CN115229032A - Aircraft wing rib trompil fluting device - Google Patents

Aircraft wing rib trompil fluting device Download PDF

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Publication number
CN115229032A
CN115229032A CN202211154352.3A CN202211154352A CN115229032A CN 115229032 A CN115229032 A CN 115229032A CN 202211154352 A CN202211154352 A CN 202211154352A CN 115229032 A CN115229032 A CN 115229032A
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CN
China
Prior art keywords
plate
face
limiting
machine tool
sliding
Prior art date
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Pending
Application number
CN202211154352.3A
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Chinese (zh)
Inventor
林玮
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Sheyang Xingkaifei Aviation Equipment Co ltd
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Sheyang Xingkaifei Aviation Equipment Co ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Sheyang Xingkaifei Aviation Equipment Co ltd filed Critical Sheyang Xingkaifei Aviation Equipment Co ltd
Priority to CN202211154352.3A priority Critical patent/CN115229032A/en
Publication of CN115229032A publication Critical patent/CN115229032A/en
Pending legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D28/00Shaping by press-cutting; Perforating
    • B21D28/24Perforating, i.e. punching holes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B08CLEANING
    • B08BCLEANING IN GENERAL; PREVENTION OF FOULING IN GENERAL
    • B08B15/00Preventing escape of dirt or fumes from the area where they are produced; Collecting or removing dirt or fumes from that area
    • B08B15/04Preventing escape of dirt or fumes from the area where they are produced; Collecting or removing dirt or fumes from that area from a small area, e.g. a tool
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D28/00Shaping by press-cutting; Perforating
    • B21D28/24Perforating, i.e. punching holes
    • B21D28/34Perforating tools; Die holders
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D37/00Tools as parts of machines covered by this subclass
    • B21D37/04Movable or exchangeable mountings for tools

Abstract

The invention provides an aircraft wing rib perforating and slotting device, which relates to the field of perforating and slotting equipment and comprises: a machine tool main body and a limiting part; the punching mechanism comprises a machine tool body, a motor, a linkage assembly and a rocking plate, wherein the machine tool body is provided with two T-shaped sliding grooves in a bilateral symmetry manner, the upper end of the machine tool body is connected with a lower die holder in a sliding manner through the two T-shaped sliding grooves, the waste materials in the storage bin can be more flat under the rocking action through the cooperation of the motor, the inner space of the storage bin can be fully utilized, the punching punch and the lower die holder are more convenient and quick to replace and disassemble through the arrangement of a limiting part, and the problem that the punching punch and the lower die holder on the existing punching and slotting device are poor in convenience during replacement is solved.

Description

Aircraft wing rib trompil fluting device
Technical Field
The invention relates to the technical field of hole opening and grooving equipment, in particular to a hole opening and grooving device for an airplane wing rib.
Background
In the production and processing process of the aircraft wing rib, the aircraft wing rib needs to be subjected to hole opening and grooving, and when the aircraft wing rib is subjected to hole opening and grooving, a hole opening and grooving device is generally used.
1. When the existing airplane wing rib perforating and slotting device conducts perforating and slotting operation on airplane wing ribs, although generated waste materials can be guided into a material box through a material guide pipe, the waste materials are easy to be piled into a convex shape after falling into the material box, so that the internal space of the material box cannot be fully utilized;
2. the drift and the die holder of punching on the trompil fluting device of present are when changing, because punch and die holder all carry out fixed connection through fasteners such as bolts to when changing punch and die holder, need tear fasteners such as a large amount of bolts down earlier through the instrument, thereby reduced the convenience of punch and die holder when changing.
Disclosure of Invention
In view of this, the invention provides an aircraft wing rib perforating and slotting device, which enables waste collected in a storage box to be smoother under the action of shaking through the cooperation of a power mechanism, a linkage assembly and a shaking plate, so that the internal space of the storage box can be fully utilized, and secondly, through the arrangement of a limiting part, when a perforating punch and a lower die holder are replaced and disassembled, a large number of fasteners such as bolts and the like are not required to be disassembled through tools, so that the aircraft wing rib perforating and slotting device is more convenient and rapid.
