CN214655113U - Vacuum heat treatment device for metal parts for aviation seat - Google Patents
Vacuum heat treatment device for metal parts for aviation seat Download PDFInfo
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- CN214655113U CN214655113U CN202022347659.8U CN202022347659U CN214655113U CN 214655113 U CN214655113 U CN 214655113U CN 202022347659 U CN202022347659 U CN 202022347659U CN 214655113 U CN214655113 U CN 214655113U
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- fixed connection
- vacuum heat
- screw rod
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Abstract
The utility model discloses a metal parts vacuum heat treatment device for aviation seat relates to vacuum heat treatment device technical field, for solving the ordinary vacuum treatment device among the prior art problem that the metal parts treatment effect is not good enough for the aviation seat. The swivel mount is installed to the top of seal receptacle, and swivel mount and seal receptacle rotate to be connected, first servo motor is installed to the below of seal receptacle, and first servo motor and seal receptacle fixed connection, first reduction gear is installed to first servo motor's top, first servo motor and swivel mount are all through shaft coupling and first reduction gear fixed connection, the transposable top is provided with the material frame, the landing leg is installed to the below of seal receptacle, and landing leg and seal receptacle fixed connection, the pulley is installed to the below of landing leg, and the pulley rotates with the landing leg to be connected, the below of pulley is provided with the slide rail, and pulley and slide rail roll connection.
Description
Technical Field
The utility model relates to a vacuum heat treatment device technical field specifically is metal parts vacuum heat treatment device for aviation seat.
Background
The vacuum heat treatment is a novel heat treatment technology combining a vacuum technology and a heat treatment technology, the vacuum environment of the vacuum heat treatment refers to an atmosphere environment lower than one atmosphere pressure, including low vacuum, medium vacuum, high vacuum and ultrahigh vacuum, the vacuum heat treatment actually belongs to atmosphere control heat treatment, the vacuum heat treatment refers to that all and part of the heat treatment process are carried out in a vacuum state, the heat treatment quality is greatly improved, compared with the conventional heat treatment, the vacuum heat treatment can realize no oxidation, no decarburization and no carburization at the same time, can remove phosphorus chips on the surface of a workpiece, and has the functions of degreasing, degassing and the like, so that the effect of surface brightness purification is achieved.
The metal parts for the aviation seat have higher requirements on the process, and the metal parts cannot move when the common vacuum heat treatment device carries out heat treatment on the metal parts, so that the heat treatment effect is not good enough; therefore, the market urgently needs to develop a vacuum heat treatment device for metal parts for aviation seats to help people to solve the existing problems.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a metal parts vacuum heat treatment device for aircraft seat to solve the ordinary vacuum treatment device that provides among the above-mentioned background art and not good enough problem of metal parts treatment effect for the aircraft seat.
In order to achieve the above object, the utility model provides a following technical scheme: aviation is metal part vacuum heat treatment device for seat, including seal receptacle and pillar, the swivel mount is installed to the top of seal receptacle, and swivel mount and seal receptacle rotate to be connected, first servo motor is installed to the below of seal receptacle, and first servo motor and seal receptacle fixed connection, first reduction gear is installed to first servo motor's top, first servo motor and swivel mount all pass through shaft coupling and first reduction gear fixed connection, the transposable top is provided with the material frame, the landing leg is installed to the below of seal receptacle, and landing leg and seal receptacle fixed connection, the pulley is installed to the below of landing leg, and the pulley rotates with the landing leg to be connected, the below of pulley is provided with the slide rail, and pulley and slide rail roll connection.
Preferably, first horizontal pole is installed to one side of pillar, and first horizontal pole and pillar welded connection, the second horizontal pole is installed to the top of pillar, and second horizontal pole and pillar welded connection, first screw rod and second screw rod are installed respectively to the top of first horizontal pole, and just first screw rod and second screw rod all rotate with first horizontal pole to be connected, first screw rod and second screw rod all rotate with the second horizontal pole to be connected, the below of seal receptacle is provided with the layer board, first screw rod and second screw rod all with layer board threaded connection.
Preferably, second servo motor is installed to the top of pillar, and second servo motor and pillar fixed connection, the second reduction gear is installed to second servo motor's below, first screw rod and second servo motor all pass through shaft coupling and second reduction gear fixed connection, drive gear is installed in the outside of first screw rod, and drive gear and first screw rod fixed connection, the top of second horizontal pole is provided with the transmission shaft, driven gear is installed in the outside of second screw rod, and driven gear and second screw rod fixed connection.
