CN211162215U - Aircraft engine compressor blade cutting machine - Google Patents
Aircraft engine compressor blade cutting machine Download PDFInfo
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- CN211162215U CN211162215U CN201921877189.7U CN201921877189U CN211162215U CN 211162215 U CN211162215 U CN 211162215U CN 201921877189 U CN201921877189 U CN 201921877189U CN 211162215 U CN211162215 U CN 211162215U
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Abstract
The utility model relates to an aircraft engine compressor blade cutting machine, which is provided with a frame, wherein two ends of the frame are provided with sliding brackets, a cross beam is arranged between the sliding brackets, two ends of the cross beam are fixedly connected with the sliding brackets, a movable plate is arranged on the cross beam, the sliding direction of the movable plate is vertical to the sliding direction of the sliding brackets, the movable plate is provided with a cutting head which is driven by a third motor and is arranged on the movable plate in a lifting way, a blade fixing mechanism which is used for fixing blades is arranged on the frame, the blade fixing mechanism comprises an installation support frame which is fixed on the frame, a plurality of base connecting pieces and, and each blade mounting base is provided with a sucker mounting hole, each vacuum sucker is fixed in the corresponding sucker mounting hole, one end of each base connecting piece is fixedly connected with the mounting support frame, and the other end of each base connecting piece is connected with the blade mounting base. The utility model discloses can adapt to the fixed and the cutting of the blade of unidimensional not, it is high-efficient convenient.
Description
Technical Field
The utility model relates to an aeroengine compressor blade cutting machine.
Background
With the development of national economy, the engine compressor is widely applied to various fields such as industrial production, military, scientific research and the like. In the engine compressor part, the blade is a special part, needs a large amount of parts, has a complex shape, high requirements and large processing difficulty, and is a part with multiple faults, so that the manpower, material resources and financial resources invested by various manufacturers are large, and the blade needs to be matched with special cutting equipment for processing. The common processing mode of current engine compressor blade in the processing trade of cutting edge is the punch press cutting, and this kind of processing mode at first needs the heating, and not only the mould is with high costs, and easy deformation moreover is very inconvenient.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing a structure is ingenious, and can effectively fix the blade and to the aeroengine compressor blade cutting machine of its cutting.
Realize the utility model discloses the technical scheme of purpose is: the utility model has a frame, two ends of the frame are provided with sliding supports which are driven by a first motor to slide horizontally and are arranged on the frame, a cross beam is arranged between the sliding supports, two ends of the cross beam are fixedly connected with the sliding supports, a movable plate which is driven by a second motor to slide and is arranged on the cross beam, the sliding direction of the movable plate is vertical to the sliding direction of the sliding supports, a cutting head which is driven by a third motor to lift and is arranged on the movable plate, a blade fixing mechanism which is used for fixing blades on the frame is arranged on the frame, the blade fixing mechanism comprises an installation supporting frame which is fixed on the frame, a plurality of base connecting pieces, a plurality of blade installation bases and a plurality of vacuum suckers which are controlled by a vacuum pump to suck air, each blade installation base is provided with a sucker installation hole, the other end of each base connecting piece is connected with the blade mounting base.
The rack is provided with a first slide rail, the sliding support is provided with a first slide block connected with the first slide rail in a sliding manner, the rack is also provided with a first rack, the first motor is fixedly arranged on the sliding support, the output end of the first motor is provided with a gear, and the sliding support is arranged on the rack in a sliding manner through the transmission fit of the gear on the first motor and the first rack and the sliding connection of the first slide block and the first slide rail;
the beam is provided with a second slide rail, the movable plate is fixedly provided with a second slide block connected with the second slide rail in a sliding manner, the second motor is fixed on the movable plate, the output end of the second motor is also provided with a gear, the beam is provided with a second rack, and the movable plate is arranged on the beam in a sliding manner through the transmission fit of the gear on the second motor and the second rack and the sliding fit of the second slide rail and the second slide block.
The side of above-mentioned movable plate is fixed to be equipped with the extension board that sets up perpendicularly with the movable plate, and the ascending and descending of extension board is equipped with the lifter plate, and the cutting head is fixed on the lifter plate, and the third motor is fixed on the extension board, the last fixed third slide rail that is equipped with of extension board, the last fixed third slider that is equipped with third slide rail sliding connection of lifter plate, the lifter plate sets up on the extension board through the drive of third motor and the sliding fit lift of third slider and third slide rail, fixed being equipped with supplementary slide rail on the lateral wall of crossbeam, fixed being equipped with on the extension board with supplementary slide rail sliding fit's supplementary slider.
