CN211364997U - Edge cutting device for airplane horizontal tail machining - Google Patents

Edge cutting device for airplane horizontal tail machining Download PDF

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Publication number
CN211364997U
CN211364997U CN202021383900.6U CN202021383900U CN211364997U CN 211364997 U CN211364997 U CN 211364997U CN 202021383900 U CN202021383900 U CN 202021383900U CN 211364997 U CN211364997 U CN 211364997U
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plate
fixedly connected
horizontal tail
moving
motor
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CN202021383900.6U
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Chinese (zh)
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曹海伟
李大巍
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Tianjin Feiyue Intelligent Equipment Co ltd
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Tianjin Feiyue Intelligent Equipment Co ltd
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Abstract

The utility model relates to an aircraft is side cut device for horizontal tail processing, comprising a base plate, the rigid coupling has the brace table of placing the horizontal tail of waiting to process in the middle of the bottom plate top, be equipped with fixedly on the bottom plate the fixed establishment of horizontal tail, brace table one side the bottom plate top slides and is equipped with movable plate one, be equipped with cutting mechanism on the movable plate one, just be equipped with the drive on the movable plate one the power unit one that cutting mechanism removed, the brace table opposite side the bottom plate top slides and is equipped with movable plate two, be equipped with edging mechanism on the movable plate two, just be equipped with the drive on the movable plate two the power unit two that edging mechanism removed. The utility model discloses the horizontal tail is convenient for fix, and the cutting is polished conveniently, and labour saving and time saving improves work efficiency.

