CN110884661A - Transportation unmanned aerial vehicle convenient to press from both sides express delivery and get - Google Patents
Transportation unmanned aerial vehicle convenient to press from both sides express delivery and get Download PDFInfo
- Publication number
- CN110884661A CN110884661A CN201911254164.6A CN201911254164A CN110884661A CN 110884661 A CN110884661 A CN 110884661A CN 201911254164 A CN201911254164 A CN 201911254164A CN 110884661 A CN110884661 A CN 110884661A
- Authority
- CN
- China
- Prior art keywords
- unmanned aerial
- aerial vehicle
- band
- servo motor
- transportation unmanned
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 230000007246 mechanism Effects 0.000 claims abstract description 24
- 230000005540 biological transmission Effects 0.000 claims description 21
- 230000008878 coupling Effects 0.000 claims description 12
- 238000010168 coupling process Methods 0.000 claims description 12
- 238000005859 coupling reaction Methods 0.000 claims description 12
- 230000000694 effects Effects 0.000 claims description 6
- 238000003466 welding Methods 0.000 claims description 6
- 239000010687 lubricating oil Substances 0.000 claims description 4
- 239000003292 glue Substances 0.000 claims description 3
- 238000004806 packaging method and process Methods 0.000 abstract description 7
- 230000001066 destructive effect Effects 0.000 abstract description 4
- 238000012856 packing Methods 0.000 description 20
- 238000013461 design Methods 0.000 description 3
- 238000009826 distribution Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000007547 defect Effects 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
- B64D9/003—Devices for retaining pallets or freight containers
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Packaging Of Machine Parts And Wound Products (AREA)
Abstract
The invention discloses a transportation unmanned aerial vehicle convenient for clamping express delivery, and relates to the field of transportation unmanned aerial vehicles. According to the invention, through the arranged height position adjusting mechanism, the height position of the packaging box can be adjusted, and the packaging box is prevented from colliding with a landing area when the transportation unmanned aerial vehicle lands, so that destructive influence on objects in the packaging box is prevented.
Description
Technical Field
The invention relates to the field of unmanned transport vehicles, in particular to an unmanned transport vehicle convenient for clamping express.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. 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 in the industry and is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.
In the prior art, a navigation system is extremely developed and has the characteristic of high accuracy, a transportation unmanned aerial vehicle applied to the express delivery industry can realize the distribution of package box goods within a certain weight range, the transportation unmanned aerial vehicle can take off and go to only by inputting a GPS address of a receiver into the system, and the cost of manual distribution is greatly reduced, but the transportation unmanned aerial vehicle in the express delivery industry has not mature technology at present and has certain defects in design, wherein most of the transportation unmanned aerial vehicles adopt a hanging or tying method to fix the package box on the transportation unmanned aerial vehicle, the automation degree is low, the operation is troublesome, in addition, when the transportation unmanned aerial vehicle flies, the package box is easy to loosen to cause the package box to fall off, in addition, the height of the package box is different, when the package box with larger height is transported, the lowest end of the package box is lower than the bottom end of a support frame, and, when transportation unmanned aerial vehicle reachd to the destination, the heelpiece of two sets of support frames can't land, leads to the packing carton to collide with placing the plane, causes the influence to the inside object of packing carton easily, for this reason, we propose one kind be convenient for press from both sides the transportation unmanned aerial vehicle who gets the express delivery.
Disclosure of Invention
The invention aims to overcome the existing defects, provides a transportation unmanned aerial vehicle convenient for clamping express, and can effectively solve the problems in the background technology.
In order to achieve the purpose, the invention provides the following technical scheme: the utility model provides a transportation unmanned aerial vehicle convenient to press from both sides express delivery and get, includes transportation unmanned aerial vehicle main part, the outside fixed mounting of transportation unmanned aerial vehicle main part has four group's mounting brackets, the one end that transportation unmanned aerial vehicle main part was kept away from to the mounting bracket is provided with the rotor assembly, the bottom surface fixed mounting of transportation unmanned aerial vehicle main part has first support frame and second support frame, the below of transportation unmanned aerial vehicle main part is provided with high position control mechanism and presss from both sides with pressing from both sides and get the mechanism.
Preferably, the height position adjusting mechanism is composed of a mounting plate, a first cylinder, a second cylinder, a rotating shaft, a limiting ring, a threaded rod, a flange plate, a sliding chute, a first band-type brake servo motor, a first coupler, a first driving wheel, a second coupler, a second driving wheel, a driving belt and a sliding block.
