CN112496455A

CN112496455A - Anti-splashing cutting device for solar lunar vehicle

Info

Publication number: CN112496455A
Application number: CN202011311615.8A
Authority: CN
Inventors: 邓利云; 陈志强; 周颜芝; 罗双印
Original assignee: Hengyang Huiyu Technology Co ltd
Current assignee: Hengyang Huiyu Technology Co ltd
Priority date: 2020-11-20
Filing date: 2020-11-20
Publication date: 2021-03-16

Abstract

The invention discloses a splash-proof cutting device for a solar lunar vehicle, which comprises a shell, wherein the bottom wall of the inner side of the shell is provided with a chute, the inner side wall of the chute is symmetrically and slidably connected with two sliding blocks, the top of each sliding block is welded with a supporting block, the upper surface of each supporting block is provided with a first through groove, and the inner side wall of each first through groove is slidably connected with a supporting plate; through starting first electric putter, first electric putter drives the fixed plate and fixes solar energy lunar rover part, avoid rocking when cutting solar energy lunar rover part and influence the effect of cutting, promote the effect to solar energy lunar rover part cutting, start two second electric putter simultaneously, make the box rise to cutting department to solar energy lunar rover part, the waste material that splashes enters into the inside of box through trapezoidal recess, thereby play the effect to operating personnel protection, avoid operating personnel injured.

Description

Anti-splashing cutting device for solar lunar vehicle

Technical Field

The invention relates to the technical field of solar lunar vehicles, in particular to a splash-proof cutting device for a solar lunar vehicle.

Background

Solar energy is a renewable energy source. Refers to the thermal radiation energy of the sun, and refers to three modes of thermal energy propagation: the main manifestation of radiation is the so-called sun rays. In modern times it is commonly used to generate electricity or to power water heaters. Since the birth of life on the earth, people mainly live by the heat radiation energy provided by the sun, and ancient mankind also understand that objects are dried in the sun and used as methods for making food, such as salt making, salted fish drying and the like. With the ever-decreasing consumption of fossil fuels, solar energy has become an important component of energy used by humans and is constantly being developed. The lunar rover is a research and development task with complex technology and strict requirements, and developers need to break through and master the technologies of light machinery, mechanisms, teleoperation, autonomous navigation, mechanical arms and the like related to the robot, and more importantly, develop and manage according to the specification and the standard of a spacecraft. The method is divided into two types, namely an unmanned lunar vehicle and a manned lunar vehicle.

China discloses the invention: CN111547272A discloses a manned lunar vehicle, wherein a front module and a rear module are hinged with each other through a coupling mechanism, so that the lunar vehicle can be easily disassembled and has high trafficability, and has adaptability to complex terrains; the structure and the size of four walking units are the same, and the walking unit trouble of preceding module can replace the walking unit of using the back module, has effectively ensured astronaut's in the preceding module security, then the user of service is convenient for the position that indicates to L type gauge stick on the scale mark, nevertheless still has following problem:

firstly, when the manned lunar vehicle is produced, the parts of the manned lunar vehicle need to be cut, the part cutting operation of the manned lunar vehicle can generate a shaking phenomenon, so that the effect of cutting the parts of the manned lunar vehicle is influenced, and meanwhile, when the parts of the manned lunar vehicle are cut, splashed waste materials can injure personnel performing the cutting operation;

secondly, after the parts of the manned lunar rover are cut, scattered waste materials are scattered in the operation place and need to be cleaned by an operator, so that the operation amount of the operator is increased, and the working efficiency of the operator is reduced.

Disclosure of Invention

Technical problem to be solved

Aiming at the defects of the prior art, the invention provides a splash-proof cutting device for a solar lunar vehicle.

