CN113245925A - Remote sensing unmanned aerial vehicle mounting system of processing - Google Patents
Remote sensing unmanned aerial vehicle mounting system of processing Download PDFInfo
- Publication number
- CN113245925A CN113245925A CN202110519711.XA CN202110519711A CN113245925A CN 113245925 A CN113245925 A CN 113245925A CN 202110519711 A CN202110519711 A CN 202110519711A CN 113245925 A CN113245925 A CN 113245925A
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- Prior art keywords
- fixedly connected
- aerial vehicle
- unmanned aerial
- remote sensing
- processing
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B24—GRINDING; POLISHING
- B24B—MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
- B24B5/00—Machines or devices designed for grinding surfaces of revolution on work, including those which also grind adjacent plane surfaces; Accessories therefor
- B24B5/36—Single-purpose machines or devices
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B24—GRINDING; POLISHING
- B24B—MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
- B24B41/00—Component parts such as frames, beds, carriages, headstocks
- B24B41/005—Feeding or manipulating devices specially adapted to grinding machines
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B24—GRINDING; POLISHING
- B24B—MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
- B24B41/00—Component parts such as frames, beds, carriages, headstocks
- B24B41/04—Headstocks; Working-spindles; Features relating thereto
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B24—GRINDING; POLISHING
- B24B—MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
- B24B41/00—Component parts such as frames, beds, carriages, headstocks
- B24B41/06—Work supports, e.g. adjustable steadies
- B24B41/067—Work supports, e.g. adjustable steadies radially supporting workpieces
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B24—GRINDING; POLISHING
- B24B—MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
- B24B47/00—Drives or gearings; Equipment therefor
- B24B47/10—Drives or gearings; Equipment therefor for rotating or reciprocating working-spindles carrying grinding wheels or workpieces
- B24B47/12—Drives or gearings; Equipment therefor for rotating or reciprocating working-spindles carrying grinding wheels or workpieces by mechanical gearing or electric power
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B24—GRINDING; POLISHING
- B24B—MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
- B24B5/00—Machines or devices designed for grinding surfaces of revolution on work, including those which also grind adjacent plane surfaces; Accessories therefor
- B24B5/35—Accessories
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B24—GRINDING; POLISHING
- B24B—MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
- B24B55/00—Safety devices for grinding or polishing machines; Accessories fitted to grinding or polishing machines for keeping tools or parts of the machine in good working condition
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention relates to the technical field of unmanned aerial vehicle fixing pieces, in particular to a remote sensing unmanned aerial vehicle fixing piece processing system which comprises a fixing seat plate, a casting cavity, a feeding pipe and an extension component, wherein the fixing seat plate is fixedly connected with the casting cavity, the fixing seat plate is fixedly connected with the feeding pipe and communicated with the feeding pipe, the fixing seat plate is connected with the extension component capable of sliding, the extension component is connected with the casting cavity in a sliding manner, the extension component comprises a limit slide rod, a bidirectional screw rod, a vertical fixing plate, an extension block and a hollow groove opening, the casting cavity is provided with a through hollow groove opening, the fixing seat plate is fixedly connected with two limit slide rods, the fixing seat plate is rotatably connected with the bidirectional screw rod, and the two vertical fixing plates are connected with the two limit slide rods in a sliding manner. The secondary processing in the later period is not needed, the time is saved, and the working efficiency is increased.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle fixing parts, in particular to a remote sensing unmanned aerial vehicle fixing part processing system.
Background
The remote sensing unmanned aerial vehicle, utilize advanced unmanned vehicles technique, remote sensing sensor technique, telemetering remote control technique, communication technology, GPS difference positioning technology and remote sensing application technology promptly, can realize that automatic, intellectuality, specialization obtain space remote sensing information such as land resource, natural environment, earthquake disaster area fast, and accomplish remote sensing data processing, the application technique of modelling and application analysis. The unmanned aerial vehicle remote sensing system has the advantages of mobility, rapidness, economy and the like, has become a hotspot subject of dispute research of all countries in the world, and has gradually developed from the research and development to the actual application stage to become one of the main aviation remote sensing technologies in the future, and the remote sensing unmanned aerial vehicle needs a supporting leg fixing piece to support when parked, so that the remote sensing unmanned aerial vehicle is parked on the ground.