Preferably, the mounting plate is fixedly mounted at the bottom of the main body of the unmanned aerial vehicle, the first cylinder and the second cylinder are fixedly mounted at the bottom of the mounting plate, the limit ring is fixedly mounted at the bottom of the first cylinder, the first band-type servo motor is fixedly mounted inside the second cylinder, the rotating shaft is movably mounted inside the first cylinder, the bottom end of the first coupler is fixedly connected with an output shaft of the first band-type servo motor, the bottom end of the first driving wheel is fixedly connected with the top end of the first coupler, the bottom end of the second coupler is fixedly connected with the top end of the rotating shaft, the bottom end of the second driving wheel is fixedly connected with the top end of the second coupler, the second driving wheel is connected with the first driving wheel through transmission belt, an internal thread is formed on the inner wall of the rotating shaft, and an external thread is formed on the outer wall of the threaded rod, the threaded rod is connected with the rotating shaft in a threaded mode, a flange plate is fixedly mounted at the bottom end of the threaded rod, the sliding block is arranged in the sliding groove in a sliding mode, and the length of the sliding groove is smaller than that of the threaded rod.
Preferably, the inner diameter of the limiting ring is smaller than the outer diameter of the rotating shaft, and lubricating oil is coated on the outer wall of the rotating shaft.
Preferably, the clamping mechanism is composed of a mounting seat, a first clamping jaw, a second band-type brake servo motor, a third band-type brake servo motor, a rack, a first rotating rod, a second rotating rod, a first shaft sleeve and a second shaft sleeve.
Preferably, bolt and ring flange fixed connection are passed through at the top of mount pad, the equal fixed mounting in the front side of mount pad of second band-type brake servo motor and third band-type brake servo motor, the equal fixed mounting in the rear side inner wall of mount pad of first axle sleeve and second axle sleeve, the one end activity suit of first dwang is to the inside of first axle sleeve, the other end of first dwang runs through the preceding lateral wall of mount pad and second band-type brake servo motor's output shaft fixed connection, the one end activity suit of second dwang is to the inside of second axle sleeve, the other end of second dwang runs through the preceding lateral wall of mount pad and third band-type brake servo motor's output shaft fixed connection, the one end fixed mounting of first clamping jaw is in the middle part of first dwang, the one end fixed mounting of second clamping jaw is in the middle part of second dwang.
Preferably, the number of the racks is two, and the two sets of racks are fixedly installed on the adjacent surfaces of the first clamping jaw and the second clamping jaw respectively through welding.
Preferably, the outer surfaces of the bottoms of the first bottom cushion and the second bottom cushion are fixedly provided with rubber pads through strong glue adhesion, and the outer surface of the bottom of each rubber pad is provided with an anti-skid groove.
Compared with the prior art, the invention has the beneficial effects that:
1. according to the height position adjusting mechanism, when a packing box with a larger height is transported, the first band-type servo motor drives the first coupler to rotate clockwise, the first coupler drives the first transmission wheel, the first transmission wheel drives the second transmission wheel through the transmission belt, the second transmission wheel drives the rotating shaft to rotate, the sliding block in the limiting ring structure is clamped into the sliding groove in the threaded rod, the threaded rod is limited and cannot rotate along with the rotating shaft, and therefore the rotating motion is converted into linear motion, the threaded rod moves downwards and upwards and drives the clamping mechanism and the packing box below, the bottom position of the packing box is higher than the height positions of the bottom ends of the first support frame and the second support frame, the packing box is prevented from colliding with a landing area when the transport unmanned aerial vehicle lands, and destructive influence is caused on objects inside the packing box.
2. According to the clamping mechanism, the second band-type brake servo motor drives the first rotating rod to rotate anticlockwise, the third band-type brake servo motor drives the second rotating rod to rotate clockwise, the first clamping jaw and the second clamping jaw rotate towards the adjacent direction, and therefore a packaging box is clamped.
