CN109625264B - Adjustable small logistics transportation device and assembling method thereof - Google Patents
Adjustable small logistics transportation device and assembling method thereof Download PDFInfo
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- CN109625264B CN109625264B CN201811481656.4A CN201811481656A CN109625264B CN 109625264 B CN109625264 B CN 109625264B CN 201811481656 A CN201811481656 A CN 201811481656A CN 109625264 B CN109625264 B CN 109625264B
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
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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
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
Abstract
The invention discloses an adjustable small-sized logistics transportation device and an assembling method thereof. In the electric control device, the solar panel can convert solar energy into electric energy and store the electric energy into the storage battery, and the storage battery supplies power to the PLC electrically connected with the storage battery; meanwhile, the temperature and humidity sensor can sense the temperature and humidity in the transportation environment of the transportation device, the gyroscope sensor senses the levelness in the flight process, and the GPS locator is used for locating the flight position of the transportation device; the electric control device has various functions and small occupied area, and is powered by solar energy, so that energy is saved.
Description
Technical Field
The invention relates to the field of unmanned aerial vehicles for transportation, in particular to an adjustable small logistics transportation device and an assembling method thereof.
Background
With the intensification of the competition of the logistics industry, how to efficiently transport small logistics becomes a topic of intensive research of each large express logistics company. Aiming at goods with small volume and short transport distance, at present, the goods still need to be loaded into logistics equipment by workers or carrying devices for transportation, cannot safely reach the hands of customers in a short time, and reduces the transportation efficiency. Along with civilian unmanned aerial vehicle's popularization, use unmanned aerial vehicle to carry out the transportation of small-size commodity circulation and receive more and more favour.
The patent of application number 201610691366.7 discloses a logistics transportation unmanned aerial vehicle, which comprises a vehicle body, 4 flight modules, a delivery module and a carrying module, wherein the 4 flight modules are fixedly arranged on the side surface of the vehicle body; the delivery module is arranged at the bottom of the machine body; the carrying module is arranged at the top end of the machine body; this transport unmanned aerial vehicle can accomplish article fast and deliver, and the transportation volume is big, does not receive the influence that traffic jams, and is efficient, practices thrift the labour resource. However, it has the following problems: 1. the delivery module and the carrying module have complex structures, and need to be controlled by an accurate computer to realize transportation, so that the assembly and use costs are high; 2. the volume of delivering the module is limited, can't adjust, lacks limit structure for small-size commodity circulation drops easily in fixed, transportation, and the potential safety hazard is great.
Disclosure of Invention
In order to solve the technical problems, the invention aims to provide an adjustable small logistics transportation device and an assembly method thereof.
The purpose of the invention can be realized by the following technical scheme:
the invention provides an adjustable small-sized logistics transportation device, which comprises a transmission mechanism, a logistics bearing mechanism, an installation rack and an electric control device, wherein the transmission mechanism is arranged on the installation rack;
wherein, drive mechanism includes: the propeller is fixed above the motor structure and coaxially arranged; the number of the propeller and the motor structures is four and the propellers and the motor structures are distributed around the installation rack in a surrounding manner;
the motor structure includes: the servo motor is arranged in the motor shell, a rotating shaft is arranged at the part of the servo motor extending out of the top end of the motor shell, a motor mounting rod is fixed at the part of the servo motor extending out of the bottom end of the motor shell, and a motor mounting base is arranged at the bottom of the motor mounting rod;
the mounting frame includes: the device comprises a first forked connecting plate, a second forked connecting plate, an upper mounting plate and a lower mounting plate, wherein the upper mounting plate and the lower mounting plate are fixedly connected through a mounting column structure; the mounting column structure comprises a first mounting column, a second mounting column and a third mounting column which are coaxially arranged from top to bottom; the first mounting column and the second mounting column are connected through a screw rod, a mounting gap is formed between the first mounting column and the second mounting column, the third mounting column and the second mounting column are connected through a screw rod, and a mounting gap is formed between the third mounting column and the second mounting column; the motor structure is fixedly connected with the mounting column structure through the first forked connecting plate and the second forked connecting plate;
the commodity circulation bears the weight of the mechanism and includes: the device comprises an upper bearing plate and a lower bearing plate, wherein the upper bearing plate and the lower bearing plate are connected through pneumatic telescopic rods which are distributed annularly; the main bodies of the upper bearing plate and the lower bearing plate are both in a hollow annular shape; first mounting holes are uniformly distributed in the circular ring main body of the upper bearing plate, and the logistics bearing mechanism is fixedly connected with the third mounting column through a screw rod penetrating through the first mounting holes;
the electric control device comprises: the cross section of the electric control mounting platform is in a regular octagon shape, and second mounting holes are uniformly distributed in the electric control mounting platform; a temperature and humidity sensor, a gyroscope sensor, a storage battery and a GPS (global positioning system) positioner are arranged on the electric control mounting platform; the PLC is respectively and electrically connected with the servo motor, the temperature and humidity sensor, the gyroscope sensor, the storage battery and the GPS positioner, and the storage battery is electrically connected with the solar cell panel.
