particular operation, and thus should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used merely for descriptive purposes and are not intended to have any special meaning.
In the description herein, references to the description of "an embodiment," "an example" or the like are intended to mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example.
In addition, the foregoing is only the preferred embodiment of the present invention and the technical principles applied. It will be understood by those skilled in the art that the present invention is not limited to the particular embodiments described herein, but is capable of various obvious changes, rearrangements and substitutions as will now become apparent to those skilled in the art without departing from the scope of the invention. Therefore, although the present invention has been described in greater detail by the above embodiments, the present invention is not limited to the above embodiments, and may include other equivalent embodiments without departing from the spirit of the present invention, and the scope of the present invention is determined by the scope of the appended claims.

Claims (10)

1. An unmanned aerial vehicle outdoor operations equipment which characterized in that includes:
the unmanned aerial vehicle comprises a frame (1) and a carrier (2), wherein the carrier (2) is arranged in the frame (1) in a sliding mode, and the carrier (2) is used for bearing the unmanned aerial vehicle (100);
a lifting mechanism (3) arranged on the frame (1), wherein the lifting mechanism (3) is configured to bear the unmanned aerial vehicle (100) and drive the unmanned aerial vehicle to move up and down along a vertical direction;
dial oar mechanism (4), it set up in on elevating system (3), dial oar mechanism (4) and be configured as and stir the screw of unmanned aerial vehicle (100) for the descending of unmanned aerial vehicle (100).
2. Unmanned aerial vehicle outdoor work apparatus according to claim 1, wherein the lifting mechanism (3) comprises:
a lift table (31) for carrying the drone (100);
and the output end of the lifting driving source (32) is connected to the lifting platform (31), and the lifting driving source (32) can drive the lifting platform (31) to move up and down.
3. Unmanned aerial vehicle outdoor work apparatus according to claim 1, wherein the paddle-poking mechanism (4) comprises:
a first paddle assembly (41), the first paddle assembly (41) configured to secure an inboard wing of the propeller;
a second paddle assembly (42), the second paddle assembly (42) configured to paddle an outboard wing of the propeller.
4. The unmanned aerial vehicle outdoor work apparatus of claim 3, wherein the first paddle assembly (41) comprises:
the lifting mechanism (3) is provided with an accommodating through groove (311), and the rotating shaft is arranged in the accommodating through groove (311);
the reset piece is sleeved on the rotating shaft, and two ends of the reset piece are abutted against the inner wall of the accommodating through groove (311);
the first shifting lever (411) penetrates through the accommodating through groove (311) and is sleeved on the rotating shaft;
the first driving component (412) can abut against the bottom of the first deflector rod (411), so that the first deflector rod (411) rotates relative to the rotating shaft and is selectively arranged in the accommodating through groove (311) and used for fixing the inner wing.
5. The unmanned aerial vehicle outdoor work apparatus of claim 4, wherein the first drive component (412) comprises:
a turntable (4121) provided on the lifting mechanism (3), a pressing block (4122) being provided on an outer side surface of the turntable (4121);
and the output end of the rotary driving source (4123) is connected to the rotating disc (4121), and the rotary driving source (4123) can drive the rotating disc (4121) to rotate so that the pressing block (4122) is abutted against the bottom of the first deflector rod (411).
6. The unmanned aerial vehicle outdoor work apparatus of claim 3, wherein the second paddle assembly (42) comprises:
a second deflector rod (421) which is arranged outside the lifting mechanism (3);
and the second driving component (422) is connected to the second shifting lever (421), and the second driving component (422) can drive the second shifting lever (421) to horizontally move so that the second shifting lever (421) shifts the outer wing.
7. The unmanned aerial vehicle outdoor work apparatus of claim 6, wherein the second drive component (422) comprises:
a drive sprocket (4221) rotatably provided to the lifting mechanism (3);
a driven sprocket (4222) rotatably provided to the lifting mechanism (3);
a chain (4223) disposed around the lifting mechanism (3) and connected to the second shift lever (421), the chain (4223) being engaged with the driving sprocket (4221) and the driven sprocket (4222), respectively;
and the output end of the rotary driving part (4224) is connected to the driving chain wheel (4221), and the rotary driving part (4224) can drive the driving chain wheel (4221) to rotate and drive the chain (4223) and the second shifting lever (421) to move.
8. The unmanned aerial vehicle outdoor work apparatus of claim 1, further comprising a centering mechanism (9), the centering mechanism (9) being disposed on the lifting mechanism (3), the centering mechanism (9) being configured to abut against an outer side of the unmanned aerial vehicle (100) such that the unmanned aerial vehicle (100) is located in a central position of the lifting mechanism (3).
9. Unmanned aerial vehicle outdoor work apparatus according to claim 8, characterized in that the centering mechanism (9) comprises:
two first centering rods (91) respectively arranged on one group of opposite sides of the lifting mechanism (3);
two second centering rods (92) respectively arranged at the other opposite sides of the lifting mechanism (3), wherein the second centering rods (92) are perpendicular to the first centering rods (91);
the centering driving source (93) is in transmission connection with the first centering rod (91) and the second centering rod (92) respectively, and the centering driving source (93) can drive the first centering rod (91) and the second centering rod (92) to move towards the direction close to or away from each other and can abut against the outer sides of two adjacent sides of the unmanned aerial vehicle (100).
10. Unmanned aerial vehicle outdoor work apparatus according to claim 1, further comprising a shock absorber (8), the shock absorber (8) being disposed outside the frame (1).
CN202010758404.2A 2020-07-31 2020-07-31 Unmanned aerial vehicle outdoor operations equipment Pending CN111874250A (en)

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WO2023130313A1 (en) * 2022-01-06 2023-07-13 深圳市大疆创新科技有限公司 Unmanned aerial vehicle circulating storage device and system

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