Description

Edge cutting device for airplane horizontal tail machining
Technical Field
The utility model relates to an aircraft accessory processing technology field especially relates to an aircraft horizontal tail processing is with side cut device.
Background
The horizontal tail is a short term for a horizontal tail, is one of the main parts of an airplane, and is generally horizontally installed on the tail.
The butt tail still needs to carry out the finish machining to it after rough machining produces, wherein, just need cut edge the processing to it, needs to cut and polish the side of butt tail, generally cuts it on cutting equipment earlier, cuts the back, takes out the butt tail, takes to polish it on polishing equipment again, and the course of working is loaded down with trivial details, wastes time and energy, and work efficiency is low.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the defects of the prior art and provides a trimming device for the horizontal tail processing of an airplane.
The utility model discloses a realize above-mentioned purpose, adopt following technical scheme: the utility model provides an aircraft horizontal tail processing is with side cut device, includes the bottom plate, its characterized in that, the rigid coupling has the brace table of placing the horizontal tail of treating processing in the middle of the bottom plate top, be equipped with fixedly on the bottom plate the fixed establishment of horizontal tail, brace table one side the bottom plate top slides and is equipped with movable plate one, be equipped with cutting mechanism on the movable plate one, just be equipped with the drive on the movable plate one the power unit one that cutting mechanism removed, the brace table opposite side the bottom plate top slides and is equipped with movable plate two, be equipped with edging mechanism on the movable plate two, just be equipped with the drive on the movable plate two the power unit two that edging mechanism.
Particularly, the fixing mechanism comprises a pressing plate and a pair of first electric cylinders, a supporting column is fixedly connected to the middle of the front end and the rear end of the top of the bottom plate in a vertical mode, a top plate is fixedly connected to the top of the supporting column in a horizontal mode, the first electric cylinders are fixedly connected to the two ends of the bottom of the top plate in a vertical mode, the pressing plate is fixedly connected to the bottom of a piston rod of the first electric cylinders in a horizontal mode, and the horizontal tail of the electric cylinder is.
Particularly, a rubber pad is fixedly connected to the opposite surface of the pressing plate and the supporting platform.
Particularly, shock pads are fixedly connected at four corners of the bottom plate.
Particularly, a first sliding block is fixedly connected to the front end and the rear end of the bottom of the first moving plate, a first sliding groove corresponding to the first sliding block is formed in the top of the bottom plate, the first sliding block is arranged in the first sliding groove in a sliding mode, the supporting column is close to one side of the first moving plate, a second electric cylinder is horizontally and fixedly connected to the top of the bottom plate, and the tail end of a piston rod of the second electric cylinder is fixedly connected with the first moving plate.
Particularly, a second sliding block is fixedly connected to the front end and the rear end of the bottom of the second moving plate, a second sliding groove corresponding to the second sliding block is formed in the top of the bottom plate, the second sliding block is arranged in the second sliding groove in a sliding mode, the supporting column is close to one side of the second moving plate, a third electric cylinder is horizontally and fixedly connected to the top of the bottom plate, and the tail end of a piston rod of the third electric cylinder is fixedly connected with the second moving plate.
Particularly, the cutting mechanism comprises a first motor and a cutting wheel, the first motor is arranged on the first movable plate in a sliding mode, the cutting wheel is fixedly connected to the output end of the first motor, the cutting wheel is located between the first movable plate and the supporting table, the cutting wheel is not in contact with the bottom plate, a third sliding block is fixedly connected to the bottom of the first motor, a third sliding groove corresponding to the third sliding block is formed in the top of the first movable plate, and the first motor is driven by the first power mechanism to enable the third sliding block to slide in the third sliding groove.
Particularly, the first power mechanism comprises a second motor, a first lead screw, a first moving block and a first baffle, the second motor is horizontally and fixedly connected to one end, far away from the first motor, of the top of the first moving plate, the first lead screw is horizontally and fixedly connected to the output end of the second motor, the first baffle is vertically and fixedly connected to one end, close to the first motor, of the top of the first moving plate, the first lead screw penetrates through the first moving block and then is rotatably connected to the first baffle, the first lead screw is in threaded connection with the first moving block, and the first moving block is slidably arranged at the top of the first moving plate.