The solar panel can convert solar energy into electric energy and store the electric energy into the storage battery, and the storage battery supplies power to the PLC electrically connected with the storage battery; meanwhile, the temperature and humidity sensor can sense the temperature and humidity in the transportation environment of the transportation device, the gyroscope sensor senses the levelness in the flight process, and the GPS locator is used for locating the flight position of the transportation device; the electric control device has various functions and small occupied area, and is powered by solar energy, so that energy is saved.
As a further aspect of the present invention, the first forked connecting plate includes a first connecting body, a motor housing fixing ring, a first forked mounting plate; one end of the first connecting main body and the motor shell fixing ring are integrally formed, the other end of the first connecting main body and the first forked mounting plate are integrally formed, a first fastening plate is arranged on the motor shell fixing ring towards the inner side of the first connecting main body, and a first fastening hole is formed in the first fastening plate;
the tail end of the first fork-shaped mounting plate is provided with a third mounting hole, and the first fork-shaped mounting plate is sleeved in a mounting gap between the first mounting column and the second mounting column through the third mounting hole and is fixedly connected with the mounting rack.
As a further scheme of the invention, the second forked connecting plate comprises a second connecting main body, a motor base mounting plate and a second forked mounting plate; one end of the second connecting main body is integrally formed with the motor base mounting plate, the other end of the second connecting main body is integrally formed with the second forked mounting plate, a second fastening plate is arranged on the inner side, facing the second connecting main body, of the motor base mounting plate, and a second fastening hole is formed in the second fastening plate;
and the tail end of the second forked mounting plate is provided with a fourth mounting hole, and the second forked mounting plate is fixedly connected with the mounting rack by sleeving the fourth mounting hole in a mounting gap between the second mounting column and the third mounting column.
As a further scheme of the invention, the annular main body of the upper bearing plate is provided with anti-scraping structures which are distributed on the outer edge of the upper bearing plate in an annular array and are in a wave shape, a semi-circle shape or a fillet trapezoid shape; go up the anti-scraping structural shape that sets up on the loading board ring shape main part various, but convex cockscomb structure, semicircle shape or fillet trapezoidal form do not have, can not cause the scratch or pierce through the position of placing outside last loading board at the in-process of small-size commodity circulation installation and transportation, have ensured the integrality of commodity circulation transportation.
The annular main body of the lower bearing plate extends outwards to form an extension plate, and one end, far away from the lower bearing plate, of the extension plate is provided with a limiting hole for inserting a logistics fixing structure.
As a further scheme of the invention, the upper mounting plate comprises an upper mounting main body, reinforcing ribs and a center ring, wherein the center ring is coaxially arranged at the center part of the upper mounting main body, the reinforcing ribs are distributed between the upper mounting main body and the center ring in an annular array manner, and a heat dissipation area is formed between the adjacent reinforcing ribs; the upper mounting main body is provided with an upper mounting hole. In the structure of the upper mounting plate, the central ring is matched with the reinforcing ribs, so that the strength of the mounting rack can be increased, and meanwhile, the heat dissipation area formed between the reinforcing ribs is favorable for heat dissipation of electric elements in the electric control device.
As a further scheme of the invention, the lower mounting plate comprises a lower mounting main body, a fifth mounting hole is arranged on the lower mounting main body, and the lower mounting plate is fixedly connected with the first mounting column through a screw rod penetrating through the fifth mounting hole; and a lower mounting pore plate is arranged on the inner edge of the lower mounting main body.
As a further scheme of the invention, the top of the motor shell is provided with a cylindrical heat dissipation through hole.