A first hard limiting block used for limiting the sliding support is fixedly arranged on the rack, and a second hard limiting block used for limiting the moving plate is fixedly arranged on the cross beam.
The fixed spout that is equipped with in bottom of above-mentioned frame, the below of erection bracing frame is equipped with the hopper that is used for the splendid attire waste material, and the hopper slides and sets up in the spout, and the slip direction of hopper is parallel with the moving direction of movable plate.
The utility model discloses has positive effect: (1) the utility model discloses a horizontal slip sets up the sliding support in the frame, set up the crossbeam on the sliding support, it sets up the movable plate to slide on the crossbeam, it sets up the cutting head to go up and down on the movable plate, set up blade fixed frame in the frame, set blade fixed establishment to erection bracing frame, blade installation base and base connecting piece, vacuum chuck fixes in the sucking disc mounting hole on blade installation base, through vacuum pump control vacuum chuck and further fix the preforming on blade installation base with the mode that the blade passes through the negative pressure, thereby the effectual processing cost height among the prior art of having solved, and the yielding problem of blade, thereby the quality of blade processing has been guaranteed, and is practical convenient.
(2) The utility model discloses a set up first motor on sliding support, set up the second motor on the movable plate, through first motor and second motor go up the gear respectively with the transmission cooperation of first rack and second rack to and the sliding fit of first slider and first slide rail, the sliding fit of second slider and second slide rail comes the removal of control crossbeam and movable plate, thereby comes the cutting position of control cutting head, has better controllability.
(3) The utility model discloses a set up the extension board on the lateral wall of movable plate to go up and down to set up on the lifter plate through third motor control on the extension board, the movable plate with extend the sliding fit of board through the third slide rail on the crossbeam and third slider and the sliding fit of supplementary slide rail and supplementary slider, fix a position the cutting head, prevent that the cutting head from taking place shake and skew, it is high-efficient convenient in the cutting head.
(4) The utility model discloses a set up in the frame and be used for the spacing first hard stopper of sliding support to and the setting is used for carrying out the hard stopper of spacing second to the movable plate, comes to carry on spacingly, safe high-efficient to the removal of sliding support and movable plate.
(5) The utility model discloses a bottom in the frame sets up the spout to slide in the spout and set up the hopper and collect the leftover bits after the blade cutting, the effectual processing environment that has optimized, it is practical convenient.
Drawings
In order that the present invention may be more readily and clearly understood, the following detailed description of the present invention is given in conjunction with the accompanying drawings, in which
FIG. 1 is a schematic view of the overall structure of a blade cutting machine for a compressor of a medium-sized aircraft engine according to the present invention;
FIG. 2 is a schematic structural view of the connection between the middle frame and the blade fixing mechanism of the present invention;
fig. 3 is a schematic view of the overall structure of the middle cross beam of the present invention;
fig. 4 is a schematic structural view of the middle moving plate of the present invention;
FIG. 5 is a schematic view of the connection structure between the lifter plate and the cutting head of the present invention;
FIG. 6 is a schematic structural view of a blade fixing mechanism according to the present invention;
fig. 7 is a schematic view of the connection structure between the middle base connection member and the blade mounting base of the present invention.