And prior art can't process out the cylinder that has the slot, needs the later stage to process the landing leg cylinder, processes out the slot, serious waste time.
Disclosure of Invention
The invention aims to provide a remote sensing unmanned aerial vehicle fixing piece processing system which has the advantages that a cylinder with a groove can be directly processed, the cylinder with the groove is used as a fixing piece of a remote sensing unmanned aerial vehicle, secondary processing in the later period is not needed, time is saved, and working efficiency is improved.
The purpose of the invention is realized by the following technical scheme:
further, a remote sensing unmanned aerial vehicle mounting system of processing, including fixed bedplate, casting chamber, filling tube and the component of stretching out, fixedly connected with casting chamber on the fixed bedplate, fixedly connected with filling tube and intercommunication on the fixed bedplate are connected with the component of stretching out that can slide on the fixed bedplate, stretch out component and casting chamber sliding connection.
Further, it includes spacing slide bar, two-way lead screw, erects solid board, extends piece and dead slot mouth to stretch out the component, is provided with the through dead slot mouth on the casting chamber, two spacing slide bars of fixedly connected with on the fixed bedplate, it is connected with two-way lead screw to rotate on the fixed base plate, sliding connection has two to erect solid boards on two spacing slide bars, two are erect solid boards and pass through threaded connection respectively at the both ends of two-way lead screw, two are erect equal fixedly connected with on the solid board and extend the piece, two are extended the equal sliding connection of piece and are in the dead slot mouth.
Further, a plurality of conical bosses are arranged inside the two extending blocks.
Further, a remote sensing unmanned aerial vehicle mounting system of processing still includes side seal board, external traveller and extrudes the sliding plug, fixedly connected with side seal board on the casting chamber, and sliding connection has external traveller on the side seal board, and fixedly connected with extrudes the sliding plug on the external traveller, extrudes sliding plug sliding connection and in the casting intracavity.
Furthermore, a rubber sleeve is fixedly connected to the outer curved surface of the extrusion sliding plug.
Further, a remote sensing unmanned aerial vehicle mounting system of processing is still including extending chamber, lift stopper, carriage, square traveller and spring, and fixedly connected with extends chamber and carriage on the casting chamber, and sliding connection has the square traveller on the carriage, and the below fixedly connected with lift stopper of square traveller, lift stopper sliding connection are in extending the intracavity, and the cover is equipped with the spring on the square traveller, and the spring is located between lift stopper and the carriage.
Further, remote sensing unmanned aerial vehicle mounting system of processing still leans on the top bolt including the top, has the top through threaded connection on the splice frame and leans on the top bolt.
Further, remote sensing unmanned aerial vehicle mounting system of processing still includes slide switch, and slide switch fixed connection is on fixed bedplate, and casting chamber and slide switch contact and sliding connection.
Further, remote sensing unmanned aerial vehicle mounting system of processing still includes the component of polishing, and the component fixed connection of polishing is on fixed bedplate.
Further, remote sensing unmanned aerial vehicle mounting system of processing is still including paining the component, paints component fixed connection on fixed bedplate.
Further, slide switch includes bearing seat, spacing square, telescopic link and contact slide, and bearing seat fixed connection is on fixed bedplate, and spacing square of fixedly connected with and telescopic link on the bearing seat, fixedly connected with contact slide on the telescopic link, contact slide and spacing square sliding connection, contact slide and casting chamber in close contact with and sliding connection.
Further, the polishing component comprises a switching seat, a polishing cavity, a linkage gear and a transmission belt, the switching seat is fixedly connected to the fixed seat plate, the switching seat is rotatably connected with the polishing cavity, the fixed seat plate is fixedly connected with a speed reduction motor, the output shaft of the speed reduction motor is fixedly connected with the linkage gear, and the linkage gear is in transmission connection with the polishing cavity through the transmission belt.