(II) technical scheme

In order to achieve the purpose, the invention provides the following technical scheme: a splash-proof cutting device for a solar lunar vehicle comprises a shell, wherein a sliding groove is formed in the bottom wall of the inner side of the shell, two sliding blocks are symmetrically and slidably connected to the inner side wall of the sliding groove, a supporting block is welded to the top of each sliding block, a first through groove is formed in the upper surface of each supporting block, a supporting plate is slidably connected to the inner side wall of each first through groove, a first electric push rod and four second electric push rods are respectively mounted on the inner side wall of the shell, the two second electric push rods and the first electric push rod are located on the top wall of the inner side of the shell, the other two second electric push rods are located on the bottom wall of the inner side of the shell, the four second electric push rods are symmetrically arranged, the first electric push rods and the supporting blocks are symmetrically arranged, a fixing plate is welded to the piston rods of, the fixed rod is positioned between the two second electric push rods, the inner side bottom wall of the shell is welded with the supporting rod, the supporting rod and the fixed rod are symmetrically arranged, the outer side wall of the supporting rod is connected with a sleeve in a sliding way, a second through hole is formed inside the sleeve, the outer side wall of the supporting rod is provided with three first through holes, the second through hole is inserted into the inner side wall of one first through hole to form an inserting rod, the sleeve and the fixed rod are both internally provided with a third groove, the inner side wall of the third groove is provided with a motor, the output shaft of the motor is welded with a connecting rod, the outer side wall of the connecting rod is welded with a second bevel gear, the outer ring of the second bevel gear is engaged and connected with a first bevel gear, the inner ring of the first bevel gear is welded with a rod body, the outer side wall of the connecting plate is welded with a box body, the outer side wall of the box body is provided with a trapezoidal through groove, the outer side wall of the connecting plate is in threaded connection with a scraper, the outer side wall of the scraper is attached to the outer side wall of the fixed rod, the scraper is located above the box body, and the bottom of the shell is welded with a bottom plate.

Further, the top of box intercommunication has the toper pipe, the bottom intercommunication of toper pipe has the body, the lateral wall of body connect in the inside wall of box.

Furthermore, a first groove is formed in the outer side wall of the shell, and a visual window is arranged in the first groove.

As a further scheme of the present invention, a door body is installed on the front surface of the housing, and a second groove is formed on the front surface of the door body.

Further, the bottom wall of the inner side of the supporting block is provided with an air bag, and the bottom of the supporting plate is attached to the top of the air bag.

On the basis of the scheme, four circular grooves are symmetrically formed in the upper surface of the shell, and the inner side wall of each circular groove is in threaded connection with a dust screen.

Furthermore, two clamping grooves are symmetrically formed in the inner side wall of the connecting plate, two clamping blocks are symmetrically welded to the lower surface of the box body, and the outer side walls of the clamping blocks are inserted into the inner side walls of the clamping grooves.

On the basis of the scheme, an inflation valve is installed on the outer side wall of the air bag.

(III) advantageous effects

Compared with the prior art, the invention provides the anti-splashing cutting device for the solar lunar vehicle, which has the following beneficial effects:

the method comprises the steps that firstly, by starting a first electric push rod, the first electric push rod drives a fixing plate to fix a solar lunar rover part, the situation that the cutting effect is influenced due to the fact that the solar lunar rover part is shaken when cut is avoided, the cutting effect on the solar lunar rover part is improved, meanwhile, two second electric push rods are started, a box body is made to ascend to the position where the solar lunar rover part is cut, splashed waste materials enter the box body through a trapezoid groove, the effect of protecting operating personnel is achieved, and the operating personnel are prevented from being injured;

two, through starting two second electric putter, make second electric putter drive the scraper blade through the connecting plate and clear up support column and telescopic outer wall, clear up the inside of box with the waste material that part splashes, avoid operating personnel to need clear up the operation, alleviate operating personnel's work load, promote operating personnel's work efficiency.

Drawings

FIG. 1 is a schematic structural view of the present invention;

FIG. 2 is a schematic view of the internal structure of the housing according to the present invention;

FIG. 3 is a schematic structural diagram of the case of the present invention;

FIG. 4 is a schematic view of a connection structure of a first bevel gear and a second bevel gear in the invention.