The invention also provides an assembly method of the adjustable small logistics transportation device, which comprises the following steps:
s1, enabling the rotating shaft to enter the central mounting part of the propeller to complete connection of the propeller and the motor structure, fixedly connecting the motor base mounting plate and the motor mounting base through bolts and nuts penetrating through mounting holes in the motor base mounting plate, sleeving the motor shell fixing ring on the periphery of the motor shell, and fixedly connecting the first forked connecting plate and the second forked connecting plate through the bolts penetrating through the first fastening holes and the second fastening holes to complete assembly of the first forked connecting plate, the second forked connecting plate and the motor structure;
s2, fixing the first mounting column, the second mounting column and the third mounting column through screws penetrating through the third mounting hole and the fourth mounting hole and leaving mounting gaps, and completing assembly of the first forked connecting plate, the second forked connecting plate and the mounting column structure;
s3, installing the PLC, the solar panel, the temperature and humidity sensor, the gyroscope sensor, the storage battery and the GPS positioner on the electric control installation platform to complete the assembly of the electric control device;
s4, sequentially penetrating a screw through a second mounting hole on the electric control mounting platform, a mounting hole on the lower mounting hole plate and an upper mounting hole, and fastening the screw through the upper end of the first mounting column and the fifth mounting hole through a nut to complete the assembly of the mounting rack and the electric control device;
and S5, the screw penetrates through the lower end of the third mounting column and the first mounting hole and is fastened through a nut, and the transportation device is assembled.
The invention has the beneficial effects that:
1. according to the adjustable small-sized logistics transportation device, the transmission mechanism, the logistics bearing mechanism, the mounting rack and the electric control device are arranged, stable assembly can be achieved only through the screw rods and the nuts among the mechanisms and in the mechanisms, the assembly cost is low, the logistics bearing mechanism can adapt to small-sized logistics in different shapes, the control is simple, the adjustment is convenient, the transportation process is safe, the endurance time is long, and the transportation efficiency of the small-sized logistics is improved.
2. The first forked connecting plate and the second forked connecting plate are connected fixedly by sleeving the fixing ring of the motor shell into the periphery of the motor shell and then penetrating the bolt through the first fastening hole and the second fastening hole so as to complete the assembly of the first forked connecting plate, the second forked connecting plate and the motor structure, and the assembly is simple and convenient; this first fork-shaped connecting plate, second fork-shaped connecting plate have not only realized being connected of drive mechanism and installation frame, include a connection subject and a fork-shaped mounting panel simultaneously, enclose synthetic triangle-shaped regional intensity height after fork-shaped mounting panel and erection column structural erection are fixed for the transportation flight is stable, and is few with the material moreover, has reduced weight and windage in the device flight process.
3. Go up the anti-scraping structural shape that sets up on the loading board ring shape main part various, but convex cockscomb structure, semicircle shape or fillet trapezoidal form do not have, can not cause the scratch or pierce through the position of placing outside last loading board at the in-process of small-size commodity circulation installation and transportation, have ensured the integrality of commodity circulation transportation.
4. The annular main body of the lower bearing plate extends outwards to form an extension plate, so that the area for placing logistics between the lower bearing plate and the upper bearing plate can be increased, and meanwhile, a logistics fixing structure in interference fit with the logistics fixing structure can be inserted into the limiting hole, so that the logistics can be limited and fixed.
5. In the structure of the upper mounting plate, the central ring is matched with the reinforcing ribs, so that the strength of the mounting rack can be increased, and meanwhile, the heat dissipation area formed between the reinforcing ribs is favorable for heat dissipation of electric elements in the electric control device.
6. In the electric control device, the solar panel can convert solar energy into electric energy and store the electric energy into the storage battery, and the storage battery supplies power to the PLC electrically connected with the storage battery; meanwhile, the temperature and humidity sensor can sense the temperature and humidity in the transportation environment of the transportation device, the gyroscope sensor senses the levelness in the flight process, and the GPS locator is used for locating the flight position of the transportation device; the electric control device has various functions and small occupied area, and is powered by solar energy, so that energy is saved.
Drawings
The invention will be further described with reference to the accompanying drawings.
Fig. 1 is a three-dimensional view of the adjustable small-sized logistics transportation device of the invention.
Fig. 2 is an isometric view of the adjustable compact logistics transport apparatus of the present invention.
Fig. 3 is a schematic structural diagram of the logistics carrying mechanism of the invention.
Fig. 4 is a schematic structural diagram of the electric control device of the present invention.
