CN115178774A

CN115178774A - Auxiliary device for punching based on aircraft parts

Info

Publication number: CN115178774A
Application number: CN202211112911.4A
Authority: CN
Inventors: 徐俊杰
Original assignee: Sheyang Kongfeitian Aviation Equipment Co ltd
Current assignee: Sheyang Kongfeitian Aviation Equipment Co ltd
Priority date: 2022-09-14
Filing date: 2022-09-14
Publication date: 2022-10-14

Abstract

The invention provides an auxiliary device for punching aircraft parts, which relates to the technical field of punching of aircraft parts and comprises a base, wherein the main body of the base is of a rectangular structure, an electromagnetic plate is fixedly connected to the inner side of the base, and the electromagnetic plate is of a magnetic structure generated by electrifying.

Description

Auxiliary device for punching aircraft parts

Technical Field

The invention relates to the technical field of punching of aircraft parts, in particular to an auxiliary device for punching of aircraft parts.

Background

The airplane parts refer to various parts of an airplane in an assembling process, the airplane parts are drilled in a machining process, and the drilling process refers to an operation of machining holes in a solid material by using a drill.

The prior punching auxiliary device has the following defects in the practical application process:

1. when the existing punching auxiliary device is used for punching and processing airplane parts, corresponding clamping devices are generally needed to clamp the parts and then synchronously punch and process the parts, but precision processing is needed during punching, so that an effective positioning structure is lacked during punching, precision is easily reduced, and further limitation exists;

2. the existing punching auxiliary device is often low in punching efficiency due to the lack of a quick and effective positioning structure when punching processing operation is performed on airplane parts, and the punching efficiency is reduced due to the fact that manual repeated measurement and positioning are needed when punching operation is performed.

In view of the above, the present invention provides an auxiliary device for punching holes in aircraft parts, which is improved in view of the conventional structure and defects.

Disclosure of Invention

The invention provides an auxiliary device for punching aircraft parts, which solves the problems that the existing punching auxiliary device is often low in punching efficiency and further reduces the machining efficiency due to the fact that the existing punching auxiliary device is lack of a quick and effective positioning structure when the existing punching auxiliary device is used for punching the aircraft parts, and the punching efficiency is low due to the fact that manual repeated measurement and positioning are needed when the existing punching auxiliary device is used for punching the aircraft parts.

The invention provides an auxiliary device for punching parts based on an airplane, which has the purposes and effects that: base and motor B, the main part of base is the rectangle structure, and the inboard fixedly connected with electromagnetic plate of base, and the electromagnetic plate produces the magnetic structure for the circular telegram, and the inside of electromagnetic plate has seted up the transverse groove to the inside sliding connection of transverse groove who sets up in the electromagnetic plate has the slider, and the slider is equipped with two altogether, and the internally mounted of two sliders has the regulation pole A, the transmission shaft is installed to motor B's bottom, and the transmission shaft of motor B bottom installation passes the movable block downwards to the salient movable block, and install anchor clamps on the transmission shaft of motor B bottom installation, and the transmitter is installed to the bottom of movable block, and electric putter D is installed to the front end of bracket.

Furthermore, a screw rod is installed on the left side of the motor A, the motor A is used for driving the screw rod to rotate, the screw rod and the guide rod are arranged in parallel, a moving seat is installed on the outer sides of the guide rod and the screw rod, an adjusting rod B is installed at the front end of the moving seat, and the adjusting rod B is a bidirectional screw rod.

Furthermore, a transverse groove is formed in the bracket, an electric push rod C is arranged in the transverse groove formed in the bracket, a moving block is connected in a sliding mode in a longitudinal groove formed in the bracket, the electric push rod C is connected with the moving block, and a motor B is arranged at the top end of the moving block.

Furthermore, adjust pole A and be the lead screw structure, and the top of electromagnetic plate has placed well accuse ware, the inside of well accuse ware seted up with adjust pole A assorted screw, and the top of well accuse ware is installed the ware of making a video recording, and the ware of making a video recording is used for shooing the part picture.

Further, remove the inside of seat and seted up vertical groove, and remove the vertical inslot portion of seting up in the seat and be subtend sliding connection and have two splint to regulation pole B assorted screw has all been seted up to the inside of two splint, and the pressure sensor is installed to one side of splint, and has the bottom plate through spring mounting in the splint one side of installing the pressure sensor.