The invention provides a purpose and an effect of an airplane wing rib perforating and slotting device, which specifically comprise the following steps: a machine tool main body and a limiting part; the front side of the upper end face of the machine tool main body is provided with a power mechanism, the front side of the upper end face of the machine tool main body is provided with two T-shaped sliding grooves in a bilateral symmetry manner, the front side of the upper end face of the machine tool main body is connected with a lower die holder in a sliding manner through the two T-shaped sliding grooves, and the lower end of the power mechanism is provided with a punching punch through a connecting plate; the machine tool comprises a machine tool main body, a base, a rocking plate, a linkage assembly, a support plate, a storage box and a lifting mechanism, wherein the linkage assembly is arranged on the front side of the machine tool main body, the lower part of the front end surface of the machine tool main body is fixedly connected with the support plate, the upper end surface of the support plate is connected with the rocking plate in a sliding manner, and the storage box is arranged on the upper end surface of the rocking plate; the number of the limiting parts is two, and the two limiting parts are respectively arranged on the rear side of the power mechanism and the machine tool main body; the utility model discloses a lathe is equipped with the baffle box, lathe main part right-hand member face front side is opened and is equipped with the access hole, and lathe main part right-hand member face is located access hole department and rotates and be connected with the access door, is equipped with the passage on the lateral wall before the lathe main part, and lathe main part top face has seted up the circular port.
Furthermore, the power mechanism comprises a Contraband-shaped support plate, a hydraulic cylinder, a lifting plate, a driving rack and a rectangular support plate, the Contraband-shaped support plate is installed on the upper end face of the machine tool body, the hydraulic cylinder is installed at the top of the Contraband-shaped support plate, a telescopic rod of the hydraulic cylinder penetrates through the top of the Contraband-shaped support plate, the lower end of the telescopic rod of the hydraulic cylinder is fixedly connected with the lifting plate, and four corners of the upper end face of the lifting plate are fixedly connected with a vertical guide rod penetrating through the top of the Contraband-shaped support plate; the left side of the front end face of the lifting plate is fixedly connected with a driving rack, the rear end face of the lifting plate is fixedly connected with a rectangular support plate, a limiting part is installed on the rear end face of the rectangular support plate, and the bottom end face of the lifting plate is bilaterally symmetrical and provided with two T-shaped chutes.
Furthermore, punch and connecting plate fixed connection, and the connecting plate upper end is personally submitted bilateral symmetry and is described and be equipped with two T type sliders, the first plugboard of connecting plate rear end face middle part fixedly connected with, and rectangle socket has been seted up in the middle part of the first plugboard upper end face.
Furthermore, when the connecting plate is installed on the bottom end face of the lifting plate, the two T-shaped sliding blocks on the connecting plate are respectively in sliding connection with the two T-shaped sliding grooves on the bottom end face of the lifting plate, and the rear end of the first plug board penetrates through the rectangular support plate.
Furthermore, two T-shaped sliding blocks are symmetrically arranged on the left and right of the bottom end surface of the lower die holder, a second plug board is arranged in the middle of the rear end surface of the lower die holder, a rectangular socket is formed in the middle of the upper end surface of the second plug board, and a circular through hole is formed in the middle of the upper end surface of the lower die holder; when the lower die base is installed on the upper end face of the machine tool main body, the two T-shaped sliding blocks on the lower die base are respectively in sliding connection with the two T-shaped sliding grooves on the machine tool main body.
Furthermore, the linkage assembly comprises a linkage shaft, a transverse rotating shaft, a vertical rotating shaft, a circular turntable and a driving column, the linkage shaft is rotatably connected to the front side of the top of the Contraband-shaped support plate, a first belt wheel and a linkage gear are respectively arranged at the front end and the rear end of the linkage shaft, and the linkage gear is meshed with the driving rack; the transverse rotating shaft and the vertical rotating shaft are rotatably connected to the front end face of the machine tool main body, a first bevel gear is mounted at the front end of the transverse rotating shaft, a second belt wheel is mounted on the rear side outside the transverse rotating shaft, and the second belt wheel is in transmission connection with the first belt wheel through a belt; the upper end of the vertical rotating shaft is provided with a second bevel gear meshed with the first bevel gear, the lower end of the vertical rotating shaft is provided with a circular turntable, and the edge of the bottom end face of the circular turntable is provided with a driving column.
Furthermore, two sliding cylinders are arranged on the bottom end face of the shaking plate, a supporting sliding rod is connected inside each sliding cylinder in a sliding mode, the two supporting sliding rods are fixedly connected to the upper end face of the supporting plate, a T-shaped belt moving plate is fixedly connected to the middle of the left side of the shaking plate, a strip-shaped sliding opening is formed in the left side of the upper end face of the T-shaped belt moving plate, and the strip-shaped sliding opening in the T-shaped belt moving plate is connected with the driving column in a sliding mode; four rectangular bayonets and four circular jacks are formed in the upper end face of the shaking plate.
