LASER SHOCK FORGING AND LASER CUTTING COMPOSITE ADDITIVE MANUFACTURING DEVICE AND METHOD

20190283184 ยท 2019-09-19

    Inventors

    Cpc classification

    International classification

    Abstract

    The present invention discloses a laser shock forging and laser cutting composite additive manufacturing device and method. The device forms two different light guide systems by splitting an output laser beam of a laser device into two laser beams through a beam splitter system. The first light guide system splits a laser beam into a third laser beam and a fourth laser beam which are respectively applied to laser 3D (3-Dimensional) printing and laser cutting. The second laser beam is applied to laser shock forging. A three dimensional model is built according to individual design requirements of a part. Layer-by-layer slicing treatment is performed to acquire slice contour information, so as to determine a layered contour and internal complex structures such as a cavity, a pipeline and a cold pipe of the part through laser cutting. The third laser beam forms an Nth layer of slice through 3D printing, and the second laser beam performs synchronous laser shock forging in an optimal temperature region. The fourth laser beam works when the thickness of each layer of slice or each slice layer meets the requirements, thereby guaranteeing the dimension accuracy and the surface quality and realizing high-rigidity, high-accuracy and high-efficiency 3D printing. The device has the advantages of high machining efficiency, high quality and long service life.

    Claims

    1. A laser shock forging and laser cutting composite additive manufacturing device, comprising a laser generating system used for generating and controlling a laser beam, a laser shock forging system, a 3D (3-Dimensional) printing system, a laser cutting system, an on-line monitoring system used for monitoring internal structure performance, surface performance, shape and dimension of a part; and a real-time tracking and feedback system used for feeding back data to a plurality of laser beam power adjustment devices, wherein the laser generating system is respectively connected with the laser shock forging system, the 3D printing system, the laser cutting system and the real-time tracking and feedback system; the on-line monitoring system is connected with the real-time tracking and feedback system; the laser generating system comprises a computer, a laser device, a laser device power adjustment device, a beam splitter for splitting the laser beam into a first laser beam and a second laser beam, a first light guide system for controlling the first laser beam, a first power adjustment device and an adjustable beam splitter for splitting the first laser beam into a third laser beam and a fourth laser beam; the computer, the laser device power adjustment device, the laser device and the beam splitter are connected in sequence; one end of the first power adjustment device is connected with the first light guide system, and the other end of the first power adjustment device is connected with the adjustable beam splitter; the laser shock forging system comprises a second light guide system for controlling the second laser beam, a laser shock forging power adjustment device, a laser shock forging laser head and a laser shock forging control system; the second light guide system, the laser shock forging power adjustment device, the laser shock forging control system and the laser shock forging laser head are connected in sequence; the second light guide system is connected with the beam splitter; the laser cutting system comprises a fourth light guide system for controlling the fourth laser beam, a laser cutting power adjustment device, a laser cutting laser head and a laser cutting control system; the fourth light guide system, the laser cutting power adjustment device, the laser cutting control system and the laser cutting laser head are connected in sequence; the fourth light guide system is connected with the adjustable beam splitter; the 3D printing system comprises a third light guide system for controlling the third laser beam, a 3D printing power adjustment device, a 3D printing head, a powder feeding system, a powder feeding head for coaxially conveying light and powder and a 3D printing control system; the third light guide system, the 3D printing power adjustment device, the 3D printing control system and the 3D printing head are connected in sequence; the powder feeding head is mounted on the 3D printing head and is connected with the computer through the powder feeding system; the third light guide system is connected with the beam splitter; and the real-time tracking and feedback system is respectively connected with the computer, the laser power adjustment device, the first power adjustment device, the laser shock forging power adjustment device, the laser cutting power adjustment device and the 3D printing power adjustment device.

    2. The laser shock forging and laser cutting composite additive manufacturing device according to claim 1, wherein the laser cutting laser head and the 3D printing head are disposed adjacently and in parallel; and the adjustable beam splitter respectively controls the laser cutting laser head and the 3D printing head to work simultaneously or independently.

    3. The laser shock forging and laser cutting composite additive manufacturing device according to claim 2, wherein the laser shock forging system is disposed on the same side with the laser cutting laser head and the 3D printing head or on the side opposite to the laser cutting laser head and the 3D printing head, and the laser shock forging system may freely move on a working table.

    4. The laser shock forging and laser cutting composite additive manufacturing device according to claim 1, wherein the laser cutting system may act on one or more slice layers.