Particularly, the power mechanism II comprises a motor III, a moving block II, a screw rod II and a baffle II, the motor III is horizontally and fixedly connected to one end of the top of the moving plate II, the screw rod II is horizontally and fixedly connected to the output end of the motor III, the baffle II is vertically and fixedly connected to one end, far away from the motor III, of the top of the moving plate II, the screw rod II penetrates through the moving block II and then is rotatably connected to the baffle II, the screw rod II is in threaded connection with the moving block II, and the moving block II is slidably arranged on the top of the moving plate II.
The edge grinding mechanism comprises a grinding block and a U-shaped grinding plate detachably mounted on the grinding block, the moving block II is close to one side of the supporting table, the supporting table is fixedly connected with the connecting rod, the grinding block is fixedly connected with the tail end of the connecting rod, one side of the supporting table is provided with a groove corresponding to the horizontal tail side edge, the grinding plate is inserted into the groove, the front side and the rear side of the grinding plate are fixedly connected with connecting plates, and the connecting plates are fixed on the grinding block through bolts.
The utility model has the advantages that: the utility model discloses a set up bottom plate, brace table, fixed establishment, movable plate one, movable plate two, cutting mechanism, grinding machanism, power unit one, power unit two for the horizontal tail is convenient for fix, and the setting of rubber pad, avoids the horizontal tail surface to receive the influence, and simultaneously, the horizontal tail cutting is polished conveniently, need not place the horizontal tail and process on a plurality of processing equipment, and labour saving and time saving improves work efficiency.
Drawings
Fig. 1 is a schematic structural view of the present invention;
fig. 2 is a schematic structural view of the fixing mechanism of the present invention;
FIG. 3 is a schematic structural view of the polishing mechanism of the present invention;
in the figure: 1-a bottom plate; 2, moving the first plate; 3, a first motor; 4-a cutting wheel; 5-electric cylinder two; 6-support column; 7-electric cylinder three; 8-baffle II; 9-moving the second plate; 10-a second chute; 11-moving block two; 12-a grinding block; 13-a second lead screw; 14-horizontal tail; 15-supporting table; 16-motor three; 17-motor two; 18-chute one; 19-a first lead screw; 20-chute III; 21-moving block one; 22-baffle one; 23-a platen; 24-a top plate; 25-a first slide block; 26-an electric cylinder I; 27-grinding the plate; 28-a connecting plate;
the following detailed description will be made in conjunction with embodiments of the present invention with reference to the accompanying drawings.
Detailed Description
The invention will be further explained with reference to the following figures and examples:
as shown in fig. 1-3, an edge cutting device is used in processing of aircraft horizontal tail, including bottom plate 1, its characterized in that, the rigid coupling has the brace table 15 of placing the horizontal tail 14 of treating processing in the middle of the 1 top of bottom plate, be equipped with fixedly on bottom plate 1 the fixed establishment of horizontal tail 14, brace table 15 one side the 1 top of bottom plate slides and is equipped with movable plate one 2, be equipped with cutting mechanism on the movable plate one 2, just be equipped with the drive on the movable plate one 2 the power unit one that cutting mechanism removed, brace table 15 opposite side the 1 top of bottom plate slides and is equipped with movable plate two 9, be equipped with edging mechanism on the movable plate two 9, just be equipped with the drive on the movable plate two 9 the power unit two that edging mechanism.
Particularly, the fixing mechanism comprises a pressing plate 23 and a pair of first electric cylinders 26, support columns 6 are vertically fixedly connected to the middle of the front end and the rear end of the top of the bottom plate 1, a top plate 24 is horizontally fixedly connected to the top of each support column 6, the first electric cylinders 26 are vertically fixedly connected to the two ends of the bottom of the top plate 24, the pressing plate 23 is horizontally fixedly connected to the bottom of a piston rod of the first electric cylinders 26, and the horizontal tail 14 is pressed and fixed through the pressing plate 23.
In particular, a rubber pad is fixed on the opposite surface of the pressing plate 23 and the supporting platform 15.
Particularly, shock pads are fixedly connected at four corners of the bottom plate 1.
Particularly, two ends rigid coupling have slider one 25 around the movable plate one 2 bottom, bottom plate 1 top be equipped with slider one 18 that 25 corresponds, slider one 25 slides and locates in the slider one 18, support column 6 is close to movable plate one 2 one side the horizontal rigid coupling in bottom plate 1 top has a pair of electric jar two 5, just the piston rod end of electric jar two 5 with movable plate one 2 rigid coupling.