Furthermore, the bottom end face of the containing bin is fixedly connected with a mounting plate, two rectangular through holes are formed in the left side and the right side of the bottom end face of the mounting plate, an elastic buckle is connected inside each rectangular through hole in a sliding mode, a spring is installed inside each rectangular through hole, and the four elastic buckles are clamped with the four rectangular clamping openings respectively; the upper end of each elastic buckle is fixedly connected with an L-shaped belt moving rod, and each L-shaped belt moving rod is provided with a trapezoidal block; four vertical slide bars of equal fixedly connected with in the mounting panel up end left and right sides, and per four vertical slide bar outside equal sliding connection have a sliding plate, a lifting rod of sliding plate up end middle part fixedly connected with, and lifting rod upper end is equipped with the handle, and mounting panel bottom face is equipped with four spacing inserted bars, and four spacing inserted bars respectively with rock four circular jacks grafting on the plate.
Furthermore, the limiting part comprises a limiting shell, a limiting slide block, a pulling rod and a limiting plate, the limiting shell is installed on the upper end face of the installation plate, the limiting slide block is connected to the inside of the limiting shell in a sliding mode, the upper end of the limiting slide block is fixedly connected with the pulling rod penetrating through the top of the limiting shell, the upper end of the pulling rod is connected with a handle in a rotating mode, and a spring is sleeved on the outer portion of the pulling rod, located inside the limiting shell; the upper end surface of the limiting shell is symmetrically provided with two limiting plates, and the upper ends of the two limiting plates are provided with gaps; the lower end of the limiting sliding block is provided with a plug board penetrating through the bottom of the limiting shell.
Furthermore, when the two limiting parts are in a limiting state, the plug board in one limiting part at the upper part is plugged with the rectangular socket on the first plug board, and the plug board in one limiting part at the lower part is plugged with the rectangular socket on the second plug board.
Advantageous effects
1. According to the invention, through the matching of the power mechanism, the linkage assembly and the rocking plate, the lifting plate can drive the driving rack to move up and down when moving up and down, so that the linkage gear, the linkage shaft, the first belt wheel, the second belt wheel, the transverse rotating shaft, the first bevel gear, the second bevel gear, the vertical rotating shaft and the circular rotating disc are driven to rotate, then the circular rotating disc drives the driving post to rotate, and then the T-shaped driving plate is driven by the driving post to move left and right in a reciprocating manner, so that the rocking plate drives the containing box to move left and right in a reciprocating manner, so that waste materials collected in the containing box can be smoother under the rocking action, the inner space of the containing box can be fully utilized, the structure is simple, additional driving devices such as a motor are not required to be arranged for driving, and the cost and the loss of electric energy are saved.
2. According to the invention, through the arrangement of the limiting parts, when the punching punch and the lower die holder need to be replaced, the handles in the two limiting parts are pulled towards the tail end, so that the pulling rod drives the limiting slide block and the inserting plate to move towards the tail end, the head ends of the two inserting plates are respectively pulled out from the rectangular inserting opening on the first inserting plate and the rectangular inserting opening on the second inserting plate, and then the punching punch and the lower die holder are inserted in a forward sliding manner.
3. According to the invention, through the matching of the elastic buckles, the L-shaped driving rods, the sliding plates, the lifting rods and the trapezoidal blocks, when the storage bin is taken down from the shaking plate, the lifting handles at the upper ends of the two lifting rods are lifted upwards by two hands, so that the sliding plates move upwards, and then under the action of the inclined planes of the two adjacent trapezoidal blocks, the two adjacent L-shaped driving rods are forced to move towards the opposite directions, so that the two adjacent elastic buckles move towards the opposite directions, and the two adjacent elastic buckles and the two adjacent rectangular bayonets lose the clamping relation, so that the storage bin can be easily taken down from the shaking plate without other complicated operations, and the convenience of the storage bin in waste material cleaning is greatly improved.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings of the embodiments will be briefly described below.
The drawings in the following description relate to some embodiments of the invention only and are not intended to limit the invention.