    5. A laser shock forging and laser cutting composite additive manufacturing method, comprising the following steps: Step S1: inputting original data: designing a three-dimensional model of a part to be formed according to individual design requirements, performing layer-by-layer slicing treatment to determine an optimal number of layers suitable for laser cutting, calculating main process parameters of 3D printing and optimizing the parameters, estimating main process parameters of laser shock forging and optimizing the parameters, and determining an optimal temperature region for the laser shock forging; transmitting relevant data into a computer as the original data which are used as an adjustment control standard for relevant parameters of a laser shock forging and laser cutting composite additive manufacturing process; Step S2: performing error analysis: forming a first layer of slice through laser 3D printing and synchronously, performing synchronous laser shock forging in the optimal temperature region; when the Nth layer of slice is obtained, performing laser cutting on the part to obtain a layered contour and internal complex structures; monitoring, by an on-line monitoring system, whether the internal structure performance, surface performance, shape and dimension of the part meet desirable requirements or not, comparatively analyzing the original data in Step 1 to determine whether the relevant process parameters are correct or not, and performing the error analysis to automatically compensate the process parameters and determine final optimal process parameters; Step S3: automatically compensating the Nth layer of slice formed by synchronous shock forging and 3D printing on the same side: installing a 3D printing system and a laser shock forging system on the same side of a working table; printing, by the 3D, printing system, the Nth layer of slice according to the individual design requirements for internal configurations such as a cavity, a pipeline and a cold pipe of the part to be formed; simultaneously; monitoring the internal structure performance, surface performance, shape and dimension of the formed slice layer in real time and on line; feeding back, by a real-time feedback system, data parameters to the 3D printing system and the laser shock forging system in sequence to automatically compensate the relevant process parameters; meanwhile, controlling, by a second laser beam control system, the laser shock forging system to work synchronously to realize a synchronous coupling action of 3D printing-detection and feedback-laser shock forging; Step 4: performing data acquisition and error analysis after the synchronous coupling action of 3D printing-detection and feedback-laser shock forging is realized on the same side: acquiring, by the on-line monitoring system, parameters of the internal structure performance, surface performance, shape and dimension of the part to be formed and parameters of four laser beams of a laser device; storing, by a computer, the data and feeding back the data to a 3D printing power adjustment device and a laser shock forging power adjustment device, and performing the error analysis; analytically calculating an optimal thickness N of the slice formed on the same side, and determining whether the thickness of the slice formed on both sides meets the requirement or not; Step S5: if the synchronous coupling action of 3D printing-detection and feedback-laser shock forging, realized on the same side, meets the relevant requirements, and an error is within an allowable error range, enabling a laser cutting system to work to cut, with laser, the internal configurations such as the cavity, the pipeline and the cold pipe of the part to be formed according to the individual design requirements, or implementing Step S6; Step S6: automatically compensating the (N+1)th layer of slice formed by synchronous shock forging and 3D printing on both sides: distributing the 3D printing system and the laser shock forging system on both sides; printing, by the 3D printing system, the (N+1)th layer of slice according to the individual design requirements for the internal configurations of the part to be formed; simultaneously, monitoring the internal structure performance, surface performance, shape and dimension of the formed slice layer in real time and on line; feeding back, by the real-time feedback system, data parameters to the 3D printing system and the laser shock forging system in sequence to automatically compensate the relevant process parameters; meanwhile, controlling the laser shock forging system to work synchronously to realize the synchronous coupling action of 3D printing-detection and feedback-laser shock forging; Step S7: performing data acquisition and error analysis after the synchronous coupling action of 3D printing-detection and feedback-laser shock forging is realized on both sides: acquiring, by the on-line monitoring system, parameters of the internal structure performance, surface performance, shape and dimension of the part to be formed and parameters of four laser beams of the laser device; storing, by the computer, the data and feeding back the data to the 3D printing power adjustment device and the laser shock forging power adjustment device, and performing the error analysis; analytically calculating an optimal thickness N of the slice formed on both sides, and determining whether the thickness of the slice formed on both sides meets the requirement or not; Step S8: if the synchronous coupling action of 3D printing-detection and feedback-laser shock forging, realized on both sides, meets the relevant requirements, and an error is within an allowable error range, enabling the laser cutting system to work to cut, with laser, the internal configurations such as the cavity, the pipeline and the cold pipe of the part to be formed according to the individual design requirements, or implementing Step S9; Step S9: comparatively analyzing the relevant data for automatically compensating the synchronous coupling action of the 3D printing system and the laser shock forging system on the same side and the relevant data for automatically compensating the synchronous coupling action of the 3D printing system and the laser shock forging system on both sides, and selecting the working solution with the best effect; and Step S10: continuously repeatedly machining the part according to the optimal working solution till the relevant parameters of the internal structure performance, surface performance, shape and dimension of the formed part are close to the desirable requirements and the error is within the allowable error range.

    Description

    DESCRIPTION OF THE DRAWINGS

    [0033] FIG. 1 is a structural schematic diagram of an embodiment of the present invention when a 3D printing system and a laser shock forging light guide system are located on the same side of a working table;

    [0034] FIG. 2 is a structural schematic diagram of an embodiment of the present invention when a 3D printing system and a laser shock forging light guide system are located on both sides of a working table; and

    [0035] FIG. 3 is a working schematic diagram of an embodiment of the present invention.