In the figure: 1. a housing; 2. a first groove; 3. a base plate; 4. a door body; 5. a visual window; 6. a second groove; 7. a circular groove; 8. a dust screen; 9. an air bag; 10. a chute; 11. a slider; 12. an inflation valve; 13. a support plate; 14. a first through groove; 15. a first electric push rod; 16. a fixing plate; 17. a squeegee; 18. a tapered tube; 19. a box body; 20. a sleeve; 21. a second electric push rod; 22. fixing the rod; 23. a support bar; 24. a first through hole; 25. a second through hole; 26. a plug rod; 27. a third groove; 28. a clamping block; 29. a card slot; 30. a pipe body; 31. a trapezoidal through groove; 32. a connecting rod; 34. a connecting plate; 35. a motor; 36. a first bevel gear; 37. a rod body; 38. a cutting knife; 39. a second bevel gear; 40. and (7) a supporting block.

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.

Example one

Referring to fig. 1-4, the present invention provides a technical solution: a splash-proof cutting device for a solar lunar rover comprises a shell 1, a sliding groove 10 is formed in the inner side bottom wall of the shell 1, two sliding blocks 11 are symmetrically and slidably connected to the inner side wall of the sliding groove 10, supporting blocks 40 are welded to the tops of the sliding blocks 11, a first through groove 14 is formed in the upper surface of each supporting block 40, a supporting plate 13 is slidably connected to the inner side wall of each first through groove 14, a first electric push rod 15 and four second electric push rods 21 are respectively installed on the inner side wall of the shell 1, the two second electric push rods 21 and the first electric push rod 15 are located on the inner side top wall of the shell 1, the other two second electric push rods 21 are located on the inner side bottom wall of the shell 1, the four second electric push rods 21 are symmetrically arranged, the first electric push rods 15 and the supporting blocks 40 are symmetrically arranged, a fixing plate 16 is welded to a piston rod of the first electric push rod 15, the inner side bottom wall of the shell 1 is welded with a support rod 23, the support rod 23 and a fixed rod 22 are symmetrically arranged, the outer side wall of the support rod 23 is slidably connected with a sleeve 20, a second through hole 25 is formed in the sleeve 20, the outer side wall of the support rod 23 is provided with three first through holes 24, an inserting rod 26 is inserted into the inner side wall of one first through hole 24 and the second through hole 25, a third groove 27 is formed in the sleeve 20 and the fixed rod 22, a motor 35 is installed on the inner side wall of the third groove 27, an output shaft of the motor 35 is welded with a connecting rod 32, the outer side wall of the connecting rod 32 is welded with a second bevel gear 39, the outer ring of the second bevel gear 39 is engaged and connected with a first bevel gear 36, the inner ring of the first bevel gear 36 is welded with a rod body 37, one end of the rod, the outer side wall of the box body 19 is provided with a trapezoidal through groove 31, the outer side walls of the other two connecting plates 34 are in threaded connection with the scraping plates 17, the outer side walls of the scraping plates 17 are attached to the outer side walls of the fixing rods 22, the scraping plates 17 are located above the box body 19, and the bottom of the shell 1 is welded with the bottom plate 3; the switch group for controlling the start and the stop of the first electric push rod 15, the second electric push rod 21 and the motor 35 is installed on the outer side wall of the shell 1, and the switch group is connected with an external mains supply and used for supplying power to the first electric push rod 15, the second electric push rod 21 and the motor 35.

In this embodiment, specifically: the top of the box body 19 is communicated with a conical pipe 18, the bottom of the conical pipe 18 is communicated with a pipe body 30, and the outer side wall of the pipe body 30 is connected with the inner side wall of the box body 19; by arranging the tapered tube 18 and the tube body 30, the tapered tube 18 increases the area after receiving and cleaning dust, and the dust is prevented from entering the bottom of the shell 1, so that the workload of operators is increased.

In this embodiment, specifically: the outer side wall of the shell 1 is provided with a first groove 2, and a visual window 5 is arranged in the first groove 2; through setting up first recess 2 and visual window 5, first recess 2 is used for fixed visual window 5, and operating personnel passes through visual window 5, is convenient for carry out operation on next step to solar energy lunar rover part.

In this embodiment, specifically: a door body 4 is arranged on the front surface of the shell 1, and a second groove 6 is formed in the front surface of the door body 4; through setting up the door body 4 and second recess 6, operating personnel opens the door body 4 again through putting into the inside of second recess 6 with the hand, puts into or takes out solar energy lunar rover part, maintains and clears up the inside of casing 1 simultaneously.