Further, scribble the component including the supporting seat, scribble the cotton and communicate the awl mouth, supporting seat fixed connection is on fixed bedplate, and the cotton is scribbled to fixedly connected with on the supporting seat, fixedly connected with on the supporting seat communicates the awl mouth, communicates the awl mouth and scribbles cotton intercommunication.
The remote sensing unmanned aerial vehicle fixing piece processing system has the beneficial effects that:
can install not only can directly process out the support cylinder that has the slot, but also can ensure to be processed the support cylindrical quality that has the slot, its inside bubble that does not have guarantees the support cylindrical quality that has the slot, but also can polish the processing to the support cylinder that has the slot, on polishing the completion back again paint the anticorrosive coating to the support cylinder that has the slot, increase the support cylindrical life that has the slot.
Drawings
The invention is described in further detail below with reference to the accompanying drawings and specific embodiments.
FIG. 1 is a schematic structural view of a casting embodiment of a support cylinder with a groove;
FIG. 2 is a schematic structural diagram of an embodiment of molten metal storage;
FIG. 3 is a schematic cross-sectional structural view of an embodiment of a molten metal reservoir;
FIG. 4 is a schematic structural view of an embodiment of a support cylinder vent for metal hydraulics and with slots;
FIG. 5 is a schematic structural view of an embodiment of a groove machining for a casting cylinder;
FIG. 6 is a schematic view of the vertical mounting plate and extension block configuration of the present invention;
FIG. 7 is a schematic structural diagram of an embodiment for sensing whether molten metal is completely compressed;
FIG. 8 is a schematic view of the slide switch of the present invention;
FIG. 9 is a schematic illustration of a grinding member construction according to the present invention;
FIG. 10 is a cross-sectional structural schematic view of a grinding member of the present invention;
fig. 11 is a schematic view of the construction of the application member of the present invention.
In the figure:
a fixed seat plate 101;
a casting cavity 102;
a feed tube 103;
an external strut 105;
an extrusion spool 106;
a limiting slide rod 201;
a bidirectional lead screw 202;
a vertical fixing plate 203;
an extension block 204;
a hollow notch 205;
an extension cavity 301;
a lift plug 302;
a connection frame 303;
a square strut 304;
a spring 305;
against the top bolt 306;
a bearing holder 401;
a limiting square bar 402;
a telescopic rod 403;
a contact sled 404;
an adapter 501;
a grinding chamber 502;
a linkage gear 503;
a belt 504;
a support base 601;
smearing cotton 602;
communicating with the cone 603.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings.
The following description that combines figures 1, 2, 3, 5 and 6 in detail, a remote sensing unmanned aerial vehicle mounting system of processing, including fixed bedplate 101, casting chamber 102, filling tube 103 and the component of stretching out, be connected with casting chamber 102 through welded fastening on the fixed bedplate 101, be connected with filling tube 103 and intercommunication through welded fastening on the fixed bedplate 101, be connected with the component of stretching out that can slide on the fixed bedplate 101, stretch out component and casting chamber 102 sliding connection.
The following detailed description is provided with reference to fig. 1, 2, 3, 5 and 6, the extending member includes a limiting slide bar 201, a bidirectional screw 202, a vertical fixing plate 203, an extending block 204 and a hollow notch 205, a through hollow notch 205 is provided on the casting cavity 102, two limiting slide bars 201 are fixedly connected to the fixed seat plate 101 by welding, the two bidirectional screw 202 is rotatably connected to the fixed seat plate 101 by a bearing, two vertical fixing plates 203 are slidably connected to the two limiting slide bars 201, the two vertical fixing plates 203 are respectively connected to two ends of the bidirectional screw 202 by threads, the extending block 204 is fixedly connected to the two vertical fixing plates 203 by welding, and the two extending blocks 204 are respectively slidably connected to the hollow notch 205.