Preferably, a first transmission gear is installed at one end of the transmission shaft, a second transmission gear is installed at the other end of the transmission shaft, the first transmission gear and the second transmission gear are both fixedly connected with the transmission shaft, the first transmission gear is connected with the driving gear in an occlusion mode, and the second transmission gear is connected with the driven gear in an occlusion mode.
Preferably, a vacuum heat treatment furnace is installed above the second cross rod and is fixedly connected with the second cross rod, an exhaust pipe is arranged above the vacuum heat treatment furnace and is integrated with the vacuum heat treatment furnace, an electric heating plate is installed inside the vacuum heat treatment furnace and is fixedly connected with the vacuum heat treatment furnace.
Preferably, the gas-supply pipe is installed to the top of exhaust tube, and the gas-supply pipe passes through flange fixed connection with the exhaust tube, the valve is installed in the outside of gas-supply pipe, and valve and gas-supply pipe fixed connection, the one end that the exhaust tube was kept away from to the gas-supply pipe is installed the vacuum pump, and the vacuum pump passes through flange fixed connection with the gas-supply pipe, the top of vacuum pump is provided with the filter tube, and filter tube and vacuum pump set up structure as an organic whole, the internally mounted of filter tube has the filter pulp, and filter pulp and filter tube fixed connection.
Compared with the prior art, the beneficial effects of the utility model are that:
1. the utility model discloses a through the setting of swivel mount, the top of swivel mount is provided with the material frame, the metal parts that the aviation seat was used can be placed in the top of material frame, the first servo motor drive of swivel mount accessible rotates simultaneously to make vacuum heat treatment furnace when to metal parts vacuum heating process, make material frame and metal parts rotate through the swivel mount, thereby make all metal parts can be by even heating and thermal treatment, thereby provide the heat treatment effect, make metal parts's better quality.
2. The utility model discloses a through the setting of filter tube, the internally mounted of filter tube has the filter pulp, can block the impurity in the air through the filter pulp, when the inside delivery air to vacuum heat treatment furnace through the vacuum pump for when cooling, can prevent that the impurity of air from polluting the metal parts to improve the smoothness of metal parts thermal treatment rear surface.
Drawings
FIG. 1 is a front view of the vacuum heat treatment apparatus for metal parts for aviation seats of the present invention;
FIG. 2 is a schematic view of the internal structure of the vacuum heat treatment furnace of the present invention;
fig. 3 is a schematic view of the internal structure of the filtering pipe of the present invention.
In the figure: 1. a sealing seat; 2. rotating; 3. a first decelerator; 4. a first servo motor; 5. a support leg; 6. a pulley; 7. a material rack; 8. a pillar; 9. a first cross bar; 10. a second cross bar; 11. a first screw; 12. a support plate; 13. a second servo motor; 14. a second decelerator; 15. a drive gear; 16. a first drive gear; 17. a drive shaft; 18. a driven gear; 19. a second screw; 20. a vacuum heat treatment furnace; 21. an air exhaust pipe; 22. a gas delivery pipe; 23. a valve; 24. a vacuum pump; 25. a filter tube; 26. an electrical heating plate; 27. filtering cotton; 28. a second transmission gear.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.
Referring to fig. 1-3, the present invention provides an embodiment: aviation is metal part vacuum heat treatment device for seat, including seal receptacle 1 and pillar 8, swivel mount 2 is installed to seal receptacle 1's top, and swivel mount 2 rotates with seal receptacle 1 and is connected, first servo motor 4 is installed to seal receptacle 1's below, and first servo motor 4 and seal receptacle 1 fixed connection, first reduction gear 3 is installed to first servo motor 4's top, first servo motor 4 and swivel mount 2 all pass through shaft coupling and first reduction gear 3 fixed connection, swivel mount 2's top is provided with material frame 7, landing leg 5 is installed to seal receptacle 1's below, and landing leg 5 and seal receptacle 1 fixed connection, pulley 6 is installed to landing leg 5's below, and pulley 6 rotates with landing leg 5 to be connected, pulley 6's below is provided with the slide rail, and pulley 6 and slide rail roll connection.
Further, first horizontal pole 9 is installed to one side of pillar 8, and first horizontal pole 9 and pillar 8 welded connection, second horizontal pole 10 is installed to the top of pillar 8, and second horizontal pole 10 and pillar 8 welded connection, first screw rod 11 and second screw rod 19 are installed respectively to the top of first horizontal pole 9, and first screw rod 11 and second screw rod 19 all rotate with first horizontal pole 9 and be connected, first screw rod 11 and second screw rod 19 all rotate with second horizontal pole 10 and be connected, the below of seal receptacle 1 is provided with layer board 12, first screw rod 11 and second screw rod 19 all with layer board 12 threaded connection, first horizontal pole 9, first screw rod 11 and second screw rod 19 all are provided with two, pillar 8 and second horizontal pole 10 all are provided with four.