Further, the rear side of base is opened and is equipped with the transverse groove, and the transverse groove internally mounted that the base rear side was seted up has electric putter A to the rear side sliding connection of base has the support, and electric putter A is connected with the support, and electric putter B is installed on the top of support, and the bracket is installed on electric putter B's top.

Further, the recognizer is installed to electric putter D's front end to the thermoscope is installed to the bottom of recognizer, and the thermoscope is used for detecting the laser temperature that the laser instrument launches, and the receiver is installed on the top of recognizer, and the receiver is used for the transmitter under the position.

Furthermore, the laser is installed in the top end face central position of well accuse ware, and the laser is installed for perpendicular with well accuse ware, and the laser is used for transmitting laser, and the inboard fixedly connected with guide arm of base, the right side of base still installs motor A.

Compared with the prior art, the invention has the following beneficial effects:

1. when adjusting pole B and rotating, can carry out the transmission through the splint with two of sliding connection in removing the seat and be connected, and draw close each other through two splint and carry out quick tight spacing operation of clamp to the aircraft spare part of placing on removing the seat, and press from both sides tight spacing in-process, install the bottom plate in the splint outside and can contact with the spare part of placing on removing the seat, and synchronous extrudeing the pressure sensor of installing in the splint outside and detect, the pressure sensor of installing through two splint outsides detects when the pressurized data of spare part is unanimous then explains that the spare part of placing on removing the seat at present is in accurate spacing state, and then reach the purpose of quick location.

2. The regulation pole A of installing in the slider is holding through manual and is driving well accuse ware and removing along the electromagnetic plate, and synchronous horizontal position of accuse ware in the middle of adjust the back that finishes, resynchronize adjusts the vertical position of accuse ware on the electromagnetic plate through manual rotation regulation pole A, carry out quick discernment location through the position that the camera need punch to spare part and accomplish the back, the laser is launched out at the laser instrument on well accuse ware top to spare part to the start-up of resynchronization, make the position that spare part need punch the processing carry out local intensification operation, and then reach the purpose of quick location.

3. The temperature detector detects that the central area of placing the local intensification of spare part on removing the seat carries out quick location discernment can, the resynchronization is installed on the anchor clamps with the drill bit this moment, the electric putter C of start-up installation in the bracket will come the movable block to promote to the front side, until can be installed after the receiver on the recognizer top receives the quick location operation to the drill bit at the light beam of launching at the transmitter of installing the movable block bottom, the resynchronization withdraws the recognizer this moment, the electric putter B of start-up installation on the support top drives the bracket and synchronous drives the drill bit and descends, then the resynchronization start-up install motor B on the movable block top rotate the drive to the anchor clamps in order to carry out quick processing operation of punching to spare part can, and then reach more practical purpose.

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 only some embodiments of the invention and are not intended to limit the invention.

In the drawings:

FIG. 1 is a schematic front side view showing a partially sectioned auxiliary device according to an embodiment of the present invention;

FIG. 2 is a schematic view of a partial cross-sectional structure of an auxiliary device according to an embodiment of the present invention;

FIG. 3 is a view showing an assembled structure of an auxiliary device according to an embodiment of the present invention;

FIG. 4 is a schematic top view of an auxiliary device according to an embodiment of the present invention;

FIG. 5 is a schematic view of a cradle to receiver display structure of an accessory device according to an embodiment of the present invention;

FIG. 6 shows a schematic view of a mount to laser display structure of an auxiliary device according to an embodiment of the invention;

FIG. 7 is an enlarged schematic view of an auxiliary device according to an embodiment of the invention at A in FIG. 2;

fig. 8 is an enlarged structural view of an auxiliary device according to an embodiment of the present invention at B in fig. 2.

List of reference numerals

1. A base; 2. an electromagnetic plate; 3. a slider; 4. adjusting a rod A; 5. a central controller; 6. a camera; 7. a laser; 8. a guide bar; 9. a motor A; 10. a screw; 11. a movable seat; 12. an adjusting rod B; 13. a splint; 14. a pressure sensor; 15. a base plate; 16. an electric push rod A; 17. a support; 18. an electric push rod B; 19. a bracket; 20. an electric push rod C; 21. a moving block; 22. a motor B; 23. a clamp; 24. a transmitter; 25. an electric push rod D; 26. an identifier; 27. a temperature detector; 28. a receiver.