Fig. 5 is a schematic view of the motor structure of the present invention.
FIG. 6 is a schematic view of a first forked web of the invention.
Fig. 7 is a structural schematic diagram of a second forked connecting plate of the invention.
Fig. 8 is a schematic view of the structure of the lower mounting plate of the present invention.
Fig. 9 is a schematic view of the structure of the upper mounting plate of the present invention.
In the figure: 100. a transmission mechanism; 110. a propeller; 120. a motor structure; 121. a rotating shaft; 122. a servo motor; 123. a motor housing; 124. a motor mounting rod; 125. a motor mounting base; 126. a heat dissipating through hole; 200. a logistics carrying mechanism; 210. an upper bearing plate; 2101. a scratch-resistant structure; 211. a first mounting hole; 220. a lower bearing plate; 221. an extension plate; 222. a limiting hole; 230. a pneumatic telescopic rod; 300. installing a frame; 310. a first forked connecting plate; 311. a first connecting body; 312. a motor housing fixing ring; 313. a first fork mounting plate; 314. a first fastening plate; 3131. a third mounting hole; 3141. a first fastening hole; 320. a second forked connecting plate; 321. a second connecting body; 322. a motor base mounting plate; 323. a second forked mounting plate; 3231. a fourth mounting hole; 324. a second fastening plate; 3241. a second fastening hole; 330. an upper mounting plate; 331. an upper mounting body; 3311. an upper mounting hole; 332. reinforcing ribs; 333. a center ring; 334. a heat dissipation area; 340. a lower mounting plate; 341. a lower mounting body; 3411. a fifth mounting hole; 342. a lower mounting orifice plate; 350. a first mounting post; 360. a second mounting post; 370. a third mounting post; 400. an electric control device; 410. an electronic control mounting platform; 420. a PLC controller; 430. a solar panel; 440. a temperature and humidity sensor; 450. a gyroscope sensor; 460. a storage battery; 470. a GPS locator; 480. and a second mounting hole.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1 to 9, an adjustable small-sized logistics transportation device of the present embodiment includes a transmission mechanism 100, a logistics carrying mechanism 200, a mounting frame 300, and an electric control device 400. Wherein, drive mechanism 100 includes: the propeller 110 and the motor structure 120 are arranged in a coaxial mode, and the propeller 110 is fixed above the motor structure 120; the number of the propellers 110 and the motor structures 120 is four and is distributed around the installation frame 300. The motor structure 120 includes: servo motor 122, motor housing 123, servo motor 122 sets up in motor housing 123, and the part that servo motor 122 stretches out the motor housing 123 top is provided with rotation axis 121, and the part that servo motor 122 stretches out the motor housing 123 bottom is fixed with motor installation pole 124, and the bottom of motor installation pole 124 is equipped with motor installation base 125. The top of the motor housing 123 is provided with a cylindrical heat dissipating through-hole 126.
Referring to fig. 1, 2, 6, and 7, the mounting frame 300 includes: the mounting structure comprises a first forked connecting plate 310, a second forked connecting plate 320, an upper mounting plate 330 and a lower mounting plate 340, wherein the upper mounting plate 330 and the lower mounting plate 340 are fixedly connected through a mounting column structure. The mounting column structure comprises a first mounting column 350, a second mounting column 360 and a third mounting column 370 which are coaxially arranged from top to bottom; the first mounting column 350 is connected with the second mounting column 360 through a screw, a mounting gap is formed between the first mounting column and the second mounting column, the third mounting column 370 is connected with the second mounting column 360 through a screw, and a mounting gap is formed between the third mounting column and the second mounting column; the motor structure 120 is fixedly connected to the mounting post structure via the first forked connecting plate 310 and the second forked connecting plate 320. The first forked connecting plate 310 includes a first connecting body 311, a motor housing fixing ring 312, a first forked mounting plate 313; one end of the first connecting body 311 is integrally formed with the motor housing fixing ring 312, the other end is integrally formed with the first fork-shaped mounting plate 313, a first fastening plate 314 is disposed on the motor housing fixing ring 312 toward the inner side of the first connecting body 311, and a first fastening hole 3141 is disposed on the first fastening plate 314. The end of the first forked mounting plate 313 is provided with a third mounting hole 3131, and the first forked mounting plate 313 is tightly connected with the mounting frame 300 by sleeving the third mounting hole 3131 in the mounting gap between the first mounting post 350 and the second mounting post 360. The second forked connecting plate 320 comprises a second connecting body 321, a motor base mounting plate 322 and a second forked mounting plate 323; one end of the second connecting body 321 is integrally formed with the motor base mounting plate 322, the other end of the second connecting body is integrally formed with the second forked mounting plate 323, a second fastening plate 324 is disposed on the inner side of the motor base mounting plate facing the second connecting body 321, and a second fastening hole 3241 is disposed on the second fastening plate 324. The end of the second fork-shaped mounting plate 323 is provided with a fourth mounting hole 3231, and the second fork-shaped mounting plate 323 is fastened to the mounting frame 300 by sleeving the fourth mounting hole 3231 in the mounting gap between the second mounting column 360 and the third mounting column 370.