Drawings
FIG. 1 is a front view of the present invention;
FIG. 2 is an enlarged view of A of FIG. 1 in accordance with the present invention;
FIG. 3 is a schematic structural view of a height position adjusting mechanism according to the present invention;
FIG. 4 is an enlarged view of B of FIG. 3 in accordance with the present invention;
FIG. 5 is a schematic view of the structure of the stop collar and the threaded rod of the present invention;
FIG. 6 is a schematic view of the gripping mechanism of the present invention;
FIG. 7 is an enlarged view of C of FIG. 6 in accordance with the present invention;
FIG. 8 is a bottom view of the mounting base of the present invention;
in the figure: 1. transporting the unmanned aerial vehicle main body; 2. a mounting frame; 3. a rotor assembly; 4. a first support frame; 5. a second support frame; 6. a first base pad; 7. a second base pad; 8. a height position adjusting mechanism; 81. mounting a plate; 82. a first cylinder; 83. a second cylinder; 84. a rotating shaft; 85. a limiting ring; 86. a threaded rod; 87. a flange plate; 88. a chute; 89. a first band-type brake servo motor; 810. a first coupling; 811. a first drive pulley; 812. a second coupling; 813. a second transmission wheel; 814. a transmission belt; 815. a slider; 9. a gripping mechanism; 91. a mounting seat; 92. a first jaw; 93. a second jaw; 94. a second band-type brake servo motor; 95. a third band-type brake servo motor; 96. a rack; 97. a first rotating lever; 98. a second rotating lever; 99. a first bushing; 910. and a second shaft sleeve.
Detailed Description
In order to make the technical means, the creation characteristics, the achievement purposes and the effects of the invention easy to understand, the invention is further described with the specific embodiments.
In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front", "rear", "both ends", "one end", "the other end", and the like indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of description and simplicity of description, but do not indicate or imply that the referred device or element must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "connected," and the like are to be construed broadly, such as "connected," which may be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
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.
Referring to fig. 1-8, the present invention provides a technical solution: the utility model provides a transportation unmanned aerial vehicle convenient to press from both sides express delivery and get, including transportation unmanned aerial vehicle main part 1, the outside fixed mounting of transportation unmanned aerial vehicle main part 1 has four group's mounting bracket 2, the one end that transportation unmanned aerial vehicle main part 1 was kept away from to mounting bracket 2 is provided with rotor assembly 3, the bottom external fixed surface of transportation unmanned aerial vehicle main part 1 installs first support frame 4 and second support frame 5, the below of transportation unmanned aerial vehicle main part 1 is provided with height position adjustment mechanism 8 and presss from both sides and get mechanism 9, press from both sides through height position adjustment mechanism 8 and clamp and get mechanism 9, can realize that the clamp of express delivery.
First band-type brake servo motor 89 starts, first band-type brake servo motor 89 drives first shaft coupling 810 and rotates, first shaft coupling 810 drives first drive wheel 811, first drive wheel 811 drives second drive wheel 813 through drive belt 814, second drive wheel 813 drives pivot 84 and rotates, slider 815 in the spacing ring 85 structure is blocked in the spout 88 on the threaded rod 86, play the restriction effect to threaded rod 86, make threaded rod 86 can not follow pivot 84 and rotate, thereby, convert rotary motion into linear motion, threaded rod 86 can longitudinal reciprocating motion, with this height position of control packing carton, prevent when transporting unmanned aerial vehicle to descend, the packing carton collides with the descending region, cause destructive influence to the inside object of packing carton, in this embodiment, preferably, height position adjustment mechanism 8 is by mounting panel 81, first barrel 82, second barrel 83, The device comprises a rotating shaft 84, a limiting ring 85, a threaded rod 86, a flange 87, a sliding groove 88, a first band-type servo motor 89, a first coupler 810, a first transmission wheel 811, a second coupler 812, a second transmission wheel 813, a transmission belt 814 and a sliding block 815. The mounting plate 81 is fixedly mounted at the bottom of the main body 1 of the unmanned aerial vehicle by welding, the first cylinder 82 and the second cylinder 83 are fixedly mounted at the bottom of the mounting plate 81 by welding, the limit ring 85 is fixedly mounted at the bottom end of the first cylinder 82 by welding, the first band-type servo motor 89 is fixedly mounted inside the second cylinder 83, the rotating shaft 84 is movably mounted inside the first cylinder 82, the bottom end of the first coupling 810 is fixedly connected with an output shaft of the first band-type servo motor 89, the bottom end of the first driving wheel 811 is fixedly connected with the top end of the first coupling 810, the bottom end of the second coupling 812 is fixedly connected with the top end 813 of the rotating shaft 84, the bottom end of the second driving wheel is fixedly connected with the top end of the second coupling 812, the second driving wheel 813 is in transmission connection with the first driving wheel 811 by a driving belt 814, an inner wall of the rotating shaft 84 is provided with an inner thread, an outer wall, the threaded rod 86 is in threaded connection with the rotating shaft 84, a flange plate 87 is fixedly mounted at the bottom end of the threaded rod 86, the sliding block 815 is arranged in the sliding groove 88 in a sliding mode, and the length of the sliding groove 88 is smaller than that of the threaded rod 86.