In the drawings:
FIG. 1 is a first perspective structural view of an aircraft rib aperture grooving apparatus according to an embodiment of the present invention;
FIG. 2 is a schematic structural diagram of a second perspective view of an aircraft rib opening and grooving device according to an embodiment of the invention;
FIG. 3 is a schematic structural view of an aircraft rib hole opening and grooving device according to an embodiment of the invention in a disassembled state;
FIG. 4 is a schematic diagram of the power mechanism and the punching punch of the aircraft rib hole-forming and slotting device according to the embodiment of the invention;
FIG. 5 is a schematic structural diagram of a lifting plate and a connecting plate of the aircraft rib hole opening and slotting device of the embodiment of the invention after being disassembled;
FIG. 6 is a schematic view, partly in section, of the machine tool body of the aircraft rib tapping device according to an embodiment of the invention;
FIG. 7 is a schematic structural view of a linkage assembly and a wobble plate of an aircraft rib opening notching device according to an embodiment of the present invention;
FIG. 8 is an enlarged partial schematic view of a section A in FIG. 1 of an aircraft rib hole opening and slotting device according to an embodiment of the invention;
FIG. 9 is a schematic structural diagram of the aircraft rib hole-opening slotting device with the vertical rotating shaft and the rocking plate detached according to the embodiment of the invention;
FIG. 10 is a schematic view of a storage bin configuration of an aircraft rib aperturing and slotting device of an embodiment of the present invention;
FIG. 11 is a schematic structural view of an aircraft rib tapping and grooving device according to an embodiment of the invention after the mounting plate and the elastic buckle are separated;
FIG. 12 is a schematic structural view of the aircraft rib tapping and grooving apparatus with the vertical sliding rod and the sliding plate separated according to the embodiment of the present invention;
fig. 13 is a schematic structural diagram of the aircraft rib hole-opening slotting device according to the embodiment of the invention after the limiting part is disassembled.
List of reference numerals
1. A machine tool main body; 101. an access hole; 102. an access door; 103. a material guide pipe; 104. a circular hole; 2. a power mechanism; 201. 5363 a Contraband-shaped plate; 202. a hydraulic cylinder; 203. a lifting plate; 204. a drive rack; 205. a rectangular support plate; 3. punching a punch; 301. a connecting plate; 302. a first patch panel; 4. a lower die holder; 401. a second patch panel; 402. a circular through hole; 5. a linkage assembly; 501. a linkage shaft; 502. a transverse rotating shaft; 503. a vertical rotating shaft; 504. a circular turntable; 505. driving the column; 6. a support plate; 7. shaking the plate; 701. a T-shaped driving plate; 702. a sliding cylinder; 703. a rectangular bayonet; 8. a storage bin; 801. mounting a plate; 802. a rectangular through opening; 803. an elastic buckle; 804. an L-shaped driving rod; 805. a vertical slide bar; 806. a sliding plate; 807. lifting a pull rod; 808. a trapezoidal block; 9. a limiting part; 901. a limiting shell; 902. a limiting slide block; 903. pulling a rod; 904. and a limiting plate.
Detailed Description
In order to make the objects, aspects and advantages of the embodiments of the present invention more apparent, the embodiments of the present invention will be described in detail with reference to the accompanying drawings. Unless otherwise indicated, terms used herein have the ordinary meaning in the art. Like reference symbols in the various drawings indicate like elements.
Example (b): please refer to fig. 1 to fig. 13:
the invention provides an aircraft wing rib perforating and slotting device, which comprises a machine tool main body 1 and a limiting part 9; a power mechanism 2 is installed on the front side of the upper end face of the machine tool body 1, the power mechanism 2 comprises a Contraband-shaped support plate 201, a hydraulic cylinder 202, a lifting plate 203, a driving rack 204 and a rectangular support plate 205, the Contraband-shaped support plate 201 is installed on the upper end face of the machine tool body 1, the hydraulic cylinder 202 is installed on the top of the Contraband-shaped support plate 201, a telescopic rod of the hydraulic cylinder 202 penetrates through the top of the Contraband-shaped support plate 201, the lower end of the telescopic rod of the hydraulic cylinder 202 is fixedly connected with the lifting plate 203, and four corners of the upper end face of the lifting plate 203 are fixedly connected with a vertical guide rod penetrating through the top of the Contraband-shaped support plate 201; a driving rack 204 is fixedly connected to the left side of the front end face of the lifting plate 203, a rectangular support plate 205 is fixedly connected to the rear end face of the lifting plate 203, a limiting part 9 is mounted on the rear end face of the rectangular support plate 205, two T-shaped sliding grooves are symmetrically formed in the left and right of the bottom end face of the lifting plate 203, and the power mechanism 2 is arranged to provide downward impact force for the punching punch 3;