Detailed Description

The embodiments of the present invention will be described in further detail with reference to the drawings and examples. The following examples are intended to illustrate the invention but are not intended to limit the scope of the invention.

Example (b):

as shown in figures 1 to 8:

the invention provides an auxiliary device for punching based on aircraft parts, which comprises: base 1 and motor B22, the main part of base 1 is the rectangle structure, and the inboard fixedly connected with electromagnetic plate 2 of base 1, electromagnetic plate 2 produces the magnetic structure for the circular telegram, and the transverse groove has been seted up to the inside of electromagnetic plate 2, and the inside sliding connection of the transverse groove who sets up in the electromagnetic plate 2 has slider 3, slider 3 is equipped with two altogether, and the internally mounted of two slider 3 has regulation pole A4, the transmission shaft is installed to motor B22's bottom, and the transmission shaft that motor B22 bottom was installed passes movable block 21 downwards, and salient movable block 21, and install anchor clamps 23 on the transmission shaft that motor B22 bottom was installed, and transmitter 24 is installed to the bottom of movable block 21, electric putter D25 is installed to the front end of bracket 19, recognizer 26 is installed to electric putter D25's front end, and thermoscope 27 is installed to recognizer 26's bottom, thermoscope 27 is used for detecting the laser temperature that laser 7 launched, and receiver 28 is installed on recognizer 26's top, receiver 28 is used for transmitter 24 under the position.

Wherein, adjust pole A4 and be the lead screw structure, and well accuse ware 5 has been placed on the top of electromagnetism board 2, well accuse ware 5's inside is seted up and is adjusted pole A4 assorted screw, and the top of well accuse ware 5 is installed camera 6, camera 6 is used for shooing the part picture, well accuse ware 5's top end face central point puts and installs laser instrument 7, laser instrument 7 and well accuse ware 5 are installed for perpendicular, and laser instrument 7 is used for transmitting laser, the inboard fixedly connected with guide arm 8 of base 1, motor A9 is still installed on the right side of base 1, detect when thermoscope 27 place the central zone that the part on moving seat 11 heaies up carries out quick location discernment can, install the drill bit on anchor clamps 23 when this moment resynchronization, the electric putter C20 of start-up installation in bracket 19 promotes the movable block 21 forward, carry out the quick location operation to the drill bit after can be installed at the receiver 28 on the recognizer 26 top at the transmitter 24 of installing in movable block 21 bottom can be received, the synchronous drill bit that this moment withdrawal of withdrawing of rethronizing, start-up the electric putter B18 that installs the bracket 17 top drive the drill bit and carry out the synchronous operation of carrying out, then, the top that the drill bit is installed and carry out the practical drilling to carry out the practical quick operation can be carried out, the utility part to the drill bit in order to carry out the utility part that the utility of moving block 23.

Wherein, a screw rod 10 is installed on the left side of a motor A9, the motor A9 is used for driving the screw rod 10 to rotate, and the screw rod 10 and the guide rod 8 are arranged in parallel, a moving seat 11 is installed on the outer sides of the guide rod 8 and the screw rod 10, an adjusting rod B12 is installed at the front end of the moving seat 11, the adjusting rod B12 is a bidirectional screw rod, a longitudinal groove is formed in the moving seat 11, two clamping plates 13 are connected in the moving seat 11 in a sliding manner, screw holes matched with the adjusting rod B12 are formed in the two clamping plates 13, a pressure sensor 14 is installed on one side of each clamping plate 13, a bottom plate 15 is installed on one side of each clamping plate 13, a regulating rod A4 installed in the sliding block 3 is manually held to drive the central controller 5 to move along the electromagnetic plate 2, and after the horizontal position of the central controller 5 is regulated synchronously, the longitudinal position of the central controller 5 on the electromagnetic plate 2 is regulated again synchronously through manual rotation of the regulating rod A4, after the position of the part to be punched is quickly identified and positioned by the camera 6, the top end of the central controller 5 is started, and the part 7 is subjected to the laser punching operation, and the part heating operation required for the part punching operation is achieved.