Example two

The invention also provides an embodiment different from the first embodiment, and the difference from the first embodiment is that:

an air bag 9 is arranged on the bottom wall of the inner side of a supporting block 40, and the bottom of a supporting plate 13 is attached to the top of the air bag 9; through setting up gasbag 9, after solar energy lunar rover part placed in backup pad 13, at the fixed plate 16 simultaneously to the fixed back of solar energy lunar rover part, the vibration that cutting knife 38 produced when cutting solar energy lunar rover part carries out the shock attenuation through gasbag 9, promotes the stability to solar energy lunar rover part.

In this embodiment, specifically: four circular grooves 7 are symmetrically formed in the upper surface of the shell 1, and the inner side walls of the circular grooves 7 are in threaded connection with dust screens 8; through setting up dust screen 8 and circular recess 7, circular recess 7 is used for the air admission and exhaust for the inside of casing 1 is taken a breath, and dust screen 8 plays the effect to dirt-proof, avoids the dust to enter into the inside of casing 1, influences inside equipment operation.

In this embodiment, specifically: two clamping grooves 29 are symmetrically formed in the inner side wall of the connecting plate 34, two clamping blocks 28 are symmetrically welded to the lower surface of the box body 19, and the outer side walls of the clamping blocks 28 are inserted into the inner side walls of the clamping grooves 29; by arranging the clamping block 28 and the clamping groove 29, an operator separates the clamping block 28 from the clamping groove 29, so that the box body 19 is separated from the connecting plate 34, and the operator cleans dust and impurities in the box body 19.

In this embodiment, specifically: the outer side wall of the air bag 9 is provided with an inflation valve 12; by providing the inflation valve 12, the inflation valve 12 is used to supplement the interior of the airbag 9 with gas.

In this embodiment, the types of the first electric push rod 15 and the second electric push rod 21 are: SC 63.

In this embodiment, the motor 35 is of the type: 5IK60 GU-CF.

To sum up, the working principle and working process of the splash-proof cutting device for the solar lunar rover are that when the splash-proof cutting device is used, firstly, an operator puts hands into the second groove 6, opens the door body 4, puts solar lunar rover parts on the surface of the supporting plate 13, starts the first electric push rod 15 by using the switch group, the first electric push rod 15 drives the fixing plate 16 to move downwards, so that the fixing plate 16 fixes the solar lunar rover parts, then the operator puts the solar lunar rover parts between the two cutting knives 38, moves the sleeve 20 to drive one cutting knife 38 to ascend, when the insertion rod 26 is respectively inserted into the first through hole 24 and the second through hole 25 to fix the sleeve 20, the sleeve 20 is prevented from shaking during cutting operation, so that the cutting knife 38 is adjusted, when the solar lunar rover parts are positioned between the two cutting knives 38, an operator closes the door body 4, starts the second electric push rod 21, the piston rod of the second electric push rod 21 drives the box body 19 to lift through the connecting plate 34, the trapezoidal through groove 31 is positioned at the cutting position of the solar lunar rover part, the motor 35 is started, the output shaft of the motor 35 drives the connecting rod 32 to rotate, the connecting rod 32 drives the second bevel gear 39 to rotate, the second bevel gear 39 drives the first bevel gear 36, the first bevel gear 36 drives the rod body 37 to rotate, the rod body 37 drives the cutter 38 to rotate, the cutter 38 cuts the solar lunar rover part, splashed waste materials are generated by cutting the solar lunar rover part, the waste materials enter the box body 19 through the trapezoidal through groove 31, after the solar lunar rover part is cut, the operator sequentially drives the connecting plate 34 and the scraper 17 to move by starting the second electric push rod 21, and the scraper 17 cleans the outer side walls of the fixed rod 22 and the sleeve 20, the cleaned dust and sundries enter the box body 19 through the conical pipe 18 and the pipe body 30, and therefore the cleaning operation is completed.