The first forked connecting plate 310 and the second forked connecting plate 320 are ingenious in structural design, the motor shell fixing ring 312 is sleeved on the periphery of the motor shell 123, and then bolts penetrate through the first fastening holes 3141 and the second fastening holes 3241 to fixedly connect the first forked connecting plate 310 and the second forked connecting plate 320, so that the first forked connecting plate, the second forked connecting plate and the motor structure are assembled, and the assembly is simple and convenient. This first fork-shaped connecting plate, second fork-shaped connecting plate have not only realized being connected of drive mechanism and installation frame, include a connection subject and a fork-shaped mounting panel simultaneously, enclose synthetic triangle-shaped regional intensity height after fork-shaped mounting panel and erection column structural erection are fixed for the transportation flight is stable, and is few with the material moreover, has reduced weight and windage in the device flight process.
Referring to fig. 1 and 3, the logistics carrying mechanism 200 includes: the bearing plate comprises an upper bearing plate 210 and a lower bearing plate 220, wherein the upper bearing plate 210 and the lower bearing plate 220 are connected through pneumatic telescopic rods 230 which are distributed annularly; the main bodies of the upper bearing plate 210 and the lower bearing plate 220 are both in a hollow circular ring shape; first mounting holes 211 are uniformly distributed on the circular ring main body of the upper bearing plate 210, and the logistics bearing mechanism 200 is fixedly connected with the third mounting columns 370 through screws passing through the first mounting holes 211. The annular main body of the upper bearing plate 210 is provided with a scratch-proof structure 2101, and the scratch-proof structure 2101 is distributed on the outer edge of the upper bearing plate 210 in an annular array and is in a wave shape, a semi-circular shape or a rounded trapezoid shape. The annular main body of the lower bearing plate 220 is extended with an extension plate 221, and one end of the extension plate 221 away from the lower bearing plate 220 is provided with a limiting hole 222 for inserting a material flow fixing structure.
Referring to fig. 1 and 4, the electronic control device 400 includes: the solar energy photovoltaic power generation system comprises an electric control mounting platform 410, a PLC (programmable logic controller) 420 and a solar cell panel 430, wherein the cross section of the electric control mounting platform 410 is in a regular octagon shape, and second mounting holes 480 are uniformly distributed on the electric control mounting platform. The electronic control mounting platform 410 is provided with a temperature and humidity sensor 440, a gyroscope sensor 450, a storage battery 460 and a GPS (global positioning system) positioner 470; the PLC controller 420 is electrically connected to the servo motor 122, the temperature and humidity sensor 440, the gyroscope sensor 450, the battery 460, and the GPS locator 470, and the battery 460 is electrically connected to the solar panel 430.
In the electric control device, the solar panel 430 can convert solar energy into electric energy and store the electric energy into the storage battery 460, and the storage battery 460 supplies power to the PLC 420 electrically connected with the storage battery 460; meanwhile, the temperature and humidity sensor 440 can sense the temperature and humidity in the transportation environment of the transportation device, the gyroscope sensor 450 senses the levelness in the flight process, and the GPS positioner 470 positions the flight position of the transportation device; the electric control device has various functions and small occupied area, and is powered by solar energy, so that energy is saved.