the front side of the upper end face of the machine tool main body 1 is provided with two T-shaped sliding grooves in a bilateral symmetry manner, the front side of the upper end face of the machine tool main body 1 is connected with a lower die holder 4 in a sliding manner through the two T-shaped sliding grooves, and the lower end of the power mechanism 2 is provided with a punching punch 3 through a connecting plate 301; the punching punch 3 is fixedly connected with the connecting plate 301, two T-shaped sliding blocks are symmetrically arranged on the upper end surface of the connecting plate 301 in a bilateral mode, the middle of the rear end surface of the connecting plate 301 is fixedly connected with a first inserting plate 302, a rectangular inserting opening is formed in the middle of the upper end surface of the first inserting plate 302, the punching punch 3 is used for punching the airplane wing rib, and when the airplane wing rib needs to be grooved, the corresponding grooving punch only needs to be replaced to the bottom of the lifting plate 203;
when the connecting plate 301 is mounted to the bottom end face of the lifting plate 203, the two T-shaped sliders on the connecting plate 301 are respectively in sliding connection with the two T-shaped chutes on the bottom end face of the lifting plate 203, and the rear end of the first plug-in plate 302 penetrates through the rectangular support plate 205;
the front side of a machine tool main body 1 is provided with a linkage assembly 5, the lower part of the front end face of the machine tool main body 1 is fixedly connected with a supporting plate 6, the upper end face of the supporting plate 6 is connected with a shaking plate 7 in a sliding manner, the bottom end face of the shaking plate 7 is provided with two sliding cylinders 702, a supporting sliding rod is connected inside each sliding cylinder 702 in a sliding manner, the two supporting sliding rods are fixedly connected to the upper end face of the supporting plate 6, the middle part of the left side of the shaking plate 7 is fixedly connected with a T-shaped driving plate 701, the left side of the upper end face of the T-shaped driving plate 701 is provided with a strip-shaped sliding opening, and the strip-shaped sliding opening on the T-shaped driving plate 701 is connected with a driving column 505 in a sliding manner; the upper end face of the shaking plate 7 is provided with four rectangular bayonets 703 and four round jacks, and the shaking plate 7 is used for driving the containing box 8 to shake left and right in a reciprocating manner;
a containing box 8 is arranged on the upper end surface of the shaking plate 7; the number of the limiting parts 9 is two, and the two limiting parts 9 are respectively arranged on the rear side of the power mechanism 2 and the machine tool main body 1; the access hole 101 is opened to 1 right-hand member face front side of lathe main part, is convenient for pull rod 903 in the spacing portion 9 in lower part to carry out the pulling operation, and 1 right-hand member face of lathe main part is located access hole 101 and rotates and be connected with access door 102, is equipped with passage 103 on the lateral wall before lathe main part 1, and lathe main part 1 top face has seted up circular port 104 to make the waste material can drop to inside passage 103 through circular port 104.
As shown in fig. 1 and 6, two T-shaped sliders are symmetrically arranged at the left and right of the bottom end surface of the lower die holder 4, a second plug board 401 is arranged at the middle of the rear end surface of the lower die holder 4, a rectangular socket is arranged at the middle of the upper end surface of the second plug board 401, and a circular through hole 402 is arranged at the middle of the upper end surface of the lower die holder 4; when the lower die holder 4 is installed on the upper end surface of the machine tool main body 1, the two T-shaped sliding blocks on the lower die holder 4 are respectively in sliding connection with the two T-shaped sliding grooves on the machine tool main body 1, so that the lower die holder 4 is more stable on the upper end surface of the machine tool main body 1.
As shown in fig. 1 and 7, the linkage assembly 5 includes a linkage shaft 501, a transverse rotating shaft 502, a vertical rotating shaft 503, a circular turntable 504 and a driving post 505, the linkage shaft 501 is rotatably connected to the front side of the top of the Contraband-shaped supporting plate 201, the front end and the rear end of the linkage shaft 501 are respectively provided with a first belt pulley and a linkage gear, and the linkage gear is engaged with the driving rack 204; the transverse rotating shaft 502 and the vertical rotating shaft 503 are rotatably connected to the front end surface of the machine tool body 1, a first bevel gear is mounted at the front end of the transverse rotating shaft 502, a second belt wheel is mounted on the rear side of the outer portion of the transverse rotating shaft 502, and the second belt wheel is in transmission connection with the first belt wheel through a belt; vertical pivot 503 upper end is equipped with the second bevel gear with first bevel gear meshing, and vertical pivot 503 lower extreme is equipped with circular carousel 504, and circular carousel 504 bottom face edge is equipped with and drives post 505, through the setting of linkage subassembly 5 for take simultaneously at power unit 2 operation and rock plate 7 and carry out left and right reciprocating motion.
