CN215356264U - Radial drilling machine for aerospace mold preparation - Google Patents
Radial drilling machine for aerospace mold preparation Download PDFInfo
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- CN215356264U CN215356264U CN202022305323.5U CN202022305323U CN215356264U CN 215356264 U CN215356264 U CN 215356264U CN 202022305323 U CN202022305323 U CN 202022305323U CN 215356264 U CN215356264 U CN 215356264U
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Abstract
The utility model relates to the field of drilling machines, and discloses a radial drilling machine for aerospace mold preparation, which comprises a workbench, wherein a fixed plate is arranged on the left side of the top of the workbench, a lifting plate is arranged on the top of the fixed plate, an electric push rod is fixedly connected to the right end of the lifting plate, and a movable plate is fixedly connected to the right end of the electric push rod. This radial drill is used in space mould preparation, the space mould that needs drilling is placed on the fixing base, then the upset cutting ferrule, the cutting ferrule can overlap on the space mould, then consolidate the position of cutting ferrule through reinforcing bolt, make the space mould fixed, fixing base can be rotated as required, treat that fixing base and space mould are rotated behind the suitable position, screw in fixing bolt again, can fix the space mould position after the regulation, and then can reprocess, the process of air mould refastening has been reduced, make the porous processing of air mould more high-efficient and convenient.
Description
Technical Field
The utility model relates to the field of drilling machines, in particular to a radial drilling machine for aerospace mold preparation.
Background
Aviation refers to the navigation activity of an aircraft in the earth's atmosphere, and aerospace refers to the navigation activity of an aircraft in the space outside the atmosphere. The aerospace greatly changes the structure of transportation, and through the rapid development of the recent hundred years, the aerospace becomes the most active and influential scientific and technical field in the 21 st century, and the significant achievement obtained in the field marks the high development of human civilization and also represents the advanced level of the national science and technology.
In the aerospace activity, drilling machines are required to be used for drilling aircraft accessories or aerospace molds, a plurality of holes may be required to be drilled on some components, and when the existing radial drilling machine is used, the machining efficiency of the components needing to be drilled is low. Therefore, the radial drilling machine for aerospace mold preparation is designed.
SUMMERY OF THE UTILITY MODEL
Aiming at the defects of the prior art, the utility model provides a radial drilling machine for manufacturing an aerospace mold, which solves the problems that a plurality of holes may need to be drilled on some aerospace molds, and the existing radial drilling machine is low in machining efficiency aiming at the aerospace mold needing to be drilled with the plurality of holes when in use.
In order to achieve the purpose, the utility model adopts the technical scheme that:
radial drill is used in space mould preparation, comprises a workbench, the fixed plate is installed in the left side at workstation top, the lifter plate is installed at the top of fixed plate, the right-hand member fixedly connected with electric putter of lifter plate, electric putter's right-hand member fixedly connected with movable plate, the right-hand member fixedly connected with drilling motor of movable plate, the output shaft fixedly connected with drill bit of drilling motor.
The drill bit drilling machine is characterized in that a fixing seat right facing a drill bit is rotatably connected to the top of the workbench, the left end and the right end of the fixing seat are connected with the top of the workbench through fixing bolts, a clamping sleeve is hinged to the top of the fixing seat, a positioning plate is fixedly connected to the left end of the clamping sleeve, and a reinforcing bolt connected with the top of the fixing seat is in threaded connection with the top of the positioning plate.
Furthermore, an adjusting motor is installed at the top of the fixing plate, an output shaft of the adjusting motor is fixedly connected with a threaded rod rotatably connected with the fixing plate, a moving sleeve is connected with the external thread of the threaded rod, and the right side wall of the moving sleeve is fixedly connected with the left end of the lifting plate.
Furthermore, the top of the movable sleeve is fixedly connected with a vertical spring which is sleeved outside the threaded rod, and the top of the vertical spring is fixedly connected with the inner wall of the fixed plate.
Furthermore, the top of lifter plate fixedly connected with is spacing pipe, the inside sliding connection of spacing pipe has the gag lever post, the right-hand member of gag lever post and the top fixed connection of movable plate.
Furthermore, the top of the workbench is provided with an annular groove corresponding to the fixed seat, the inside of the annular groove is connected with two moving blocks in a sliding manner, the top of each moving block is fixedly connected with the bottom of the fixed seat, the inner bottom wall of the annular groove is provided with a plurality of threaded grooves which are uniformly distributed, and the bottom end of the fixing bolt is connected in the threaded grooves in a threaded manner.
Furthermore, a discharge hole corresponding to the bottom of the fixed seat is formed in the top of the workbench.
The utility model has the beneficial effects that:
1. the utility model discloses a, the space mould that needs drilling places on the fixing base, then the upset cutting ferrule, the cutting ferrule can overlap on the space mould, then consolidate the position of cutting ferrule through reinforcing bolt, make the space mould fixed, as required can the rotating fixing base, treat that fixing base and space mould are rotated suitable position after, screw in fixing bolt again, can fix the space mould position after adjusting, and then can reprocess, the process of aviation mould refastening has been reduced, make the porous machining of aviation mould more high-efficient and convenient.