Referring to fig. 2, 8 and 9, the upper mounting plate 330 includes an upper mounting body 331, reinforcing ribs 332 and a center ring 333, the center ring 333 is coaxially disposed at a central portion of the upper mounting body 331, the reinforcing ribs 332 are distributed in an annular array between the upper mounting body 331 and the center ring 333, and a heat dissipation area 334 is formed between adjacent reinforcing ribs 332; the upper mounting body 331 is provided with an upper mounting hole 3311. The lower mounting plate 340 comprises a lower mounting body 341, a fifth mounting hole 3411 is formed in the lower mounting body 341, and the lower mounting plate 340 is fixedly connected with the first mounting column 350 through a screw passing through the fifth mounting hole 3411; the lower mounting body 341 has a lower mounting hole plate 342 at an inner edge thereof.
The assembling method of the adjustable small logistics transportation device comprises the following steps:
s1, rotating the rotating shaft 121 into the central mounting portion of the propeller 110 to complete the connection between the propeller 110 and the motor structure 120, fixedly connecting the motor base mounting plate 322 and the motor mounting base 125 by bolts and nuts passing through the mounting holes thereof, sleeving the motor housing fixing ring 312 into the periphery of the motor housing 123, and fixedly connecting the first forked connecting plate 310 and the second forked connecting plate 320 by the bolts passing through the first fastening holes 3141 and the second fastening holes 3241 to complete the assembly of the first forked connecting plate 310, the second forked connecting plate 320 and the motor structure 120;
s2, fixing the first mounting post 350, the second mounting post 360, and the third mounting post 370 with screws passing through the third mounting hole 3131 and the fourth mounting hole 3231 with mounting gaps left, and completing the assembly of the first forked connecting plate 310, the second forked connecting plate 320, and the mounting post structure;
s3, installing the PLC 420, the solar panel 430, the temperature and humidity sensor 440, the gyroscope sensor 450, the storage battery 460 and the GPS locator 470 on the electric control installation platform 410 to complete the assembly of the electric control device 400;
s4, passing the screw through the second mounting hole 480 on the electric control mounting platform 410, the mounting hole on the lower mounting hole plate 342, and the upper mounting hole 3311 in sequence, passing the screw through the upper end of the first mounting post 350 and the fifth mounting hole 3411, and fastening them by nuts, thereby completing the assembly of the mounting frame 300 and the electric control device 400;
and S5, penetrating the screw through the lower end of the third mounting column 370 and the first mounting hole 211 and fastening the screw through a nut to complete the assembly of the transportation device.
This adjustable small-size commodity circulation conveyer bears mechanism, installation frame, electrically controlled device through setting up drive mechanism, commodity circulation, only need can realize firm equipment through screw rod, nut between each mechanism and within each mechanism, and the equipment cost is low, and the commodity circulation bears the mechanism and can adapt to the small-size commodity circulation of different shapes, and control is simple, convenient regulation, and transportation safety and duration are long, have improved the conveying efficiency of small-size commodity circulation.
In the description herein, references to the description of "one embodiment," "an example," "a specific 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. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
The foregoing is illustrative and explanatory only and is not intended to be exhaustive or to limit the invention to the precise embodiments described, and various modifications, additions, and substitutions may be made by those skilled in the art without departing from the scope of the invention or exceeding the scope of the claims.
Claims (1)
1. An adjustable small-sized logistics transportation device is characterized by comprising a transmission mechanism (100), a logistics carrying mechanism (200), a mounting rack (300) and an electric control device (400);
wherein the transmission mechanism (100) comprises: the propeller (110) is fixed above the motor structure (120) and is coaxially arranged; the number of the propellers (110) and the number of the motor structures (120) are four and are distributed around the installation rack (300);
the motor structure (120) comprises: the servo motor (122) is arranged in the motor shell (123), a rotating shaft (121) is arranged on the part, extending out of the top end of the motor shell (123), of the servo motor (122), a motor mounting rod (124) is fixed on the part, extending out of the bottom end of the motor shell (123), of the servo motor (122), and a motor mounting base (125) is arranged at the bottom of the motor mounting rod (124);