The limiting ring 85 limits the rotating shaft 84, so that the rotating shaft 84 cannot move down, the design of the lubricating oil can reduce the friction force when the rotating shaft 84 rotates, and reduce the kinetic energy loss, in the embodiment, preferably, the inner diameter of the limiting ring 85 is smaller than the outer diameter of the rotating shaft 84, and the outer wall of the rotating shaft 84 is coated with the lubricating oil.
Second band-type brake servo motor 94 drives first dwang 97 anticlockwise rotation, third band-type brake servo motor 95 drives second dwang 98 clockwise rotation, first dwang 97 drives first clamping jaw 92, second dwang 98 drives second clamping jaw 93, make first clamping jaw 92 and second clamping jaw 93 rotate to adjacent direction, thereby press from both sides tight packing carton, second band-type brake servo motor 94 and third band-type brake servo motor 95 after the shut down, can automatic band-type brake locking, make first clamping jaw 92 and second clamping jaw 93 keep the clamp state, in this embodiment, preferably, press from both sides and get mechanism 9 and comprise mount pad 91, first clamping jaw 92, second clamping jaw 93, second band-type brake servo motor 94, third band-type brake servo motor 95, rack 96, first dwang 97, second 98, first axle sleeve 99 and second axle sleeve 910. The top of the mounting seat 91 is fixedly connected with the flange 87 through a bolt, the second band-type brake servo motor 94 and the third band-type brake servo motor 95 are both fixedly installed on the front side of the mounting seat 91, the first shaft sleeve 99 and the second shaft sleeve 910 are both fixedly installed on the inner wall of the rear side of the mounting seat 91, one end of the first rotating rod 97 is movably sleeved inside the first shaft sleeve 99, the other end of the first rotating rod 97 penetrates through the front side wall of the mounting seat 91 and is fixedly connected with the output shaft of the second band-type brake servo motor 94, one end of the second rotating rod 98 is movably sleeved inside the second shaft sleeve 910, the other end of the second rotating rod 98 penetrates through the front side wall of the mounting seat 91 and is fixedly connected with the output shaft of the third band-type brake servo motor 95, one end of the first clamping jaw 92 is fixedly installed in the middle of the first rotating rod 97, and one end of the second clamping jaw 93 is.
The design of the racks 96 can increase the friction force between the first clamping jaw 92, the second clamping jaw 93 and the packing box, and improve the clamping force, in this embodiment, preferably, the number of the racks 96 is two, and the two sets of racks 96 are respectively fixedly mounted on the adjacent surfaces of the first clamping jaw 92 and the second clamping jaw 93 by welding.
After transportation unmanned aerial vehicle reachd the destination, it is subaerial to descend, first heelpiece 6 and second heelpiece 7 and the ground contact of first support frame 4 and 5 bottoms of second support frame, the rubber pad that first heelpiece 6 and 7 bottoms of second heelpiece set up can provide shock attenuation protection when descending, make overall structure more steady when descending, in this embodiment, it is preferred, first heelpiece 6 all is fixed with the rubber pad through powerful glue with the bottom surface of second heelpiece 7, the non-slip groove has been seted up to the bottom surface of rubber pad.