Particularly, a second sliding block is fixedly connected to the front end and the rear end of the bottom of the second moving plate 9, a second sliding groove 10 corresponding to the second sliding block is formed in the top of the bottom plate 1, the second sliding block is arranged in the second sliding groove 10 in a sliding mode, the supporting column 6 is close to one side of the second moving plate 9, a third electric cylinder 7 is horizontally and fixedly connected to the top of the bottom plate 1, and the tail end of a piston rod of the third electric cylinder 7 is fixedly connected with the second moving plate 9.
Particularly, cutting mechanism includes motor 3, cutting wheel 4, motor 3 slides and locates on the movable plate 2, the vertical rigid coupling of cutting wheel 4 is in the output of motor 3, just cutting wheel 4 is located movable plate 2 with between the brace table 15, cutting wheel 4 with bottom plate 1 contactless, the rigid coupling of motor 3 bottom has slider three, 2 tops of movable plate be equipped with three spouts 20 that correspond of slider three, motor 3 pass through the drive of power unit and then make slider three slide in spout three 20.
Particularly, the first power mechanism comprises a second motor 17, a first lead screw 19, a first moving block 21 and a first baffle 22, the second motor 17 is horizontally and fixedly connected to one end, far away from the first motor 3, of the top of the first moving plate 2, the first lead screw 19 is horizontally and fixedly connected to the output end of the second motor 17, the first baffle 22 is vertically and fixedly connected to one end, close to the first motor 3, of the top of the first moving plate 2, the first lead screw 19 penetrates through the first moving block 21 and then is rotatably connected to the first baffle 22, the first lead screw 19 is in threaded connection with the first moving block 21, and the first moving block 21 is slidably arranged on the top of the first moving plate 2.
Particularly, the power mechanism two comprises a motor three 16, a moving block two 11, a lead screw two 13 and a baffle two 8, the motor three 16 is horizontally and fixedly connected to one end of the top of the moving plate two 9, the lead screw two 13 is horizontally and fixedly connected to the output end of the motor three 16, the baffle two 8 is vertically and fixedly connected to one end, far away from the motor three 16, of the top of the moving plate two 9, the lead screw two 13 penetrates through the moving block two 11 and then is rotatably connected to the baffle two 8, the lead screw two 13 is in threaded connection with the moving block two 11, and the moving block two 11 is slidably arranged on the top of the moving plate two 9.
Specially, edging mechanism includes sanding block 12, demountable installation the U-shaped board 27 of polishing on sanding block 12, two 11 moving blocks are close to supporting bench 15 one side rigid coupling has the connecting rod, sanding block 12 rigid coupling is in the connecting rod is terminal, sanding block 12 is close to supporting bench 15 one side be equipped with the recess that the horizontal tail 14 side corresponds, sanding block 27 inserts in the recess, just both sides rigid coupling has connecting plate 28 around sanding block 27, connecting plate 28 passes through the bolt fastening and is in on sanding block 12.
When the utility model works, the horizontal tail 14 to be processed is placed on the supporting table 15, the part to be cut is left, the first electric cylinder 26 is started, the pressing plate 23 moves downwards and presses and fixes the horizontal tail 14, the second electric cylinder 5 is started, the first movable plate 2 drives the cutting wheel 4 to move to a designated position, the first motor 3 and the second motor 17 are started, the cutting wheel 4 rotates and moves to start to cut the edge of the horizontal tail 14, after the cutting is finished, the horizontal tail 14 is turned over, the steps are repeated, the other side edge of the horizontal tail 14 is cut, meanwhile, the third electric cylinder 7 is started, the second moving plate 9 drives the polishing block 12 to move to a designated position, at the moment, the side edge of the horizontal tail 14 is inserted into the groove, the polishing plate 27 is in contact with the side edge of the horizontal tail 14, the third motor 16 is started, the polishing block 12 moves, the side edge of the horizontal tail 14 after cutting starts to be polished, and the steps are repeated on other side edges of the horizontal tail 14. The utility model discloses horizontal tail 14 is convenient for fixed, and the cutting is polished conveniently, and labour saving and time saving improves work efficiency.
The present invention has been described above with reference to the accompanying drawings, and it is obvious that the present invention is not limited by the above embodiments, and various improvements made by the method concept and technical solution of the present invention or directly applied to other occasions without improvement are all within the protection scope of the present invention.