Detailed Description
Referring to fig. 1 to 7, the utility model has a frame 1, two ends of the frame 1 are provided with sliding brackets 11 driven by a first motor 12 and horizontally slidably arranged on the frame 1, a cross beam 2 is arranged between the sliding brackets 11, two ends of the cross beam 2 are fixedly connected with the sliding brackets 11, a moving plate 25 driven by a second motor 26 and slidably arranged on the cross beam 2 is arranged on the cross beam 2, the sliding direction of the moving plate 25 is perpendicular to the sliding direction of the sliding brackets 11, a cutting head 3 driven by a third motor 31 and arranged on the moving plate 25 is arranged on the moving plate 25, a blade fixing mechanism 4 for fixing the blade is arranged on the frame 1, the blade fixing mechanism 4 comprises a mounting support 41 fixed on the frame 1, a plurality of base connecting pieces 42, a plurality of blade mounting bases 43, and a plurality of vacuum suction cups 44 controlled by a vacuum pump, the size of the blade mounting bases 43 can be changed and adjusted according to the size of the blade to be, the vacuum pump is fixedly arranged on the frame 1, each blade mounting base 43 is provided with a sucker mounting hole 45, each vacuum sucker 44 is fixed in the corresponding sucker mounting hole 45, one end of each base connecting piece 42 is fixedly connected with the mounting support frame 41, and the other end of each base connecting piece 42 is connected with the blade mounting base 43;
a first sliding rail 13 is arranged on the rack 1, a first sliding block 16 connected with the first sliding rail 13 in a sliding manner is arranged on the sliding support 11, a first rack 14 is also arranged on the rack 1, the first motor 12 is fixedly arranged on the sliding support 11, a gear is arranged at the output end of the first motor 12, and the sliding support 11 is arranged on the rack 1 in a sliding manner through the transmission fit of the gear on the first motor 12 and the first rack 14 and the sliding connection of the first sliding block 16 and the first sliding rail 13;
the cross beam 2 is provided with a second slide rail 21, the moving plate 25 is fixedly provided with a second slide block 24 connected with the second slide rail 21 in a sliding manner, the second motor 26 is fixed on the moving plate 25, the output end of the second motor 26 is also provided with a gear, the cross beam 2 is provided with a second rack 22, and the moving plate 25 is arranged on the cross beam 2 in a sliding manner through the transmission fit of the gear on the second motor 26 and the second rack 22 and the sliding fit of the second slide rail 21 and the second slide block 24;
an extension plate 32 which is perpendicular to the moving plate 25 is fixedly arranged on the side edge of the moving plate 25, a lifting plate 33 is arranged on the extension plate 32 in a lifting way, the cutting head 3 is fixed on the lifting plate 33, a third motor 31 is fixed on the extension plate 32, a third slide rail 35 is fixedly arranged on the extension plate 32, a third slide block 36 connected with the third slide rail 35 in a sliding manner is fixedly arranged on the lifting plate 33, the lifting plate 33 is arranged on the extension plate 32 in a lifting manner through the driving of a third motor 31 and the sliding fit of the third slide block 36 and the third slide rail 35, a screw is rotatably arranged on the extension plate 32, a lifting block is matched with the screw in a threaded manner, the lifting block is fixedly connected with the lifting plate 33, the output end of the third motor 31 is fixedly connected with the screw, an auxiliary slide rail 27 is fixedly arranged on the side wall of the cross beam 2, and an auxiliary slide block 34 in sliding fit with the auxiliary slide rail 27 is fixedly arranged on the extension plate 32;
a first hard limiting block 15 for limiting the sliding support 11 is fixedly arranged on the rack 1, and a second hard limiting block 23 for limiting the moving plate 25 is fixedly arranged on the cross beam 2;
the bottom of the rack 1 is fixedly provided with a sliding groove 17, a hopper 5 for containing waste materials is arranged below the mounting support frame 41, the hopper 5 is arranged in the sliding groove 17 in a sliding manner, and the sliding direction of the hopper 5 is parallel to the moving direction of the moving plate 25.
The utility model discloses a theory of operation: the utility model discloses well erection bracing frame 41 is installed in frame 1, base connector 42 is installed on erection bracing frame 41, blade installation base 43 is installed on base connector 42, the blade is installed on blade installation base 43, then install vacuum chuck 44, further put the blade on blade installation base 43, open the vacuum pump, breathe in the vacuum pump through control button, the air in the sucking disc is siphoned away like this, effect through the negative pressure, vacuum chuck 44 adsorbs the blade and fixes, then cutting head 3 cuts, the cutting finishes the back, close the vacuum pump, open through control button and breathe in the solenoid valve and make gas get into the sucking disc and form the malleation, the blade is under the effect of vacuum chuck 44 malleation this moment, just get off very easily, accomplish the unloading, get into next duty cycle.
The above-mentioned embodiments, further detailed description of the objects, technical solutions and advantages of the present invention, it should be understood that the above-mentioned embodiments are only specific embodiments of the present invention, and are not intended to limit the present invention, and any modifications, equivalent substitutions, improvements, etc. made within the spirit and principle of the present invention should be included in the scope of the present invention.