2. The utility model discloses a, start drilling motor, drilling motor can drive the drill bit and rotate, and then can carry out drilling processing to the aeronautical mold after fixing, can drive drilling motor and drill bit synchronous lifting in the time of the lifter plate lift, and then can effectual control drilling depth for it is more high-efficient and accurate in the drilling process.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a top view of the table of the present invention;
FIG. 3 is an enlarged view of A in FIG. 1;
fig. 4 is an enlarged view of B in fig. 1.
In the figure: 1. a work table; 2. a fixing plate; 3. a lifting plate; 4. an electric push rod; 5. moving the plate; 6. a drilling motor; 7. a drill bit; 8. a fixed seat; 9. fixing the bolt; 10. a card sleeve; 11. positioning a plate; 12. reinforcing the bolt; 13. adjusting the motor; 14. a threaded rod; 15. moving the sleeve; 16. a vertical spring; 17. a limiting pipe; 18. a limiting rod; 19. an annular groove; 20. a moving block; 21. a discharge port; 22. a thread groove.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, 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 some, but not all, embodiments of the present invention. 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 FIGS. 1-4: the radial drilling machine for preparing the aerospace mould comprises a workbench 1, wherein a fixed plate 2 is installed on the left side of the top of the workbench 1, a lifting plate 3 is installed on the top of the fixed plate 2, an electric push rod 4 is fixedly connected to the right end of the lifting plate 3, a movable plate 5 is fixedly connected to the right end of the electric push rod 4, a drilling motor 6 is fixedly connected to the right end of the movable plate 5, a drill bit 7 is fixedly connected to an output shaft of the drilling motor 6, the aerospace mould is fixed on the workbench 1, the position of the movable plate 5 can be adjusted through the electric push rod 4, the positions of the drilling motor 6 and the drill bit 7 can be adjusted, the drilling motor 6 is started, the drilling motor 6 can drive the drill bit 7 to rotate, further the fixed aerospace mould can be drilled, the drilling motor 6 and the drill bit 7 can be driven to synchronously lift when the lifting plate 3 lifts, and the drilling depth can be effectively controlled, the drilling process is more efficient and accurate.
The top of the workbench 1 is rotatably connected with a fixed seat 8 which is right opposite to the drill bit 7, the left end and the right end of the fixed seat 8 are both connected with the top of the workbench 1 through fixing bolts 9, the top of the fixed seat 8 is hinged with a cutting sleeve 10, the left end of the cutting sleeve 10 is fixedly connected with a positioning plate 11, the top of the positioning plate 11 is in threaded connection with a reinforcing bolt 12 which is connected with the top of the fixed seat 8, an aerospace mold needing drilling is placed on the fixed seat 8, then the cutting sleeve 10 is turned over, the cutting sleeve 10 can be sleeved on the aerospace mold, then the position of the cutting sleeve 10 is reinforced through the reinforcing bolt 12, so that the aerospace mold is fixed, then, the drilling motor 6 can drive the drill bit 7 to process the fixed mold, the fixed seat 8 can be rotated as required, after the fixed seat 8 and the aerospace mold are rotated to proper positions, the fixing bolt 9 is screwed in, so that the position of the adjusted aerospace mold can be fixed, and then can reprocess, reduced the process that the aviation mould was fixed again for the porous processing of aviation mould is more high-efficient and convenient.
The drilling motor 6 and the drill bit 7 can be driven to synchronously move when the lifting plate 3 moves, the adjusting motor 13 is installed at the top of the fixed plate 2, the output shaft of the adjusting motor 13 is fixedly connected with a threaded rod 14 which is rotatably connected with the fixed plate 2, the external thread of the threaded rod 14 is connected with a moving sleeve 15, the right side wall of the moving sleeve 15 is fixedly connected with the left end of the lifting plate 3, the top of the moving sleeve 15 is fixedly connected with a vertical spring 16 which is sleeved outside the threaded rod 14, the top of the vertical spring 16 is fixedly connected with the inner wall of the fixed plate 2, the threaded rod 14 can be driven to rotate after the drilling motor 6 is electrified, when the threaded rod 14 rotates in the moving sleeve 15, due to the effect of the screw thread, the movable sleeve 15 can move up and down under the limit of the fixed plate 2, in this process, the length of the vertical spring 16 is changed as the moving sleeve 15 is moved, thereby making the drilling process more convenient.
The movable plate 5 can be driven to move when the electric push rod 4 stretches out and draws back, the positions of the movable plate 5 and the drilling motor 6 can be adjusted, the top fixedly connected with limiting pipe 17 of the lifting plate 3, the inner sliding connection of the limiting pipe 17 is provided with a limiting rod 18, the right end of the limiting rod 18 is fixedly connected with the top of the movable plate 5, the limiting rod 18 can be driven to move when the movable plate 5 moves, the limiting rod 18 can be limited by the limiting pipe 17 when moving, and the movable plate 5 can move more stably and stably.