The two limiting slide bars 201 can provide sliding space for the two vertical fixing plates 203 and limit the two vertical fixing plates, so that the two vertical fixing plates 203 can only slide back and forth, the dereference directions of the two ends of the bidirectional screw 202 are opposite, the two vertical fixing plates 203 can provide connecting space for the two extending blocks 204, the hollow groove port 205 can provide sliding space for the two extending blocks 204, the internal structure of the casting cavity 102 is changed by utilizing the contact of the two extending blocks 204, the bidirectional screw 202 is rotated and the two vertical fixing plates 203 are driven to move inwards before metal liquid is added into the casting cavity 102, the two vertical fixing plates 203 can drive the two extending blocks 204 to move inwards, after the two extending blocks 204 are contacted, the two extending blocks 204 form a hollow circle, which is equivalent to the formation of a circular boss in the casting cavity 102, the hollow groove is machined on the casting cylinder, and can be convenient for the connection of the heightening inclined bars of the remote sensing unmanned aerial vehicle fixing bracket in the later period, when the molten metal in the casting cavity 102 is solidified, the solidified molten metal needs to be discharged, at this time, the bidirectional screw 202 needs to be rotated reversely, the two vertical fixing plates 203 drive the two extending blocks 204 to move towards the outer ends, so that the two extending blocks 204 are separated from the casting cavity 102, and at this time, the cylindrical row with the empty slot cast in the casting cavity 102 can be extruded.
As will be described in detail below with reference to fig. 6, a plurality of conical bosses are provided on the inside of each of the two extension blocks 204.
After being provided with a plurality of circular cone bosss, can process out a plurality of circular cone recesses in casting cylindrical dead slot, at this moment increase the down tube and connect and can produce bigger frictional force behind the cylindrical dead slot of casting, increase the down tube and can not rotate with the emergence of casting cylinder easily, realize the firm support to remote sensing unmanned aerial vehicle.
With reference to fig. 1, 2, 3 and 4, the remote sensing unmanned aerial vehicle fixing piece processing system further includes a side sealing plate 104, an external sliding column 105 and an extrusion sliding plug 106, the casting cavity 102 is connected with the side sealing plate 104 through welding, the side sealing plate 104 is connected with the external sliding column 105 in a sliding manner, the external sliding column 105 is connected with the extrusion sliding plug 106 through welding, and the extrusion sliding plug 106 is connected in the casting cavity 102 in a sliding manner.
The side sealing plate 104 can seal the right end of the casting cavity 102 to prevent the molten metal from flowing out from the opening at the right end of the casting cavity 102, the side sealing plate 104 can also provide a connecting space for the external sliding column 105, the outer end of the external sliding column 105 is fixedly connected with the hydraulic rod, the hydraulic rod can be fixedly connected with the fixed seat plate 101, at this time, the hydraulic rod connected with the externally-connected sliding column 105 is started to drive the extrusion sliding plug 106 to slide in the casting cavity 102, so as to discharge the column cast in the casting cavity 102, and it is desirable to have the squeeze plugs 106 at the right end of the casting cavity 102 prior to adding molten metal to the casting cavity 102, after sufficient molten metal is in the casting cavity 102, the external sliding column 105 can be started to drive the extrusion sliding plug 106 to move to the left in the casting cavity 102, so that the metal liquid in the casting cavity 102 is compressed, no gap is formed between the metal liquid, and a cylinder with higher toughness can be formed.
As will be described in detail below with reference to fig. 3 and 4, a rubber sleeve is fixedly connected to the outer curved surface of the extruded sliding plug 106 through a plurality of screws.
After the rubber sleeve is arranged, the extrusion sliding plug 106 and the casting cavity 102 are in a sealed state, molten metal cannot be extruded from the joint of the extrusion sliding plug 106 and the casting cavity 102, if the molten metal is extruded from the joint of the extrusion sliding plug 106 and the casting cavity 102, the quality of a cylinder cast in the casting cavity 102 cannot be guaranteed, and because the molten metal in the casting cavity 102 cannot be compressed, gaps may exist between the molten metal, so that the quality of the cast cylinder is reduced.