The working principle and the using process of the invention are as follows: when the clamping device is used, a packaging box is placed between a first clamping jaw 92 and a second clamping jaw 93, a second band-type brake servo motor 94 and a third band-type brake servo motor 95 are synchronously controlled to start, the second band-type brake servo motor 94 drives a first rotating rod 97 to rotate anticlockwise, the third band-type brake servo motor 95 drives a second rotating rod 98 to rotate clockwise, the first rotating rod 97 drives the first clamping jaw 92, the second rotating rod 98 drives the second clamping jaw 93 to rotate the first clamping jaw 92 and the second clamping jaw 93 towards the adjacent direction, so that the packaging box is clamped, after the second band-type brake servo motor 94 and the third band-type brake servo motor 95 stop operating, an automatic band-type brake can be locked, the first clamping jaw 92 and the second clamping jaw 93 are kept in a clamping state, racks 96 are arranged on the adjacent surfaces of the first clamping jaw 92 and the second clamping jaw 93, so that the friction force between the first clamping jaw 92, the second clamping jaw 93 and the packaging box can be increased, the clamping force is improved, after the transport unmanned aerial vehicle arrives at a destination, the transport unmanned aerial vehicle lands on the ground, the first base pad 6 and the second base pad 7 at the bottom ends of the first support frame 4 and the second support frame 5 are in contact with the ground, the rubber pads arranged at the bottom parts of the first base pad 6 and the second base pad 7 can provide shock absorption protection when the transport unmanned aerial vehicle lands, so that the whole structure is more stable when the transport unmanned aerial vehicle lands, the second band-type brake servo motor 94 and the third band-type brake servo motor 95 are controlled to start, the second band-type brake servo motor 94 drives the first rotating rod 97 to rotate clockwise, the third band-type brake servo motor 95 drives the second rotating rod 98 to rotate anticlockwise, the first rotating rod 97 drives the first clamping jaw 92, the second rotating rod 98 drives the second clamping jaw 93 to rotate in opposite directions, so as to loosen the packing box, the packing box can be taken out, the distribution is completed, and when the packing box with larger transport height, after the clamping of the packing box is completed by the method, the first band-type servo motor 89 is controlled to start, the first band-type servo motor 89 drives the first coupler 810 to rotate, the first coupler 810 drives the first transmission wheel 811, the first transmission wheel 811 drives the second transmission wheel 813 through the transmission belt 814, the second transmission wheel 813 drives the rotating shaft 84 to rotate, the slide block 815 in the structure of the limiting ring 85 is clamped in the chute 88 on the threaded rod 86 to limit the threaded rod 86, so that the threaded rod 86 can not rotate along with the rotating shaft 84, the rotating motion is converted into linear motion, the threaded rod 86 can longitudinally reciprocate, when the first band-type servo motor 89 rotates clockwise, the threaded rod 86 moves upwards, when the first band-type servo motor 89 operates anticlockwise, the threaded rod 86 moves downwards, when the threaded rod moves downwards, because the length of the chute 88 is smaller than that of the threaded rod 86, slider 815 slides when the peak of spout 88, plays the limiting displacement to threaded rod 86, makes threaded rod 86 can not continue to move down, prevents that threaded rod 86 from droing, and when threaded rod 86 rebound, the clamp of drive below gets mechanism 9 and packing carton, and at this moment, the bottom position of packing carton is higher than the high position in first support frame 4 and 5 bottoms of second support frame, prevents to transport unmanned aerial vehicle when descending, and the packing carton collides with descending regional emergence, leads to the fact destructive influence to the inside object of packing carton.
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 invention, the scope of which is defined in the appended claims and their equivalents.
Claims (8)
1. The utility model provides a transportation unmanned aerial vehicle convenient to press from both sides express delivery and get, includes transportation unmanned aerial vehicle main part (1), its characterized in that: the utility model discloses a mechanism for unmanned aerial vehicle, including transportation unmanned aerial vehicle main part (1), the outside fixed mounting of transportation unmanned aerial vehicle main part (1) has four groups of mounting bracket (2), the one end that transportation unmanned aerial vehicle main part (1) was kept away from in mounting bracket (2) is provided with rotor assembly (3), the bottom surface fixed mounting of transportation unmanned aerial vehicle main part (1) has first support frame (4) and second support frame (5), the below of transportation unmanned aerial vehicle main part (1) is provided with height position adjustment mechanism (8) and presss from both sides and get mechanism (9.
2. The transportation unmanned aerial vehicle convenient to press from both sides express delivery of claim 1, characterized in that: the height position adjusting mechanism (8) is composed of a mounting plate (81), a first barrel (82), a second barrel (83), a rotating shaft (84), a limiting ring (85), a threaded rod (86), a flange plate (87), a sliding groove (88), a first band-type servo motor (89), a first coupler (810), a first transmission wheel (811), a second coupler (812), a second transmission wheel (813), a transmission belt (814) and a sliding block (815).
3. The transportation unmanned aerial vehicle convenient to press from both sides express delivery of claim 2, characterized in that: the utility model discloses a take unmanned aerial vehicle, including mounting panel (81), first barrel (82) and second barrel (83) all through welded fastening in the bottom of mounting panel (81), spacing ring (85) are through welded fastening in the bottom of first barrel (82), first band-type servo motor (89) fixed mounting is in the inside of second barrel (83), pivot (84) movable mounting is in the inside of first barrel (82), the bottom of first shaft coupling (810) and the output shaft fixed connection of first band-type servo motor (89), the top fixed connection of first drive wheel (811) bottom and first shaft coupling (810), the top fixed connection of the bottom of second shaft coupling (812) and pivot (84), the bottom of second drive wheel (813) and the top fixed connection of second shaft coupling (812), second drive wheel (813) and first drive wheel (811) are connected through drive belt (814) transmission, the inner wall of pivot (84) is seted up there is the internal thread, the external screw thread has been seted up to the outer wall of threaded rod (86), threaded rod (86) and pivot (84) threaded connection, the bottom fixed mounting of threaded rod (86) has ring flange (87), slider (815) slide to set up in spout (88), the length of spout (88) is less than the length of threaded rod (86).