Further, a second servo motor 13 is installed above the support column 8, the second servo motor 13 is fixedly connected with the support column 8, a second speed reducer 14 is installed below the second servo motor 13, the first screw rod 11 and the second servo motor 13 are fixedly connected with the second speed reducer 14 through a coupler, a driving gear 15 is installed on the outer side of the first screw rod 11, the driving gear 15 is fixedly connected with the first screw rod 11, a transmission shaft 17 is arranged above the second cross rod 10, a driven gear 18 is installed on the outer side of the second screw rod 19, the driven gear 18 is fixedly connected with the second screw rod 19, and the driving gear 15, the second servo motor 13 and the second speed reducer 14 are all provided with two gears.
Further, a first transmission gear 16 is installed at one end of the transmission shaft 17, a second transmission gear 28 is installed at the other end of the transmission shaft 17, the first transmission gear 16 and the second transmission gear 28 are both fixedly connected with the transmission shaft 17, the first transmission gear 16 is connected with the driving gear 15 in an occlusion mode, the second transmission gear 28 is connected with the driven gear 18 in an occlusion mode, a fixing table is arranged between the transmission shaft 17 and the second cross rod 10, and the fixing table is rotatably connected with the transmission shaft 17 and used for supporting and fixing the transmission shaft 17.
Further, a vacuum heat treatment furnace 20 is installed above the second cross bar 10, the vacuum heat treatment furnace 20 is fixedly connected with the second cross bar 10, an exhaust pipe 21 is arranged above the vacuum heat treatment furnace 20, the exhaust pipe 21 and the vacuum heat treatment furnace 20 are arranged into an integral structure, an electric heating plate 26 is installed inside the vacuum heat treatment furnace 20, the electric heating plate 26 is fixedly connected with the vacuum heat treatment furnace 20, the electric heating plate 26 surrounds the inner wall of the vacuum heat treatment furnace 20 for a circle, and the lower side of the vacuum heat treatment furnace 20 is in an open state.
Further, the air delivery pipe 22 is installed to the top of exhaust tube 21, and air delivery pipe 22 passes through flange fixed connection with exhaust tube 21, valve 23 is installed in the outside of air delivery pipe 22, and valve 23 and air delivery pipe 22 fixed connection, vacuum pump 24 is installed to the one end that exhaust tube 21 was kept away from to air delivery pipe 22, and vacuum pump 24 passes through flange fixed connection with air delivery pipe 22, vacuum pump 24's top is provided with filter tube 25, and filter tube 25 sets up structure as an organic whole with vacuum pump 24, the internally mounted of filter tube 25 has filter pulp 27, and filter pulp 27 and filter tube 25 fixed connection, vacuum pump 24 can bleed, also can blow simultaneously.
The working principle is as follows: when the device is used, metal parts for the aviation seat are placed on the material frame 7, the sealing seat 1 is pushed to be under the vacuum heat treatment furnace 20, then the second servo motor 13 is started, the second servo motor 13 drives the first screw rod 11 after being decelerated by the second speed reducer 14, the first screw rod 11 drives the first transmission gear 16 to rotate through the driving gear 15, so that the transmission shaft 17 rotates, the transmission shaft 17 drives the second screw rod 19 to rotate through the second transmission gear 28 and the driven gear 18, so that the first screw rod 11 and the second screw rod 19 rotate simultaneously, the supporting plate 12 supports the sealing seat 1 through the rotation of the first screw rod 11 and the second screw rod 19, so that the sealing seat 1 is lifted to be lifted to the bottom of the vacuum heat treatment furnace 20, the material frame 7 is pushed into the vacuum heat treatment furnace 20, and finally the sealing seat 1 is tightly attached to the bottom of the vacuum heat treatment furnace 20, starting a vacuum pump 24, opening a valve 23, extracting the air inside the vacuum heat treatment furnace 20 by the vacuum pump 24 through an air conveying pipe 22 and an air exhaust pipe 21, enabling the inside of the vacuum heat treatment furnace 20 to be in a vacuum state, then electrifying an electric heating plate 26, enabling the temperature inside the vacuum heat treatment furnace 20 to rise, realizing the heating effect, starting a first servo motor 4, driving a rotary seat 2 to rotate after the first servo motor 4 is decelerated through a first speed reducer 3, and enabling a material rack 7 to rotate, so that all metal parts on the material rack 7 can be uniformly heated.