Claims (5)
1. The utility model provides an aeroengine compressor blade cutting machine, has frame (1), its characterized in that: the blade fixing mechanism is characterized in that sliding supports (11) driven by a first motor (12) to horizontally slide and arranged on the rack (1) are arranged at two ends of the rack (1), cross beams (2) are arranged between the sliding supports (11), two ends of each cross beam (2) are fixedly connected with the sliding supports (11), a moving plate (25) driven by a second motor (26) to slide and arranged on each cross beam (2) is arranged on each cross beam (2), the sliding direction of each moving plate (25) is perpendicular to the sliding direction of each sliding support (11), a cutting head (3) driven by a third motor (31) to ascend and descend and arranged on each moving plate (25) is arranged on each moving plate (25), a blade fixing mechanism (4) used for fixing blades is arranged on the rack (1), and each blade fixing mechanism (4) comprises a mounting support frame (41), a plurality of base connecting pieces (42) and a plurality of blade mounting bases (43) fixed on the rack, and a plurality of vacuum chucks (44) which are controlled by a vacuum pump to suck air, wherein each blade mounting base (43) is provided with a chuck mounting hole (45), each vacuum chuck (44) is fixed in the corresponding chuck mounting hole (45), one end of each base connecting piece (42) is fixedly connected with the mounting support frame (41), and the other end of each base connecting piece (42) is connected with the blade mounting base (43).
2. The aircraft engine compressor blade cutting machine according to claim 1, characterized in that: the rack (1) is provided with a first sliding rail (13), the sliding support (11) is provided with a first sliding block (16) connected with the first sliding rail (13) in a sliding manner, the rack (1) is also provided with a first rack (14), the first motor (12) is fixedly arranged on the sliding support (11), the output end of the first motor (12) is provided with a gear, and the sliding support (11) is arranged on the rack (1) in a sliding manner through the transmission fit of the gear on the first motor (12) and the first rack (14) and the sliding connection of the first sliding block (16) and the first sliding rail (13);
be equipped with second slide rail (21) on crossbeam (2), fixed being equipped with on movable plate (25) with second slide rail (21) sliding connection's second slider (24), second motor (26) are fixed on movable plate (25), the output of second motor (26) also is equipped with the gear, be equipped with second rack (22) on crossbeam (2), movable plate (25) slide the setting on crossbeam (2) through the gear on second motor (26) and the transmission cooperation of second rack (22) and the sliding fit of second slide rail (21) and second slider (24).
3. The aircraft engine compressor blade cutting machine according to claim 2, characterized in that: the side of movable plate (25) is fixed to be equipped with extension board (32) with movable plate (25) perpendicular setting, and extension board (32) rising and falling is equipped with lifter plate (33), and cutting head (3) are fixed on lifter plate (33), and third motor (31) are fixed on extension board (32), extension board (32) are gone up and are fixed to be equipped with third slide rail (35), and lifter plate (33) are gone up and are fixed to be equipped with third slider (36) with third slide rail (35) sliding connection, and lifter plate (33) go up and down to set up on extension board (32) through the drive of third motor (31) and the sliding fit of third slider (36) and third slide rail (35), fixed being equipped with on the lateral wall of crossbeam (2) auxiliary slide rail (27), extension board (32) are gone up and are fixed to be equipped with auxiliary slide rail (34) with auxiliary slide rail (27) sliding fit.
4. The aircraft engine compressor blade cutting machine according to claim 3, characterized in that: a first hard limiting block (15) used for limiting the sliding support (11) is fixedly arranged on the rack (1), and a second hard limiting block (23) used for limiting the moving plate (25) is fixedly arranged on the cross beam (2).
5. The aircraft engine compressor blade cutting machine according to claim 1, characterized in that: the bottom of frame (1) is fixed and is equipped with spout (17), and the below of erection bracing frame (41) is equipped with hopper (5) that are used for the splendid attire waste material, and hopper (5) slide to be set up in spout (17), and the slip direction of hopper (5) is parallel with the moving direction of movable plate (25).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921877189.7U CN211162215U (en) | 2019-11-04 | 2019-11-04 | Aircraft engine compressor blade cutting machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921877189.7U CN211162215U (en) | 2019-11-04 | 2019-11-04 | Aircraft engine compressor blade cutting machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211162215U true CN211162215U (en) | 2020-08-04 |
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ID=71822808
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921877189.7U Active CN211162215U (en) | 2019-11-04 | 2019-11-04 | Aircraft engine compressor blade cutting machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211162215U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112775568A (en) * | 2020-12-29 | 2021-05-11 | 苏州达翔新材料有限公司 | Die cutting material-saving device and process thereof |
-
2019
- 2019-11-04 CN CN201921877189.7U patent/CN211162215U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112775568A (en) * | 2020-12-29 | 2021-05-11 | 苏州达翔新材料有限公司 | Die cutting material-saving device and process thereof |
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