4. The transportation unmanned aerial vehicle convenient to press from both sides express delivery of claim 2, characterized in that: the inner diameter of the limiting ring (85) is smaller than the outer diameter of the rotating shaft (84), and lubricating oil is coated on the outer wall of the rotating shaft (84).
5. The transportation unmanned aerial vehicle convenient to press from both sides express delivery of claim 1, characterized in that: the clamping mechanism (9) is composed of a mounting seat (91), a first clamping jaw (92), a second clamping jaw (93), a second band-type brake servo motor (94), a third band-type brake servo motor (95), a rack (96), a first rotating rod (97), a second rotating rod (98), a first shaft sleeve (99) and a second shaft sleeve (910).
6. The transportation unmanned aerial vehicle convenient to press from both sides express delivery of claim 5, characterized in that: the top of mount pad (91) is passed through bolt and ring flange (87) fixed connection, the equal fixed mounting in the front side of mount pad (91) of second band-type servo motor (94) and third band-type servo motor (95), first axle sleeve (99) and the equal fixed mounting in the rear side inner wall of mount pad (91) of second axle sleeve (910), the inside to first axle sleeve (99) of one end activity suit of first dwang (97), the other end of first dwang (97) runs through the preceding lateral wall of mount pad (91) and the output shaft fixed connection of second band-type servo motor (94), the inside to second axle sleeve (910) of one end activity suit of second dwang (98), the other end of second dwang (98) runs through the preceding lateral wall of mount pad (91) and the output shaft fixed connection of third band-type servo motor (95), one end fixed mounting of first clamping jaw (92) is in the middle part of first dwang (97), the one end fixed mounting of second clamping jaw (93) is in the middle part of second dwang (98).
7. The transportation unmanned aerial vehicle convenient to press from both sides express delivery of claim 5, characterized in that: the number of the racks (96) is two, and the two groups of racks (96) are fixedly installed on the adjacent surfaces of the first clamping jaw (92) and the second clamping jaw (93) through welding.
8. The transportation unmanned aerial vehicle convenient to press from both sides express delivery of claim 1, characterized in that: the outer surfaces of the bottoms of the first bottom cushion (6) and the second bottom cushion (7) are fixedly provided with rubber cushions through strong glue, and the outer surface of the bottom of each rubber cushion is provided with an anti-slip groove.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911254164.6A CN110884661A (en) | 2019-12-06 | 2019-12-06 | Transportation unmanned aerial vehicle convenient to press from both sides express delivery and get |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911254164.6A CN110884661A (en) | 2019-12-06 | 2019-12-06 | Transportation unmanned aerial vehicle convenient to press from both sides express delivery and get |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110884661A true CN110884661A (en) | 2020-03-17 |
Family
ID=69751168
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201911254164.6A Pending CN110884661A (en) | 2019-12-06 | 2019-12-06 | Transportation unmanned aerial vehicle convenient to press from both sides express delivery and get |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110884661A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112158340A (en) * | 2020-10-13 | 2021-01-01 | 西北工业大学 | Scalable anti-drop of unmanned aerial vehicle snatchs structure |
| CN112793792A (en) * | 2021-02-26 | 2021-05-14 | 上海润璋智能科技股份有限公司 | Unmanned aerial vehicle for delivering light and handy goods |
| CN118239253A (en) * | 2024-05-28 | 2024-06-25 | 深圳辉业科技有限公司 | Cargo grabbing system for unmanned aerial vehicle and unmanned aerial vehicle rotating shaft |