It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Claims (6)
1. Aviation is metal parts vacuum heat treatment device for seat, including seal receptacle (1) and pillar (8), its characterized in that: swivel mount (2) is installed to the top of seal receptacle (1), and swivel mount (2) rotates with seal receptacle (1) and is connected, first servo motor (4) is installed to the below of seal receptacle (1), and first servo motor (4) and seal receptacle (1) fixed connection, first reduction gear (3) is installed to the top of first servo motor (4), first servo motor (4) and swivel mount (2) all pass through shaft coupling and first reduction gear (3) fixed connection, the top of swivel mount (2) is provided with material frame (7), landing leg (5) are installed to the below of seal receptacle (1), and landing leg (5) and seal receptacle (1) fixed connection, pulley (6) are installed to the below of landing leg (5), and pulley (6) rotate with landing leg (5) and are connected, the below of pulley (6) is provided with the slide rail, and the pulley (6) is connected with the sliding rail in a rolling way.
2. The vacuum heat treatment apparatus for metal parts for aircraft seats according to claim 1, characterized in that: first horizontal pole (9) are installed to one side of pillar (8), and first horizontal pole (9) and pillar (8) welded connection, second horizontal pole (10) are installed to the top of pillar (8), and second horizontal pole (10) and pillar (8) welded connection, first screw rod (11) and second screw rod (19) are installed respectively to the top of first horizontal pole (9), and just first screw rod (11) and second screw rod (19) all rotate with first horizontal pole (9) and be connected, first screw rod (11) and second screw rod (19) all rotate with second horizontal pole (10) and are connected, the below of seal receptacle (1) is provided with layer board (12), first screw rod (11) and second screw rod (19) all with layer board (12) threaded connection.
3. The vacuum heat treatment apparatus for metal parts for aircraft seats according to claim 2, characterized in that: second servo motor (13) is installed to the top of pillar (8), and second servo motor (13) and pillar (8) fixed connection, second reduction gear (14) are installed to the below of second servo motor (13), first screw rod (11) and second servo motor (13) all are through shaft coupling and second reduction gear (14) fixed connection, drive gear (15) are installed in the outside of first screw rod (11), and drive gear (15) and first screw rod (11) fixed connection, the top of second horizontal pole (10) is provided with transmission shaft (17), driven gear (18) are installed in the outside of second screw rod (19), and driven gear (18) and second screw rod (19) fixed connection.
4. The vacuum heat treatment apparatus for metal parts for aircraft seats according to claim 3, characterized in that: first transmission gear (16) is installed to the one end of transmission shaft (17), second transmission gear (28) are installed to the one end in addition of transmission shaft (17), first transmission gear (16) and second transmission gear (28) all with transmission shaft (17) fixed connection, first transmission gear (16) and drive gear (15) interlock are connected, second transmission gear (28) and driven gear (18) interlock are connected.
5. The vacuum heat treatment apparatus for metal parts for aircraft seats according to claim 3, characterized in that: vacuum heat treatment furnace (20) is installed to the top of second horizontal pole (10), and vacuum heat treatment furnace (20) and second horizontal pole (10) fixed connection, the top of vacuum heat treatment furnace (20) is provided with exhaust tube (21), and exhaust tube (21) and vacuum heat treatment furnace (20) set up structure as an organic whole, the internally mounted of vacuum heat treatment furnace (20) has electric heating board (26), and electric heating board (26) and vacuum heat treatment furnace (20) fixed connection.
6. The vacuum heat treatment apparatus for metal parts for aircraft seats according to claim 5, characterized in that: air supply pipe (22) are installed to the top of exhaust tube (21), and air supply pipe (22) and exhaust tube (21) pass through flange fixed connection, valve (23) are installed in the outside of air supply pipe (22), and valve (23) and air supply pipe (22) fixed connection, air supply pipe (22) are kept away from the one end of exhaust tube (21) and are installed vacuum pump (24), and vacuum pump (24) and air supply pipe (22) pass through flange fixed connection, the top of vacuum pump (24) is provided with filter tube (25), and filter tube (25) and vacuum pump (24) set up structure as an organic whole, the internally mounted of filter tube (25) has filter pulp (27), and filter pulp (27) and filter tube (25) fixed connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022347659.8U CN214655113U (en) | 2020-10-21 | 2020-10-21 | Vacuum heat treatment device for metal parts for aviation seat |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022347659.8U CN214655113U (en) | 2020-10-21 | 2020-10-21 | Vacuum heat treatment device for metal parts for aviation seat |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214655113U true CN214655113U (en) | 2021-11-09 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022347659.8U Active CN214655113U (en) | 2020-10-21 | 2020-10-21 | Vacuum heat treatment device for metal parts for aviation seat |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214655113U (en) |
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- 2020-10-21 CN CN202022347659.8U patent/CN214655113U/en active Active
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