The bottom end face of the containing bin 8 is fixedly connected with a mounting plate 801, two rectangular through holes 802 are formed in the left side and the right side of the bottom end face of the mounting plate 801, an elastic buckle 803 is connected to the inside of each rectangular through hole 802 in a sliding mode, a spring is installed inside each rectangular through hole 802, and the four elastic buckles 803 are respectively clamped with the four rectangular bayonets 703; the upper end of each elastic buckle 803 is fixedly connected with an L-shaped driving rod 804, and each L-shaped driving rod 804 is provided with a trapezoidal block 808; four vertical slide bars 805 of the equal fixedly connected with in mounting panel 801 up end left and right sides, and per four vertical slide bars 805 outside equal sliding connection have a sliding plate 806, a lifting rod 807 of sliding plate 806 up end middle part fixedly connected with, and lifting rod 807 upper end is equipped with the handle, mounting panel 801 bottom end face is equipped with four spacing inserted bars, and four spacing inserted bars peg graft with four circular jacks on rocking plate 7 respectively, thereby make and accomodate workbin 8 and can obtain effectual limiting displacement rocking plate 7 upper portion.
The limiting part 9 comprises a limiting shell 901, a limiting slider 902, a pulling rod 903 and a limiting plate 904, the limiting shell 901 is mounted on the upper end face of the mounting plate 801, the limiting slider 902 is connected to the inside of the limiting shell 901 in a sliding manner, the upper end of the limiting slider 902 is fixedly connected with the pulling rod 903 penetrating through the top of the limiting shell 901, the upper end of the pulling rod 903 is rotatably connected with a handle, and a spring is sleeved outside the pulling rod 903 and positioned inside the limiting shell 901; the upper end surface of the limiting shell 901 is symmetrically provided with two limiting plates 904, and the upper ends of the two limiting plates 904 are provided with gaps; the lower end of the limiting slide block 902 is provided with an inserting plate penetrating through the bottom of the limiting shell 901, and the limiting part 9 is used for limiting the punching punch 3 and the lower die holder 4;
when the two limiting parts 9 are in a limiting state, the plug board in one limiting part 9 at the upper part is plugged with the rectangular socket on the first plug board 302, and the plug board in one limiting part 9 at the lower part is plugged with the rectangular socket on the second plug board 401, so that the punching punch 3 and the lower die holder 4 can be effectively limited.
The specific use mode and function of the embodiment are as follows: when the airplane wing rib is subjected to hole opening and slotting, the airplane wing rib is firstly arranged at the upper part of a lower die holder 4 and then extends downwards through an expansion link of a hydraulic cylinder 202, so that a lifting plate 203, a connecting plate 301 and a punching punch 3 are driven to move downwards quickly, then the airplane wing rib at the upper part of the lower die holder 4 is subjected to punching operation through the lower end of the punching punch 3, and punched waste materials fall into a storage bin 8 through a circular hole 104 and a material guide pipe 103;
in the up-down moving process of the lifting plate 203, the driving rack 204 is driven to move up and down, so that the linkage gear, the linkage shaft 501 and the first belt wheel are driven to rotate, then the first belt wheel drives the second belt wheel to rotate through a belt, so that the transverse rotating shaft 502 drives the first bevel gear, the second bevel gear, the vertical rotating shaft 503 and the circular turntable 504 to rotate, then the circular turntable 504 drives the column 505 to rotate, then the column 505 drives the T-shaped driving plate 701 to move left and right in a reciprocating manner, so that the swinging plate 7 drives the containing box 8 to move left and right in a reciprocating manner, waste materials collected in the containing box 8 can be smoother under the swinging action, the inner space of the containing box 8 can be fully utilized, the structure is simple, additional driving devices such as a motor and the like are not needed, and the cost and the loss of electric energy are saved;
when punch 3 and die holder 4 need to be changed, at first pull the handle in two spacing portions 9 to the tail end pulling, make pulling pole 903 take spacing slider 902 and picture peg to the tail end removal, thereby make two picture peg head ends respectively from the rectangle socket on first plugboard 302 and the inside extraction of rectangle socket on the second plugboard 401, thereby make connecting plate 301 lose limiting displacement in lifter plate 203 bottom, and die holder 4 loses limiting displacement at lathe main part 1 up end, then it can to slide forward and insert punch 3 and die holder 4, whole change in-process, owing to need not to tear down fasteners such as a large amount of bolts through the instrument, and the convenience of punch 3 and die holder 4 when changing has been improved.