The following detailed description that combines figures 1, 2, 3 and 7, a remote sensing unmanned aerial vehicle mounting system of processing still includes and extends chamber 301, lift stopper 302, linking frame 303, square sliding column 304 and spring 305, it extends chamber 301 and linking frame 303 to cast to be connected with through welding fixed on the chamber 102, sliding connection has square sliding column 304 on the linking frame 303, welding fixed connection has lift stopper 302 below square sliding column 304, lift stopper 302 sliding connection is in extending chamber 301, the cover is equipped with spring 305 on the square sliding column 304, spring 305 is located between lift stopper 302 and the linking frame 303.
The extension cavity 301 can provide a connecting space for the lifting plug 302, the lifting plug 302 can seal the extension cavity 301, the lower part of the lifting plug 302 is positioned on the same plane with the inner curved surface of the casting cavity 102, the lifting plug 302 can not be recessed or extended relative to the casting cavity 102 after being positioned at the lowest point, the connecting frame 303 plays a role of connecting and supporting, the lifting plug 302 is limited by the sliding connection of the square sliding column 304 and the connecting frame 303, the lifting plug 302 only can slide up and down, the lifting plug 302 is positioned at the lowest point by the elastic force generated by the spring 305, when the extrusion sliding plug 106 moves left in the casting cavity 102 to compress the molten metal in the casting cavity 102, the molten metal in the casting cavity 102 can be squeezed together, when the molten metal is completely squeezed, the squeezed molten metal can be applied to the lifting plug 302, and when the lifting plug 302 moves upwards, the molten metal in the casting cavity 102 can be known to be completely squeezed, at this time, the extrusion of the molten metal in the casting cavity 102 is stopped, and only the cooling of the molten metal in the casting cavity 102 is needed to be waited for until the molten metal is solidified, so that the processing of the grooved cylindrical fixed rod is completed.
Referring to fig. 7 in the following, a remote sensing unmanned aerial vehicle mounting processing system further includes a top bolt 306, and the top bolt 306 is connected to the connection frame 303 through a thread.
When the lifting plug 302 moves upwards, it can be known that the molten metal in the casting cavity 102 is completely extruded, and at this time, the lifting plug 302 needs to return to the lowest point to ensure that the surface of the grooved cylindrical fixed rod to be processed is smooth, the top bolt 306 can be rotated to abut against the top bolt 306, the top bolt 306 can move downwards, so as to contact with the square sliding column 304 and drive the square sliding column to move downwards, and finally, the lifting plug 302 is driven to move downwards, so that the lifting plug 302 is located at the lowest point, thereby not only ensuring the smooth surface of the grooved cylindrical fixed rod to be processed, but also facilitating the discharge of the processed cylinder.
The remote sensing unmanned aerial vehicle fixing piece processing system further comprises a sliding switch, wherein the sliding switch is fixedly connected to the fixing base plate 101 through welding, and the sliding switch is in contact with and is in sliding connection with the casting cavity 102.
The opening at the left end of the casting cavity 102 is shielded and sealed by a slide switch, so that the molten metal is prevented from flowing out from the opening at the left end of the casting cavity 102.
Slide switch includes bearing seat 401, spacing square strip 402, telescopic link 403 and contact slide 404, and bearing seat 401 passes through welded fastening to be connected on fixed bedplate 101, and bearing seat 401 is last through welded fastening to be connected with spacing square strip 402 and telescopic link 403, through welded fastening to be connected with contact slide 404 on the telescopic link 403, contact slide 404 and spacing square strip 402 sliding connection, contact slide 404 and casting chamber 102 in close contact with and sliding connection.
Bearing seat 401 plays the effect of bearing the weight of and connecting, provide gliding space for spacing square strip 402 and telescopic link 403, spacing square strip 402 can provide gliding space and carry on spacingly to it for contact slide 404, let spacing square strip 402 can only slide around, utilize spacing square strip 402 to shelter from sealed the processing to the opening part of casting chamber 102 left end, prevent that the metal liquid in the casting chamber 102 from flowing out, after processing is accomplished in the trough of belt cylinder dead lever in casting chamber 102, start telescopic link 403 and drive contact slide 404 and remove, let the opening of casting chamber 102 left end expose, the convenient trough of belt cylinder dead lever that will be accomplished by processing discharges and carries out processing on next step.