    [0036] Numerals in the Drawings:

    [0037] 1: laser shock forging laser head; 2: laser cutting laser head; 3: laser shock forging control system; 4: laser cutting control system; 5: laser cutting power adjustment device; 6: laser shock forging power adjustment device; 7: fourth light guide system; 8: second light guide system; 9: third light guide system; 10: adjustable beam splitter; 11: first power adjustment device; 12: beam splitter; 13: laser device; 14: first light guide system; 15: laser device power adjustment device; 16: computer; 17: 3D printing power adjustment device; 18: powder feeding system; 19: 3D printing control system; 20: powder feeding head; 21: real-time tracking and feedback system; 22: 3D printing head; and 23: on-line monitoring system.

    DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS

    [0038] In order to make the purposes, technical solutions and advantages of the present invention clearer and more specific, the present invention is further described below with reference to accompanying drawings and embodiments.

    [0039] Embodiment 1

    [0040] As shown in FIGS. 1, 2 and 3, the present invention discloses a laser shock forging and laser cutting composite additive manufacturing device and method. The manufacturing device mainly includes a laser shock forging control system 3 for controlling a second light guide system 8, a laser shock forging power adjustment device 6 and a laser shock forging laser head 1; a laser cutting control system 4 for controlling a fourth laser beam light guide system 7, a laser cutting power adjustment device 5 and a laser cutting laser head 2; a 3D printing control system 19 for controlling a third laser beam light guide system 9, a 3D printing power adjustment device 17 and a 3D printing head 22; a powder feeding system 18; a powder feeding head 20 for coaxially conveying light and powder; an on-line monitoring system 23 for monitoring the internal structure performance, surface performance, shape and dimension of a part; a real-time tracking and feedback system 21 for feeding back data monitored by the on-line monitoring system 23 to the laser beam power adjustment devices; a power adjustment device 15 for controlling the laser device 13; a beam splitter 12; a first light guide system 14; a first laser beam power adjustment device 11; and an adjustable beam splitter 10 for splitting a first laser beam into a third laser beam and a fourth laser beam. The real-time tracking and feedback system 21, the powder feeding system 18, the 3D printing power adjustment device 17, the first laser beam power adjustment device 11 and the power adjustment device 15 are connected with the computer 16 and are controlled by the computer 16.

    [0041] The laser shock forging light guide system 3 may freely move on both sides of the working table. The 3D printing system 20 and the laser shock forging system 1 synchronously work on the same side: spacing distances from the on-line monitoring system 23 to the 3D printing system 20 and the laser shock forging system 1 are obtained by blending analysis of corresponding temperature fields of the 3D printing and the shock forging to realize a synchronous action of the three systems. The 3D printing system 20 and the laser shock forging system 1 may be distributed at corresponding portions of both sides of a blade and work synchronously: the 3D printing system 20 and the laser shock forging system 1 are symmetrically distributed along a center line, and the on-line monitoring system and the 3D printing system are distributed in a certain spacing, and also may independently rotate to the laser shock forging side to achieve the synchronization action of the three systems. An optimal working solution is selected through error analysis to improve the machining efficiency.

    [0042] The 3D printing system 3, the laser shock forging system 2 and the laser cutting system 4 may enable the laser beam light guide systems of the laser device to select different parameters according to different requirements in the machining technological process. The on-line monitoring system 23 is used to synchronously detect a formed part, and the real-time tracking and feedback system 21 adjusts information and parameters such as the internal structure performance, surface performance, shape and dimension of the part and transmits the information and parameters to the laser beam power adjustment devices to respectively adjust and control relevant parameters of laser beams. After the relevant parameters are automatically compensated, the part is machined repeatedly for multiple times.

    [0043] As shown in FIG. 3, the present invention discloses a laser shock forging and laser cutting composite additive manufacturing method. The method specifically includes the following working steps:

    [0044] (1) original data are input:

    [0045] a three-dimensional model of a part to be formed is designed according to individual design requirements, for example: internal configurations such as a cavity, a pipeline and a cold pipe of the formed part; layer-by-layer slicing treatment is performed to determine an optimal number of layers suitable for laser cutting; main process parameters of 3D printing are calculated and then optimized; main process parameters of laser shock forging are estimated and then optimized; an optimal temperature region for the laser shock forging is determined; relevant data are transmitted into a computer as the original data which are used as an adjustment control standard for relevant parameters of a laser shock forging and laser cutting composite additive manufacturing process;

    [0046] (2) error analysis is performed;