Claims (10)

1. The utility model provides an aircraft horizontal tail processing is with side cut device, includes bottom plate (1), its characterized in that, the rigid coupling has in the middle of bottom plate (1) top to place a supporting bench (15) of waiting to process horizontal tail (14), be equipped with on bottom plate (1) and fix the fixed establishment of horizontal tail (14), supporting bench (15) one side bottom plate (1) top slides and is equipped with movable plate (2), be equipped with cutting mechanism on movable plate (2), just be equipped with the drive on movable plate (2) the power unit one that cutting mechanism removed, supporting bench (15) opposite side bottom plate (1) top slides and is equipped with movable plate two (9), be equipped with edging mechanism on movable plate two (9), just be equipped with the drive on movable plate two (9) the power unit two that edging mechanism removed.
2. The edge cutting device for processing the airplane horizontal tail according to claim 1, wherein the fixing mechanism comprises a pressing plate (23) and a pair of first electric cylinders (26), a supporting column (6) is vertically fixedly connected to the middle of the front end and the rear end of the top of the bottom plate (1), a top plate (24) is horizontally fixedly connected to the top of the supporting column (6), the first electric cylinders (26) are vertically fixedly connected to the two ends of the bottom of the top plate (24), the pressing plate (23) is horizontally fixedly connected to the bottom of a piston rod of the first electric cylinders (26), and the horizontal tail (14) is pressed and fixed through the pressing plate (23).
3. The trimming device for airplane horizontal tail processing according to claim 2, wherein rubber pads are fixedly connected to the opposite surfaces of the pressure plate (23) and the support platform (15).
4. The trimming device for processing the horizontal tail of the airplane as claimed in claim 3, wherein shock absorbing pads are fixedly connected to the four corners of the bottom of the base plate (1).
5. The edge cutting device for airplane horizontal tail machining according to claim 4, characterized in that a first sliding block (25) is fixedly connected to the front end and the rear end of the bottom of the first moving plate (2), a first sliding groove (18) corresponding to the first sliding block (25) is formed in the top of the bottom plate (1), the first sliding block (25) is slidably arranged in the first sliding groove (18), a pair of second electric cylinders (5) is horizontally and fixedly connected to the top of the bottom plate (1) on the side, close to the first moving plate (2), of the support column (6), and the tail ends of piston rods of the second electric cylinders (5) are fixedly connected with the first moving plate (2).
6. The edge cutting device for airplane horizontal tail machining according to claim 5, wherein a second sliding block is fixedly connected to the front end and the rear end of the bottom of the second moving plate (9), a second sliding groove (10) corresponding to the second sliding block is formed in the top of the bottom plate (1), the second sliding block is slidably arranged in the second sliding groove (10), a pair of third electric cylinders (7) is horizontally and fixedly connected to the top of the bottom plate (1) on one side, close to the second moving plate (9), of the support column (6), and the tail ends of piston rods of the third electric cylinders (7) are fixedly connected with the second moving plate (9).
7. The edge cutting device for processing the horizontal tail of the airplane according to claim 6, wherein the cutting mechanism comprises a first motor (3) and a first cutting wheel (4), the first motor (3) is slidably disposed on the first moving plate (2), the first cutting wheel (4) is vertically and fixedly connected to an output end of the first motor (3), the first cutting wheel (4) is located between the first moving plate (2) and the supporting table (15), the first cutting wheel (4) is not in contact with the bottom plate (1), a third sliding block is fixedly connected to the bottom of the first motor (3), a third sliding groove (20) corresponding to the third sliding block is formed in the top of the first moving plate (2), and the first motor (3) is driven by the first power mechanism to further enable the third sliding block to slide in the third sliding groove (20).
8. The trimming device for airplane horizontal tail machining according to claim 7, wherein the first power mechanism comprises a second motor (17), a first lead screw (19), a first moving block (21) and a first baffle plate (22), the second motor (17) is horizontally and fixedly connected to the top of the first moving plate (2) far away from one end of the first motor (3), the first lead screw (19) is horizontally and fixedly connected to the output end of the second motor (17), the first baffle plate (22) is vertically and fixedly connected to the top of the first moving plate (2) close to one end of the first motor (3), the first lead screw (19) penetrates through the first moving block (21) and then is rotatably connected to the first baffle plate (22), the first lead screw (19) is in threaded connection with the first moving block (21), and the first moving block (21) is slidably arranged on the top of the first moving plate (2).
9. The trimming device for aircraft horizontal tail machining according to claim 8, wherein the second power mechanism comprises a third motor (16), a second moving block (11), a second lead screw (13) and a second baffle (8), the third motor (16) is horizontally and fixedly connected to one end of the top of the second moving block (9), the second lead screw (13) is horizontally and fixedly connected to an output end of the third motor (16), the second baffle (8) is vertically and fixedly connected to one end, far away from the third motor (16), of the top of the second moving block (9), the second lead screw (13) penetrates through the second moving block (11) and then is rotatably connected to the second baffle (8), the second lead screw (13) is in threaded connection with the second moving block (11), and the second moving block (11) is slidably arranged on the top of the second moving block (9).
10. The edge cutting device for processing the horizontal tail of the airplane as claimed in claim 9, wherein the edge grinding mechanism comprises a grinding block (12) and a U-shaped grinding plate (27) detachably mounted on the grinding block (12), a connecting rod is fixedly connected to one side, close to the supporting table (15), of the moving block two (11), the grinding block (12) is fixedly connected to the tail end of the connecting rod, a groove corresponding to the side edge of the horizontal tail (14) is formed in one side, close to the supporting table (15), of the grinding block (12), the grinding plate (27) is inserted into the groove, connecting plates (28) are fixedly connected to the front side and the rear side of the grinding plate (27), and the connecting plates (28) are fixed to the grinding block (12) through bolts.
CN202021383900.6U 2020-07-15 2020-07-15 Edge cutting device for airplane horizontal tail machining Active CN211364997U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202021383900.6U CN211364997U (en) 2020-07-15 2020-07-15 Edge cutting device for airplane horizontal tail machining

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202021383900.6U CN211364997U (en) 2020-07-15 2020-07-15 Edge cutting device for airplane horizontal tail machining

Publications (1)

Publication Number Publication Date
CN211364997U true CN211364997U (en) 2020-08-28

Family

ID=72171831

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202021383900.6U Active CN211364997U (en) 2020-07-15 2020-07-15 Edge cutting device for airplane horizontal tail machining

Country Status (1)

Country Link
CN (1) CN211364997U (en)

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