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

1. The utility model provides a solar energy lunar rover is with preventing cutting device that splashes, includes casing (1), its characterized in that: the inner side bottom wall of the shell (1) is provided with a sliding groove (10), the inner side wall of the sliding groove (10) is symmetrically and slidably connected with two sliding blocks (11), the top of each sliding block (11) is welded with a supporting block (40), the upper surface of each supporting block (40) is provided with a first through groove (14), the inner side wall of each first through groove (14) is slidably connected with a supporting plate (13), the inner side wall of the shell (1) is respectively provided with a first electric push rod (15) and four second electric push rods (21), the two second electric push rods (21) and the first electric push rod (15) are positioned on the inner side top wall of the shell (1), the other two second electric push rods (21) are positioned on the inner side bottom wall of the shell (1), the four second electric push rods (21) are symmetrically arranged, and the first electric push rods (15) and the supporting blocks (40) are symmetrically arranged, a fixed plate (16) is welded on a piston rod of the first electric push rod (15), a fixed rod (22) is welded on the top wall of the inner side of the shell (1), the fixed rod (22) is positioned between the two second electric push rods (21), a support rod (23) is welded on the bottom wall of the inner side of the shell (1), the support rod (23) and the fixed rod (22) are symmetrically arranged, the outer side wall of the support rod (23) is connected with a sleeve (20) in a sliding manner, a second through hole (25) is formed in the sleeve (20), three first through holes (24) are formed in the outer side wall of the support rod (23), an inserting rod (26) is inserted into the inner side wall of one first through hole (24) in the second through hole (25), third grooves (27) are formed in the sleeve (20) and the fixed rod (22), and a motor (35) is installed on the inner side wall of the third, the output shaft of the motor (35) is welded with a connecting rod (32), the outer side wall of the connecting rod (32) is welded with a second bevel gear (39), the outer ring of the second bevel gear (39) is meshed with a first bevel gear (36), the inner ring of the first bevel gear (36) is welded with a rod body (37), one end of the rod body (37) is provided with a cutting knife (38), the piston rod of the second electric push rod (21) is provided with connecting plates (34), the outer side walls of the two connecting plates (34) are welded with a box body (19), the outer side wall of the box body (19) is provided with a trapezoidal through groove (31), the outer side walls of the other two connecting plates (34) are in threaded connection with a scraping plate (17), the outer side wall of the scraping plate (17) is attached to the outer side wall of the fixing rod (, the bottom of the shell (1) is welded with a bottom plate (3).

2. The anti-spatter cutting device for a solar lunar vehicle according to claim 1, wherein: the top of the box body (19) is communicated with a conical pipe (18), the bottom of the conical pipe (18) is communicated with a pipe body (30), and the outer side wall of the pipe body (30) is connected with the inner side wall of the box body (19).

3. The anti-spatter cutting device for a solar lunar vehicle according to claim 1, wherein: the outer side wall of the shell (1) is provided with a first groove (2), and a visual window (5) is arranged in the first groove (2).

4. The anti-spatter cutting device for a solar lunar vehicle according to claim 1, wherein: a door body (4) is installed on the front surface of the shell (1), and a second groove (6) is formed in the front surface of the door body (4).

5. The anti-spatter cutting device for a solar lunar vehicle according to claim 1, wherein: an air bag (9) is installed on the bottom wall of the inner side of the supporting block (40), and the bottom of the supporting plate (13) is attached to the top of the air bag (9).

6. The anti-spatter cutting device for a solar lunar vehicle according to claim 1, wherein: four circular grooves (7) are symmetrically formed in the upper surface of the shell (1), and dust screens (8) are connected to the inner side walls of the circular grooves (7) in a threaded mode.

7. The anti-spatter cutting device for a solar lunar vehicle according to claim 1, wherein: two clamping grooves (29) are symmetrically formed in the inner side wall of the connecting plate (34), two clamping blocks (28) are symmetrically welded to the lower surface of the box body (19), and the outer side wall of each clamping block (28) is inserted into the inner side wall of each clamping groove (29).

8. The anti-spatter cutting device for a solar lunar vehicle according to claim 5, wherein: and an inflation valve (12) is arranged on the outer side wall of the air bag (9).