The following description is made in detail with reference to fig. 1 and 9, and the remote sensing unmanned aerial vehicle fixing piece processing system further comprises a grinding component, and the grinding component is fixedly connected to the fixing seat plate 101 through welding.
The surface of the processed cylindrical fixing rod with the groove is polished by the polishing component, so that the smoothness of the surface of the cylindrical fixing rod with the groove is ensured.
The polishing component comprises an adapter 501, a polishing cavity 502, a linkage gear 503 and a transmission belt 504, the adapter 501 is fixedly connected to the fixed seat plate 101 through welding, the adapter 501 is rotatably connected with the polishing cavity 502 through a bearing, the fixed seat plate 101 is fixedly connected with a speed reduction motor through a plurality of screws, the output shaft of the speed reduction motor is fixedly connected with the linkage gear 503 through welding, and the linkage gear 503 is in transmission connection with the polishing cavity 502 through the transmission belt 504.
After the grooved cylinder dead lever that is accomplished by processing discharges, start gear motor on the fixed bedplate 101 and drive linkage gear 503 and rotate, pivoted linkage gear 503 accessible drive belt 504 drives and grinds chamber 502 and rotate, can directly stretch in grinding chamber 502 after the grooved cylinder dead lever that is accomplished by processing discharges, the right-hand member that grinds chamber 502 is the design of conical surface, conveniently enter into grinding chamber 502 by the grooved cylinder dead lever that is accomplished by processing, at this moment the pivoted is polished chamber 502 and can be polished the processing to the grooved cylinder dead lever that is accomplished by processing, ensure that the grooved cylinder dead lever surface that is accomplished by processing is smooth.
The following description is made in detail with reference to fig. 1 and 10, and the remote sensing unmanned aerial vehicle fixing piece processing system further comprises a smearing component, and the smearing component is fixedly connected to the fixing seat plate 101 through welding.
The component is paintd to the utilization on the trough of belt cylinder dead lever that finishes of polishing is paintd the anticorrosive coating, ensures that trough of belt cylinder dead lever can not corroded by the air, increases the life of trough of belt cylinder dead lever.
The smearing component comprises a supporting seat 601, smearing cotton 602 and a communicating conical opening 603, the supporting seat 601 is fixedly connected to the fixed seat plate 101 through welding, the smearing cotton 602 is fixedly connected to the supporting seat 601 through glue, the communicating conical opening 603 is fixedly connected to the supporting seat 601 through welding, and the communicating conical opening 603 is communicated with the smearing cotton 602.
Supporting seat 601 can provide fixed space for scribbling cotton 602, the anticorrosive liquid flows to scribbling on cotton 602 through intercommunication taper mouth 603, it has anticorrosive liquid to scribble to be stained with on the cotton 602, can and scribble cotton 602 contact after being discharged by the trough of belt cylinder dead lever of the completion of polishing, at this moment scribble the anticorrosive liquid on cotton 602 and can scribble on the trough of belt cylinder dead lever, accomplish the processing of trough of belt cylinder dead lever anticorrosive coating, the trough of belt cylinder dead lever of scribbling the anticorrosive coating can not corroded, and long service life is realized.
Claims (10)
1. The utility model provides a remote sensing unmanned aerial vehicle mounting system of processing, includes fixed bedplate (101), casting chamber (102), filling tube (103) and stretches out the component, its characterized in that: the fixed seat plate (101) is fixedly connected with a casting cavity (102), the fixed seat plate (101) is fixedly connected with a feeding pipe (103) and communicated, the fixed seat plate (101) is connected with a stretching component which can slide, and the stretching component is connected with the casting cavity (102) in a sliding manner.