the mounting frame (300) comprises: the mounting structure comprises a first forked connecting plate (310), a second forked connecting plate (320), an upper mounting plate (330) and a lower mounting plate (340), wherein the upper mounting plate (330) is fixedly connected with the lower mounting plate (340) through a mounting column structure; the mounting column structure comprises a first mounting column (350), a second mounting column (360) and a third mounting column (370) which are coaxially arranged from top to bottom; the first mounting column (350) is connected with the second mounting column (360) through a screw, a mounting gap is formed between the first mounting column and the second mounting column, and the third mounting column (370) is connected with the second mounting column (360) through a screw, and a mounting gap is formed between the third mounting column and the second mounting column; the motor structure (120) is fixedly connected with the mounting column structure through a first forked connecting plate (310) and a second forked connecting plate (320);
the logistics carrying mechanism (200) comprises: the bearing plate comprises an upper bearing plate (210) and a lower bearing plate (220), wherein the upper bearing plate (210) is connected with the lower bearing plate (220) through pneumatic telescopic rods (230) which are distributed annularly; the main bodies of the upper bearing plate (210) and the lower bearing plate (220) are both in a hollow circular ring shape; first mounting holes (211) are uniformly distributed in the circular main body of the upper bearing plate (210), and the logistics bearing mechanism (200) is fixedly connected with the third mounting column (370) through a screw rod penetrating through the first mounting holes (211);
the electric control device (400) comprises: the solar energy power supply comprises an electric control mounting platform (410), a PLC (programmable logic controller) (420) and a solar panel (430), wherein the cross section of the electric control mounting platform (410) is in a regular octagon shape, and second mounting holes (480) are uniformly distributed on the electric control mounting platform; a temperature and humidity sensor (440), a gyroscope sensor (450), a storage battery (460) and a GPS (470) are arranged on the electric control mounting platform (410); the PLC (420) is respectively electrically connected with the servo motor (122), the temperature and humidity sensor (440), the gyroscope sensor (450), the storage battery (460) and the GPS positioner (470), and the storage battery (460) is electrically connected with the solar panel (430);
the first forked connecting plate (310) comprises a first connecting body (311), a motor shell fixing ring (312) and a first forked mounting plate (313); one end of the first connecting main body (311) is integrally formed with the motor shell fixing ring (312), the other end of the first connecting main body is integrally formed with the first fork-shaped mounting plate (313), a first fastening plate (314) is arranged on the motor shell fixing ring (312) towards the inner side of the first connecting main body (311), and a first fastening hole (3141) is formed in the first fastening plate (314);
the tail end of the first fork-shaped mounting plate (313) is provided with a third mounting hole (3131), and the first fork-shaped mounting plate (313) is fixedly connected with the mounting rack (300) by sleeving the third mounting hole (3131) in a mounting gap between the first mounting column (350) and the second mounting column (360);
the second forked connecting plate (320) comprises a second connecting main body (321), a motor base mounting plate (322) and a second forked mounting plate (323); one end of the second connecting main body (321) is integrally formed with the motor base mounting plate (322), the other end of the second connecting main body is integrally formed with the second forked mounting plate (323), a second fastening plate (324) is arranged on the inner side, facing the second connecting main body (321), of the motor base mounting plate, and a second fastening hole (3241) is formed in the second fastening plate (324);
a fourth mounting hole (3231) is formed in the tail end of the second forked mounting plate (323), and the second forked mounting plate (323) is fixedly connected with the mounting rack (300) by sleeving the fourth mounting hole (3231) in a mounting gap between the second mounting column (360) and the third mounting column (370);
the scraping-resistant structure (2101) is arranged on the circular main body of the upper bearing plate (210), and the scraping-resistant structure (2101) is distributed on the outer edge of the upper bearing plate (210) in an annular array and is in a wave shape, a semi-circle shape or a fillet ladder shape;
an extension plate (221) extends outwards from the circular main body of the lower bearing plate (220), and a limiting hole (222) for inserting a logistics fixing structure is formed in one end, far away from the lower bearing plate (220), of the extension plate (221);
the upper mounting plate (330) comprises an upper mounting main body (331), reinforcing ribs (332) and a central ring (333), wherein the central ring (333) is coaxially arranged at the central part of the upper mounting main body (331), the reinforcing ribs (332) are distributed between the upper mounting main body (331) and the central ring (333) in an annular array, and a heat dissipation area (334) is formed between the adjacent reinforcing ribs (332); the upper mounting main body (331) is provided with an upper mounting hole (3311);