The rear side of the base 1 is provided with a transverse groove, an electric push rod a16 is installed inside the transverse groove formed in the rear side of the base 1, the rear side of the base 1 is connected with a support 17 in a sliding mode, the electric push rod a16 is connected with the support 17, an electric push rod B18 is installed at the top end of the support 17, a bracket 19 is installed at the top end of the electric push rod B18, the transverse groove is formed inside the bracket 19, an electric push rod C20 is installed inside the transverse groove formed in the bracket 19, a moving block 21 is connected inside a longitudinal groove formed in the bracket 19 in a sliding mode, the electric push rod C20 is connected with the moving block 21, a motor B22 is installed at the top end of the moving block 21, when the adjusting rod B12 rotates, the adjusting rod can be in transmission connection with two clamping plates 13 connected in the moving seat 11 in a sliding mode, airplane parts placed on the moving seat 11 are quickly clamped and limited through mutual closing of the two clamping plates 13, in the clamping limiting process, a bottom plate 15 installed outside the clamping plate 13 can be in contact with the parts placed on the moving seat 11 accurately, and the pressing sensor 14 can detect whether the pressing sensor is in the pressing state, and the pressing sensor 14 is detected by the pressing sensor.

When in use: firstly, when the airplane parts need to be punched, the parts need to be punched can be placed on the movable seat 11 with the front faces upward, and the parts can be synchronously rotated through an adjusting rod B12 which is manually rotated and arranged at the front end of the movable seat 11;

when the adjusting rod B12 rotates, the adjusting rod B can be in transmission connection with two clamping plates 13 which are slidably connected in the movable seat 11, and the aircraft parts placed on the movable seat 11 can be quickly clamped and limited by the mutual approach of the two clamping plates 13, in the process of clamping and limiting, a bottom plate 15 arranged on the outer side of the clamping plate 13 can be in contact with the parts placed on the movable seat 11 and synchronously carries out extrusion detection on a pressure sensor 14 arranged on the outer side of the clamping plate 13, and when the pressure sensors 14 arranged on the outer sides of the two clamping plates 13 detect that the pressure data of the parts are consistent, the parts currently placed on the movable seat 11 are in a precise limiting state, so that the purpose of quick positioning is achieved;

then, a motor A9 arranged on the outer side of the base 1 is synchronously started to drive the screw rod 10 to rotate, the screw rod 10 is in transmission connection with a moving seat 11 connected to the outer side of the guide rod 8 in a sliding mode to drive the moving seat 11 to move, parts limited on the inner side of the clamping plate 13 are driven by the moving seat 11 to be rapidly moved and adjusted, and therefore the purpose of improving machining efficiency is achieved;

then, synchronously manually holding an adjusting rod A4 arranged in the sliding block 3 to drive the central controller 5 to move along the electromagnetic plate 2, synchronously adjusting the transverse position of the central controller 5, synchronously adjusting the longitudinal position of the central controller 5 on the electromagnetic plate 2 by manually rotating the adjusting rod A4, quickly identifying and positioning the position of the part to be punched by the camera 6, synchronously starting a laser 7 arranged at the top end of the central controller 5 to emit laser to irradiate the part, and locally heating the position of the part to be punched, so that the purpose of quick positioning is achieved;

then, the electric push rod a16 installed at the rear side of the base 1 is synchronously started to adjust the transverse position of the support 17, the electric push rod D25 installed at the front end of the bracket 19 is synchronously started to push the identifier 26 and the temperature detector 27 together to the outside until the temperature detector 27 detects that the central area of the part placed on the moving seat 11 is heated locally is quickly positioned and identified, at the moment, the drill bit is synchronously installed on the clamp 23, the electric push rod C20 installed in the bracket 19 is started to push the moving block 21 to the front side until the light beam emitted by the emitter 24 installed at the bottom end of the moving block 21 can be received by the receiver 28 installed at the top end of the identifier 26 to quickly position the drill bit, at the moment, the identifier 26 is synchronously withdrawn, the electric push rod B18 installed at the top end of the support 17 is started to drive the bracket 19 and synchronously drive the drill bit to descend, and then the motor B22 installed at the top end of the moving block 21 is synchronously started to rotate the clamp 23 to drive the clamp 23 to quickly drill the part, so as to achieve the purpose of being more practical.