Citations (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105014687A (en) * | 2015-08-07 | 2015-11-04 | 东北电力大学 | Mechanical arm with multi-rotor-wing unmanned aerial vehicle |
| CN106184757A (en) * | 2016-07-15 | 2016-12-07 | 杭州迅蚁网络科技有限公司 | A kind of unmanned plane goods loads and jettison system automatically |
| CN106347650A (en) * | 2016-10-09 | 2017-01-25 | 北京理工大学 | Tandem double-duct type flight robot and dynamics cooperative control method thereof |
| CN106828937A (en) * | 2017-03-13 | 2017-06-13 | 广东工业大学 | A kind of hooking type loading unmanned plane |
| CN107230946A (en) * | 2017-07-31 | 2017-10-03 | 国网安徽省电力公司合肥供电公司 | A kind of circuit foreign body eliminating apparatus based on unmanned plane |
| CN107471212A (en) * | 2017-08-24 | 2017-12-15 | 佛山伊贝尔科技有限公司 | A kind of flexible pneumatic manipulator |
| CN107484753A (en) * | 2017-09-30 | 2017-12-19 | 国网河南省电力公司邓州市供电公司 | A kind of intelligent substation scarer |
| CN107697292A (en) * | 2017-09-29 | 2018-02-16 | 河南送变电建设有限公司 | High-voltage transmission line pole tower scarer |
| CN107756427A (en) * | 2017-11-23 | 2018-03-06 | 叶词贵 | A kind of damping and slide-prevention type automatic mechanical hand |
| CN107881980A (en) * | 2017-12-14 | 2018-04-06 | 郑州启硕电子科技有限公司 | A kind of rubbish pickup unmanned plane for integrating dustbin |
| CN107902079A (en) * | 2017-12-14 | 2018-04-13 | 郑州启硕电子科技有限公司 | A kind of unmanned plane that rubbish is picked up on Yushan Hill |
| CN207698006U (en) * | 2017-11-27 | 2018-08-07 | 毛芃吁 | Hawser releasing type express delivery unmanned plane |
| CN108505466A (en) * | 2018-04-24 | 2018-09-07 | 陈磊 | A kind of intelligent transportation equipment and its working method with unmanned plane integration of operation |
| CN109250118A (en) * | 2018-10-18 | 2019-01-22 | 沈阳大学 | A kind of controllable bird claw mechanical gripper device of small drone |
| CN109367778A (en) * | 2018-11-20 | 2019-02-22 | 南京森林警察学院 | A kind of police catching formula rotor wing unmanned aerial vehicle |
| CN109625284A (en) * | 2019-01-22 | 2019-04-16 | 广州市妙伊莲科技有限公司 | A kind of heavy duty detergent unmanned plane having a smooth flight for logistics distribution |
| CN208813511U (en) * | 2018-09-28 | 2019-05-03 | 邹健 | A kind of unmanned plane clamps the device of foreign matter in the air |
| CN109878734A (en) * | 2018-12-29 | 2019-06-14 | 罗海洋 | A kind of Intelligent unattended machine express delivery delivery system |
-
2019
- 2019-12-06 CN CN201911254164.6A patent/CN110884661A/en active Pending
Patent Citations (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105014687A (en) * | 2015-08-07 | 2015-11-04 | 东北电力大学 | Mechanical arm with multi-rotor-wing unmanned aerial vehicle |
| CN106184757A (en) * | 2016-07-15 | 2016-12-07 | 杭州迅蚁网络科技有限公司 | A kind of unmanned plane goods loads and jettison system automatically |
| CN106347650A (en) * | 2016-10-09 | 2017-01-25 | 北京理工大学 | Tandem double-duct type flight robot and dynamics cooperative control method thereof |
| CN106828937A (en) * | 2017-03-13 | 2017-06-13 | 广东工业大学 | A kind of hooking type loading unmanned plane |
| CN107230946A (en) * | 2017-07-31 | 2017-10-03 | 国网安徽省电力公司合肥供电公司 | A kind of circuit foreign body eliminating apparatus based on unmanned plane |
| CN107471212A (en) * | 2017-08-24 | 2017-12-15 | 佛山伊贝尔科技有限公司 | A kind of flexible pneumatic manipulator |
| CN107697292A (en) * | 2017-09-29 | 2018-02-16 | 河南送变电建设有限公司 | High-voltage transmission line pole tower scarer |
| CN107484753A (en) * | 2017-09-30 | 2017-12-19 | 国网河南省电力公司邓州市供电公司 | A kind of intelligent substation scarer |
| CN107756427A (en) * | 2017-11-23 | 2018-03-06 | 叶词贵 | A kind of damping and slide-prevention type automatic mechanical hand |
| CN207698006U (en) * | 2017-11-27 | 2018-08-07 | 毛芃吁 | Hawser releasing type express delivery unmanned plane |
| CN107881980A (en) * | 2017-12-14 | 2018-04-06 | 郑州启硕电子科技有限公司 | A kind of rubbish pickup unmanned plane for integrating dustbin |