Can adjust the position of fixing base 8 as required, the ring channel 19 that corresponds with fixing base 8 is seted up at the top of workstation 1, the inside sliding connection of ring channel 19 has two movable blocks 20, and the top of movable block 20 and the bottom fixed connection of fixing base 8, a plurality of evenly distributed's thread groove 22 has been seted up to the inner diapire of ring channel 19, fixing bolt 9's bottom threaded connection is in thread groove 22, the discharge gate 21 that corresponds with fixing base 8's bottom is seted up at workstation 1's top, the setting of ring channel 19, can make movable block 20 slide at its inside steadily, and then can adjust fixing base 8's position, and the setting of a plurality of thread grooves 22, can conveniently fix a position fixing bolt 9, and then can fix fixing base 8's position, can fix aviation mould's position.
In summary, when the aerospace mold drilling fixture is used, an aerospace mold to be drilled is placed on the fixing seat 8, then the cutting sleeve 10 is turned over, the cutting sleeve 10 can be sleeved on the aerospace mold, then the position of the cutting sleeve 10 is reinforced through the reinforcing bolt 12, so that the aerospace mold is fixed, the drilling motor 6 is started, the drilling motor 6 can drive the drill bit 7 to rotate, and further the fixed aerospace mold can be drilled.
The above examples are only intended to illustrate the technical solution of the present invention, but not to limit it; although the present invention has been described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some technical features may be equivalently replaced; and such modifications or substitutions do not depart from the spirit and scope of the corresponding technical solutions of the embodiments of the present invention.
Claims (6)
1. Radial drill is used in aerospace mould preparation, including workstation (1), its characterized in that: a fixed plate (2) is mounted on the left side of the top of the workbench (1), a lifting plate (3) is mounted on the top of the fixed plate (2), an electric push rod (4) is fixedly connected to the right end of the lifting plate (3), a movable plate (5) is fixedly connected to the right end of the electric push rod (4), a drilling motor (6) is fixedly connected to the right end of the movable plate (5), and a drill bit (7) is fixedly connected to an output shaft of the drilling motor (6);
the drill bit fixing device is characterized in that a fixing seat (8) opposite to the drill bit (7) is connected to the top of the workbench (1) in a rotating mode, the left end and the right end of the fixing seat (8) are connected with the top of the workbench (1) through fixing bolts (9), a clamping sleeve (10) is hinged to the top of the fixing seat (8), a positioning plate (11) is fixedly connected to the left end of the clamping sleeve (10), and a reinforcing bolt (12) connected with the top of the fixing seat (8) is connected to the top of the positioning plate (11) in a threaded mode.
2. The radial drill press for aerospace mold preparation as claimed in claim 1, wherein: adjusting motor (13) is installed at the top of fixed plate (2), the output shaft fixedly connected with of adjusting motor (13) rotates threaded rod (14) of being connected with fixed plate (2), the outside threaded connection of threaded rod (14) has removal cover (15), the right side wall of removal cover (15) and the left end fixed connection of lifter plate (3).
3. The radial drilling machine for preparing the aerospace mold as claimed in claim 2, wherein: the top of the movable sleeve (15) is fixedly connected with a vertical spring (16) sleeved outside the threaded rod (14), and the top of the vertical spring (16) is fixedly connected with the inner wall of the fixed plate (2).
4. The radial drill press for aerospace mold preparation as claimed in claim 1, wherein: the top fixedly connected with spacing pipe (17) of lifter plate (3), the inside sliding connection of spacing pipe (17) has gag lever post (18), the right-hand member of gag lever post (18) and the top fixed connection of movable plate (5).
5. The radial drill press for aerospace mold preparation as claimed in claim 1, wherein: the top of the workbench (1) is provided with an annular groove (19) corresponding to the fixed seat (8), the inner part of the annular groove (19) is connected with two moving blocks (20) in a sliding mode, the top of each moving block (20) is fixedly connected with the bottom of the fixed seat (8), the inner bottom wall of the annular groove (19) is provided with a plurality of uniformly distributed thread grooves (22), and the bottom end of each fixing bolt (9) is connected in each thread groove (22) in a threaded mode.
6. The radial drill press for aerospace mold preparation as claimed in claim 1, wherein: the top of the workbench (1) is provided with a discharge hole (21) corresponding to the bottom of the fixed seat (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022305323.5U CN215356264U (en) | 2020-10-15 | 2020-10-15 | Radial drilling machine for aerospace mold preparation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022305323.5U CN215356264U (en) | 2020-10-15 | 2020-10-15 | Radial drilling machine for aerospace mold preparation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215356264U true CN215356264U (en) | 2021-12-31 |
Family
ID=79598953
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022305323.5U Active CN215356264U (en) | 2020-10-15 | 2020-10-15 | Radial drilling machine for aerospace mold preparation |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215356264U (en) |
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2020
- 2020-10-15 CN CN202022305323.5U patent/CN215356264U/en active Active
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