The above description is intended to be illustrative of the present invention and not to limit the scope of the invention, which is defined by the claims appended hereto.

Claims (10)

1. An aircraft rib tapping and grooving device, comprising: a machine tool main body (1) and a limiting part (9); a power mechanism (2) is installed on the front side of the upper end face of the machine tool main body (1), two T-shaped sliding grooves are symmetrically formed in the front side of the upper end face of the machine tool main body (1) in a bilateral mode, a lower die holder (4) is connected to the front side of the upper end face of the machine tool main body (1) in a sliding mode through the two T-shaped sliding grooves, and a punching punch (3) is installed at the lower end of the power mechanism (2) through a connecting plate (301); the front side of the machine tool main body (1) is provided with a linkage assembly (5), the lower part of the front end face of the machine tool main body (1) is fixedly connected with a supporting plate (6), the upper end face of the supporting plate (6) is connected with a swinging plate (7) in a sliding mode, and the upper end face of the swinging plate (7) is provided with a containing bin (8); the number of the limiting parts (9) is two, and the two limiting parts (9) are respectively arranged on the rear side of the power mechanism (2) and the machine tool main body (1); the machine tool is characterized in that an access hole (101) is formed in the front side of the right end face of the machine tool body (1), the right end face of the machine tool body (1) is located at the access hole (101) and is rotatably connected with an access door (102), a material guide pipe (103) is arranged on the front side wall of the machine tool body (1), and a circular hole (104) is formed in the top end face of the machine tool body (1).
2. An aircraft rib tapping device as claimed in claim 1 wherein: the power mechanism (2) comprises Contraband-shaped support plates (201), a hydraulic cylinder (202), a lifting plate (203), a driving rack (204) and rectangular support plates (205), the Contraband-shaped support plate (201) is installed on the upper end face of the machine tool body (1), the hydraulic cylinder (202) is installed on the top of the Contraband-shaped support plate (201), an expansion rod of the hydraulic cylinder (202) penetrates through the top of Contraband-shaped support plate (201), the lower end of the expansion rod of the hydraulic cylinder (202) is fixedly connected with the lifting plate (203), and four corners of the upper end face of the lifting plate (203) are fixedly connected with a vertical guide rod penetrating through the top of the Contraband-shaped support plate (201); the left side of the front end face of the lifting plate (203) is fixedly connected with a driving rack (204), the rear end face of the lifting plate (203) is fixedly connected with a rectangular support plate (205), a limiting part (9) is installed on the rear end face of the rectangular support plate (205), and the bottom end of the lifting plate (203) is in a bilateral symmetry shape and is provided with two T-shaped sliding grooves.
3. An aircraft rib opening and grooving device as claimed in claim 2, wherein: punch drift (3) and connecting plate (301) fixed connection, and connecting plate (301) upper end is personally submitted bilateral symmetry and is described and be equipped with two T type sliders, and connecting plate (301) rear end face middle part fixedly connected with first plugboard (302), and first plugboard (302) upper end face middle part has seted up the rectangle socket.
4. An aircraft rib opening and grooving device as claimed in claim 3, wherein: when the connecting plate (301) is installed on the bottom end face of the lifting plate (203), the two T-shaped sliding blocks on the connecting plate (301) are respectively in sliding connection with the two T-shaped sliding grooves on the bottom end face of the lifting plate (203), and the rear end of the first plug-in plate (302) penetrates through the rectangular support plate (205).
5. An aircraft rib opening and grooving device as claimed in claim 3, wherein: the bottom end surface of the lower die holder (4) is bilaterally symmetrical and is provided with two T-shaped sliding blocks, the middle part of the rear end surface of the lower die holder (4) is provided with a second plug board (401), the middle part of the upper end surface of the second plug board (401) is provided with a rectangular socket, and the middle part of the upper end surface of the lower die holder (4) is provided with a circular through hole (402); when the lower die holder (4) is installed on the upper end face of the machine tool main body (1), the two T-shaped sliding blocks on the lower die holder (4) are respectively in sliding connection with the two T-shaped sliding grooves on the machine tool main body (1).