The embodiments of the present invention have been presented for purposes of illustration and description, and are not intended to be exhaustive or limited to the invention in the form disclosed. Many modifications and variations will be apparent to practitioners skilled in this art. The embodiment was chosen and described in order to best explain the principles of the invention and the practical application, and to enable others of ordinary skill in the art to understand the invention for various embodiments with various modifications as are suited to the particular use contemplated.

Claims

1. An auxiliary device based on aircraft parts usefulness of punching, its characterized in that includes: base (1) and motor B (22), the main part of base (1) is the rectangle structure, and inboard fixedly connected with electromagnetic plate (2) of base (1), electromagnetic plate (2) are for circular telegram production magnetic structure, and the transverse groove has been seted up to the inside of electromagnetic plate (2), and the inside sliding connection of transverse groove who offers in electromagnetic plate (2) has slider (3), slider (3) are equipped with two altogether, and the internally mounted of two slider (3) has regulation pole A (4), the transmission shaft is installed to the bottom of motor B (22), and the transmission shaft of motor B (22) bottom installation passes movable block (21) downwards to protrusion movable block (21), and install anchor clamps (23) on the transmission shaft of motor B (22) bottom installation, and emitter (24) are installed to the bottom of movable block (21), and electric putter D (25) are installed to the front end of bracket (19).

2. The auxiliary device for punching the aircraft component as claimed in claim 1, wherein: adjust pole A (4) and be the lead screw structure, and accuse ware (5) have been placed on the top of electromagnetic plate (2), the inside of well accuse ware (5) seted up with adjust pole A (4) assorted screw, and the top of well accuse ware (5) is installed and is made a video recording ware (6), makes a video recording ware (6) are used for shooing the part picture.

3. The auxiliary device for punching the aircraft component as claimed in claim 2, wherein: well top of accuse ware (5) face central point puts and installs laser instrument (7), and laser instrument (7) and well accuse ware (5) are installed for perpendicular, and laser instrument (7) are used for transmitting laser, and motor A (9) are still installed on the right side of base (1) to the inboard fixedly connected with guide arm (8) of base (1).

4. An auxiliary device for drilling based on aircraft parts as claimed in claim 3, wherein: screw rod (10) are installed in the left side of motor A (9), and motor A (9) are used for driving screw rod (10) to rotate, and screw rod (10) and guide arm (8) are parallel arrangement, and removal seat (11) are installed in the outside of guide arm (8) and screw rod (10), and the front end of removing seat (11) is installed and is adjusted pole B (12), adjusts pole B (12) and is two-way lead screw.

5. The auxiliary device for punching the aircraft component as claimed in claim 4, wherein: remove the inside of seat (11) and seted up vertical groove, and remove the vertical inslot portion of seting up in seat (11) and be subtend sliding connection and have two splint (13) to the screw of adjusting pole B (12) assorted has all been seted up to the inside of two splint (13), and pressure sensor (14) are installed to one side of splint (13), and have bottom plate (15) through spring mounting in splint (13) one side of installing pressure sensor (14).

6. The auxiliary device for drilling the aircraft part according to claim 1, wherein: the rear side of base (1) is opened and is equipped with the transverse groove, and the transverse groove internally mounted that base (1) rear side was seted up has electric putter A (16) to the rear side sliding connection of base (1) has support (17), and electric putter A (16) are connected with support (17), and electric putter B (18) are installed on the top of support (17), and bracket (19) are installed on the top of electric putter B (18).

7. The auxiliary device for drilling the aircraft part according to claim 6, wherein: a transverse groove is formed in the bracket (19), an electric push rod C (20) is installed in the transverse groove formed in the bracket (19), a moving block (21) is connected to the inner portion of a longitudinal groove formed in the bracket (19) in a sliding mode, the electric push rod C (20) is connected with the moving block (21), and a motor B (22) is installed at the top end of the moving block (21).

8. The auxiliary device for punching the aircraft component as claimed in claim 1, wherein: recognizer (26) is installed to the front end of electric putter D (25) to thermoscope (27) are installed to the bottom of recognizer (26), and thermoscope (27) are used for detecting the laser temperature that laser instrument (7) were launched, and receiver (28) are installed on the top of recognizer (26), and receiver (28) are used for position under emitter (24).