| CN107902079A (en) * | 2017-12-14 | 2018-04-13 | 郑州启硕电子科技有限公司 | A kind of unmanned plane that rubbish is picked up on Yushan Hill |
| CN108505466A (en) * | 2018-04-24 | 2018-09-07 | 陈磊 | A kind of intelligent transportation equipment and its working method with unmanned plane integration of operation |
| CN208813511U (en) * | 2018-09-28 | 2019-05-03 | 邹健 | A kind of unmanned plane clamps the device of foreign matter in the air |
| CN109250118A (en) * | 2018-10-18 | 2019-01-22 | 沈阳大学 | A kind of controllable bird claw mechanical gripper device of small drone |
| CN109367778A (en) * | 2018-11-20 | 2019-02-22 | 南京森林警察学院 | A kind of police catching formula rotor wing unmanned aerial vehicle |
| CN109878734A (en) * | 2018-12-29 | 2019-06-14 | 罗海洋 | A kind of Intelligent unattended machine express delivery delivery system |
| CN109625284A (en) * | 2019-01-22 | 2019-04-16 | 广州市妙伊莲科技有限公司 | A kind of heavy duty detergent unmanned plane having a smooth flight for logistics distribution |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112158340A (en) * | 2020-10-13 | 2021-01-01 | 西北工业大学 | Scalable anti-drop of unmanned aerial vehicle snatchs structure |
| CN112793792A (en) * | 2021-02-26 | 2021-05-14 | 上海润璋智能科技股份有限公司 | Unmanned aerial vehicle for delivering light and handy goods |
| CN118239253A (en) * | 2024-05-28 | 2024-06-25 | 深圳辉业科技有限公司 | Cargo grabbing system for unmanned aerial vehicle and unmanned aerial vehicle rotating shaft |
| CN118239253B (en) * | 2024-05-28 | 2024-07-19 | 深圳辉业科技有限公司 | Cargo grabbing system for unmanned aerial vehicle and unmanned aerial vehicle rotating shaft assembly |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN110884661A (en) | Transportation unmanned aerial vehicle convenient to press from both sides express delivery and get | |
| CN101298283B (en) | Airborne tripod head apparatus for collecting aerial information and use thereof | |
| CN201816738U (en) | Small high-speed locating holder for aerial survey of unmanned aerial vehicles | |
| US11643203B2 (en) | Unmanned aerial vehicle with package carrier | |
| CN111891376A (en) | Auxiliary take-off equipment for fixed-wing unmanned aerial vehicle | |
| CN213800204U (en) | Anticollision unmanned aerial vehicle frame | |
| CN107053153A (en) | Intelligent conveying robot | |
| CN209554710U (en) | A kind of lifting device and its automatic guide vehicle | |
| CN107963217B (en) | Carry on small-size unmanned aerial vehicle who puts in device of parcel | |
| CN111038700A (en) | Unmanned aerial vehicle carries automatic throwing device of formula | |
| CN113895627A (en) | Multiple rope descending type throwing mechanism for unmanned helicopter | |
| CN108033014B (en) | Small unmanned aerial vehicle capable of remotely controlling and throwing packages | |
| CN211618110U (en) | Diaxon VTOL unmanned aerial vehicle | |
| CN112793792A (en) | Unmanned aerial vehicle for delivering light and handy goods | |
| CN212980542U (en) | Unmanned aerial vehicle jettison device | |
| CN207809769U (en) | Logistics unmanned plane | |
| CN113716024B (en) | Unmanned aerial vehicle undercarriage convenient to expand and adjust | |
| CN110341954A (en) | A kind of free style multi-angle is used for carry-on mechanical arm | |
| CN214451804U (en) | Supporting leg adjustable unmanned aerial vehicle | |
| CN213414211U (en) | Relief unmanned aerial vehicle convenient to lift | |
| CN215285259U (en) | Unmanned aerial vehicle is used in specialty inspection | |
| CN207466981U (en) | A kind of unmanned plane air-supply device | |
| CN211391691U (en) | Survey and drawing unmanned aerial vehicle shock attenuation anti jamming mechanism | |
| CN111661318A (en) | Unmanned aerial vehicle buffering landing gear | |
| CN210503909U (en) | Convenient portable unmanned aerial vehicle anticollision shock attenuation transport case |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20200317 |