6. An aircraft rib opening and grooving device as claimed in claim 5, wherein: the linkage assembly (5) comprises a linkage shaft (501), a transverse rotating shaft (502), a vertical rotating shaft (503), a circular turntable (504) and a driving column (505), the linkage shaft (501) is rotatably connected to the front side of the top of the Contraband-shaped support plate (201), a first belt wheel and a linkage gear are respectively mounted at the front end and the rear end of the linkage shaft (501), and the linkage gear is meshed with the driving rack (204); the transverse rotating shaft (502) and the vertical rotating shaft (503) are rotatably connected to the front end surface of the machine tool main body (1), a first bevel gear is mounted at the front end of the transverse rotating shaft (502), a second belt wheel is mounted on the rear side of the outer portion of the transverse rotating shaft (502), and the second belt wheel is in transmission connection with the first belt wheel through a belt; the upper end of the vertical rotating shaft (503) is provided with a second bevel gear meshed with the first bevel gear, the lower end of the vertical rotating shaft (503) is provided with a circular turntable (504), and the edge of the bottom end face of the circular turntable (504) is provided with a driving column (505).
7. An aircraft rib opening and grooving device as claimed in claim 6, wherein: the bottom end face of the shaking plate (7) is provided with two sliding cylinders (702), a supporting sliding rod is connected inside each sliding cylinder (702) in a sliding mode, the two supporting sliding rods are fixedly connected to the upper end face of the supporting plate (6), the middle of the left side of the shaking plate (7) is fixedly connected with a T-shaped driving plate (701), the left side of the upper end face of the T-shaped driving plate (701) is provided with a strip-shaped sliding opening, and the strip-shaped sliding opening in the T-shaped driving plate (701) is connected with the driving column (505) in a sliding mode; four rectangular bayonets (703) and four circular jacks are formed in the upper end face of the shaking plate (7).
8. An aircraft rib opening and grooving device as claimed in claim 7, wherein: the bottom end face of the containing bin (8) is fixedly connected with a mounting plate (801), the left side and the right side of the bottom end face of the mounting plate (801) are respectively provided with two rectangular through holes (802), each rectangular through hole (802) is internally connected with an elastic buckle (803) in a sliding mode, a spring is arranged in each rectangular through hole (802), and the four elastic buckles (803) are respectively clamped with the four rectangular bayonets (703); the upper end of each elastic buckle (803) is fixedly connected with an L-shaped driving rod (804), and each L-shaped driving rod (804) is provided with a trapezoidal block (808); the mounting panel (801) up end equal fixedly connected with four vertical slide bars (805) in the left and right sides, and per four vertical slide bars (805) outside equal sliding connection have a sliding plate (806), sliding plate (806) up end middle part fixedly connected with one carry pull rod (807), and carry pull rod (807) upper end and be equipped with the handle, mounting panel (801) bottom face is equipped with four spacing inserted bars, and four spacing inserted bars are pegged graft with four circular jacks on rocking plate (7) respectively.
9. An aircraft rib opening and grooving device as claimed in claim 8, wherein: the limiting part (9) comprises a limiting shell (901), a limiting slider (902), a pulling rod (903) and a limiting plate (904), the limiting shell (901) is mounted on the upper end face of the mounting plate (801), the limiting slider (902) is connected to the inside of the limiting shell (901) in a sliding mode, the pulling rod (903) penetrating through the top of the limiting shell (901) is fixedly connected to the upper end of the limiting slider (902), a pulling handle is connected to the upper end of the pulling rod (903) in a rotating mode, and a spring is sleeved inside the limiting shell (901) outside the pulling rod (903); the upper end surface of the limiting shell (901) is symmetrically provided with two limiting plates (904), and the upper ends of the two limiting plates (904) are provided with gaps; the lower end of the limiting sliding block (902) is provided with an inserting plate penetrating through the bottom of the limiting shell (901).
10. An aircraft rib tapping device as claimed in claim 9 wherein: when the two limiting parts (9) are in limiting states, the plug board in one limiting part (9) at the upper part is plugged with the rectangular socket on the first plug board (302), and the plug board in one limiting part (9) at the lower part is plugged with the rectangular socket on the second plug board (401).
CN202211154352.3A 2022-09-22 2022-09-22 Aircraft wing rib trompil fluting device Pending CN115229032A (en)

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CN202211154352.3A CN115229032A (en) 2022-09-22 2022-09-22 Aircraft wing rib trompil fluting device

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