the lower mounting plate (340) comprises a lower mounting main body (341), a fifth mounting hole (3411) is formed in the lower mounting main body (341), and the lower mounting plate (340) is fixedly connected with the first mounting column (350) through a screw rod penetrating through the fifth mounting hole (3411); a lower mounting pore plate (342) is arranged on the inner edge of the lower mounting main body (341);
the top of the motor shell (123) is provided with a cylindrical heat dissipation through hole (126);
the method comprises the following steps:
s1, enabling the rotating shaft (121) to rotate into the central mounting position of the propeller (110) to complete connection of the propeller (110) and the motor structure (120), enabling the motor base mounting plate (322) and the motor mounting base (125) to be fixedly connected through bolts and nuts penetrating through mounting holes in the motor base mounting plate, enabling the motor shell fixing ring (312) to be sleeved on the periphery of the motor shell (123), enabling the bolts to penetrate through the first fastening holes (3141) and the second fastening holes (3241) to fixedly connect the first fork-shaped connecting plate (310) and the second fork-shaped connecting plate (320), and completing assembly of the first fork-shaped connecting plate (310), the second fork-shaped connecting plate (320) and the motor structure (120);
s2, fixing the first mounting column (350), the second mounting column (360) and the third mounting column (370) through screws penetrating through the third mounting hole (3131) and the fourth mounting hole (3231) and leaving mounting gaps to complete the assembly of the first forked connecting plate (310), the second forked connecting plate (320) and the mounting column structure;
s3, installing the PLC (420), the solar panel (430), the temperature and humidity sensor (440), the gyroscope sensor (450), the storage battery (460) and the GPS (470) on the electric control installation platform (410) to complete the assembly of the electric control device (400);
s4, sequentially penetrating a screw through a second mounting hole (480) in the electric control mounting platform (410), a mounting hole in the lower mounting hole plate (342) and an upper mounting hole (3311), and fastening the screw through the upper end of the first mounting column (350) and the fifth mounting hole (3411) through nuts to complete the assembly of the mounting rack (300) and the electric control device (400);
and S5, the screw rod penetrates through the lower end of the third mounting column (370) and the first mounting hole (211) and is fastened through the nut, and the transportation device is assembled.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811481656.4A CN109625264B (en) | 2018-12-05 | 2018-12-05 | Adjustable small logistics transportation device and assembling method thereof |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811481656.4A CN109625264B (en) | 2018-12-05 | 2018-12-05 | Adjustable small logistics transportation device and assembling method thereof |
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| CN109625264A CN109625264A (en) | 2019-04-16 |
| CN109625264B true CN109625264B (en) | 2021-08-27 |
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| CN112874798B (en) * | 2021-02-18 | 2022-11-18 | 江西洪都航空工业集团有限责任公司 | Gyro sensor assembly mounting bracket capable of adjusting course |
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|---|---|---|---|---|
| KR200474119Y1 (en) * | 2014-05-02 | 2014-09-19 | 안정철 | Unmanned plane for rescuing drowning victim |
| CN105857606A (en) * | 2016-04-11 | 2016-08-17 | 周良勇 | Multi-rotor unmanned aerial vehicle |
| CN107416176A (en) * | 2017-04-18 | 2017-12-01 | 深圳市易飞行科技有限公司 | Support arm turns down folding and unfolding unmanned plane |
| CN107495812A (en) * | 2017-10-09 | 2017-12-22 | 黄文佳 | A kind of express delivery box structure |
| CN108528693A (en) * | 2018-05-25 | 2018-09-14 | 张博 | Manned equipment |
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2018
- 2018-12-05 CN CN201811481656.4A patent/CN109625264B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR200474119Y1 (en) * | 2014-05-02 | 2014-09-19 | 안정철 | Unmanned plane for rescuing drowning victim |
| CN105857606A (en) * | 2016-04-11 | 2016-08-17 | 周良勇 | Multi-rotor unmanned aerial vehicle |
| CN107416176A (en) * | 2017-04-18 | 2017-12-01 | 深圳市易飞行科技有限公司 | Support arm turns down folding and unfolding unmanned plane |
| CN107495812A (en) * | 2017-10-09 | 2017-12-22 | 黄文佳 | A kind of express delivery box structure |
| CN108528693A (en) * | 2018-05-25 | 2018-09-14 | 张博 | Manned equipment |
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| CN109625264A (en) | 2019-04-16 |
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Effective date of registration: 20210811 Address after: 201700 room 91, Zone E, floor 2, building 1, No. 1588, FengXing Road, Huaxin Town, Qingpu District, Shanghai Applicant after: Shanghai Shike storage equipment Engineering Co.,Ltd. Address before: 239001 4th floor, international business center, Suchu modern industrial park, Chuzhou City, Anhui Province Applicant before: CHUZHOU YUNMI INDUSTRIAL DESIGN Co.,Ltd. |
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