2. The remote sensing unmanned aerial vehicle mounting system of processing of claim 1, characterized in that: the extension component comprises a limiting slide bar (201), a bidirectional screw rod (202), vertical fixing plates (203), extension blocks (204) and a hollow notch (205), a through hollow notch (205) is formed in a casting cavity (102), two limiting slide bars (201) are fixedly connected to a fixed seat plate (101), the bidirectional screw rod (202) is rotatably connected to the fixed seat plate (101), two vertical fixing plates (203) are slidably connected to the two limiting slide bars (201), the two vertical fixing plates (203) are respectively connected to two ends of the bidirectional screw rod (202) through threads, the extension blocks (204) are fixedly connected to the two vertical fixing plates (203), and the two extension blocks (204) are slidably connected to the hollow notch (205).
3. The remote sensing unmanned aerial vehicle mounting system of processing of claim 2, characterized in that: a plurality of conical bosses are arranged inside the two extension blocks (204).
4. The remote sensing unmanned aerial vehicle mounting system of processing of claim 1, characterized in that: the casting cavity is characterized by further comprising side sealing plates (104), an external sliding column (105) and an extrusion sliding plug (106), wherein the side sealing plates (104) are fixedly connected to the casting cavity (102), the external sliding column (105) is connected to the side sealing plates (104) in a sliding mode, the extrusion sliding plug (106) is fixedly connected to the external sliding column (105), and the extrusion sliding plug (106) is connected to the casting cavity (102) in a sliding mode.
5. The remote sensing unmanned aerial vehicle mounting system of processing of claim 4, characterized in that: and a rubber sleeve is fixedly connected to the outer curved surface of the extrusion sliding plug (106).
6. The remote sensing unmanned aerial vehicle mounting system of processing of claim 4, characterized in that: still including extending chamber (301), lift stopper (302), linking frame (303), square traveller (304) and spring (305), casting chamber (102) is gone up fixedly connected with and is extended chamber (301) and linking frame (303), sliding connection has square traveller (304) on linking frame (303), the below fixedly connected with of square traveller (304) goes up and down stopper (302), lift stopper (302) sliding connection is in extending chamber (301), the cover is equipped with spring (305) on square traveller (304), spring (305) are located between lift stopper (302) and linking frame (303).
7. The remote sensing unmanned aerial vehicle mounting system of processing of claim 6, characterized in that: the device also comprises a top-leaning bolt (306), wherein the top-leaning bolt (306) is connected to the connecting frame (303) through threads.
8. The remote sensing unmanned aerial vehicle mounting system of processing of claim 1, characterized in that: the casting device is characterized by further comprising a sliding switch, wherein the sliding switch capable of sealing and sealing the opening at the left end of the casting cavity (102) is fixedly connected to the fixed base plate (101), and the sliding switch is in contact with and is in sliding connection with the casting cavity (102).
9. The remote sensing unmanned aerial vehicle mounting system of processing of claim 1, characterized in that: still include adapter (501), the chamber of polishing (502), linkage gear (503) and drive belt (504), adapter (501) fixed connection is on fixed bedplate (101), rotate on adapter (501) and be connected with the chamber of polishing (502), fixedly connected with gear motor on fixed bedplate (101), fixedly connected with linkage gear (503) on gear motor's the output shaft, linkage gear (503) are connected through drive belt (504) transmission with the chamber of polishing (502).
10. The remote sensing unmanned aerial vehicle mounting system of processing of claim 9, characterized in that: the anti-corrosion coating device is characterized by further comprising a coating component, wherein the coating component capable of coating an anti-corrosion coating on the surface of the cast cylinder is fixedly connected to the fixed seat plate (101).
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| CN202110519711.XA CN113245925B (en) | 2021-05-13 | 2021-05-13 | Remote sensing unmanned aerial vehicle mounting system of processing |
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| CN202110519711.XA CN113245925B (en) | 2021-05-13 | 2021-05-13 | Remote sensing unmanned aerial vehicle mounting system of processing |
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| CN112439649A (en) * | 2020-11-30 | 2021-03-05 | 金华市彩橙机床有限公司 | Equipment is filled to inner wall gas pocket of annular casting |
| CN212792932U (en) * | 2020-07-02 | 2021-03-26 | 苏州市铧厦精密部件股份有限公司 | Heat dissipation aluminum seat die-casting forming die |
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Also Published As
| Publication number | Publication date |
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| CN113245925B (en) | 2022-01-28 |
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