    [0047] a first layer of slice is formed through laser 3D printing, and the laser shock forging is synchronously performed in the optimal temperature region; when the Nth layer of slice is obtained (N is generally equal to 8 to 10), laser cutting is performed on the part to obtain a layered contour and internal complex structures; an on-line monitoring system 23 monitors whether the internal structure performance, surface performance, shape and dimension of the part meet desirable requirements or not; the original data in Step 1 are comparatively analyzed to determine whether the relevant process parameters are correct or not; the error analysis is performed to automatically compensate the process parameters and determine final optimal process parameters;

    [0048] (3) the Nth layer of slice formed by synchronous shock forging and 3D printing is automatically compensated on the same side:

    [0049] a 3D printing system 3 and a laser shock forging system 2 are installed on the same side of a working table; the 3D printing system prints the Nth layer of slice according to the individual design requirements for the internal configurations such as the cavity, the pipeline and the cold pipe of the part to be formed; the internal structure performance, surface performance, shape and dimension of the formed slice layer are monitored in real time and on line; a real-time feedback system 21 feeds back data parameters to the 3D printing system 3 and the laser shock forging system 2 in sequence to automatically compensate the relevant process parameters; meanwhile, a second laser beam control system controls the laser shock forging system to work synchronously to realize a synchronous coupling action of 3D printing-detection and feedback-laser shock forging;

    [0050] (4) data acquisition and error analysis are performed after the synchronous coupling action of 3D printing-detection and feedback-laser shock forging is realized on the same side:

    [0051] the on-line monitoring system 23 acquires parameters of the internal structure performance, surface performance, shape and dimension of the part to be formed and parameters of four laser beams of a laser device; a computer stores the data and feeds back the data to a third laser beam power adjustment device and a second laser beam power adjustment device, and performs the error analysis; an optimal thickness N (N is generally equal to 8 to 10) of the slice formed on the same side is analytically calculated, and whether the thickness of the slice formed on both sides meets the requirement or not is determined;

    [0052] (5) if the synchronous coupling action of 3D printing-detection and feedback-laser shock forging, realized on the same side, meets the relevant requirements, and an error is within an allowable error range, a laser cutting system 4 works to cut, with laser, the internal configurations such as the cavity, the pipeline and the cold pipe of the part to be formed according to the individual design requirements, or Step (6) is implemented;

    [0053] (6) the (N+1)th layer of slice formed by synchronous shock forging and 3D printing is automatically compensated on both sides:

    [0054] the 3D printing system and the laser shock forging system are distributed on both sides; the 3D printing system prints the (N+1)th layer of slice according to the individual design requirements for the internal configurations such as the cavity, the pipeline and the cold pipe of the part to be formed; the internal structure performance, surface performance, shape and dimension of the formed slice layer are monitored in real time and on line; the real-time feedback system, feeds back data parameters to the 3D printing system 3 and the laser shock forging system 2 in sequence to automatically compensate the relevant process parameters; meanwhile, the second laser beam control system controls the laser shock forging system 2 to work synchronously to realize the synchronous coupling action of 3D printing-detection and feedback-laser shock forging;

    [0055] (7) data acquisition and error analysis are performed after the synchronous coupling action of 3D printing-detection and feedback-laser shock forging is realized on both sides:

    [0056] the on-line monitoring system acquires parameters of the internal structure performance, surface performance, shape and dimension of the part to be formed and parameters of four laser beams of the laser device; the computer stores the data and feeds back the data to the third laser beam power adjustment device and the second laser beam power adjustment device, and performs the error analysis; an optimal thickness N (N is generally equal to 8 to 10) of the slice formed on both sides is analytically calculated, and whether the thickness of the slice formed on both sides meets the requirement or not is determined;

    [0057] (8) if the synchronous coupling action of 3D printing-detection and feedback-laser shock forging, realized on both sides, meets the relevant requirements, and an error is within an allowable error range, the laser cutting system works to cut, with laser, the internal configurations such as the cavity, the pipeline and the cold pipe of the part to be formed according to the individual design requirements, or Step (9) is implemented;

    [0058] (9) the relevant data for automatically compensating the synchronous coupling action of the 3D printing system and the laser shock forging system on the same side and the relevant data for automatically compensating the synchronous coupling action of the 3D printing system and the laser, shock forging system on both sides are comparatively analyzed, and the working solution with the best effect is selected; and

    [0059] (10) the part is continuously repeatedly machined according to the optimal working solution till the relevant parameters of the internal structure performance, surface performance, shape and dimension of the formed part are close to the desirable requirements and the error is within the allowable error range.

    [0060] In this solution, the laser shock forging light guide system 2 may freely move on both sides of a workpiece; the 3D printing system 3 and the laser shock forging light guide system 2 are distributed on the same side or both sides of the workpiece; the 3D printing system additively manufactures the Nth layer of slice, and the laser shock forging is synchronously performed in the optimal temperature region; the layered contour and the internal complex structures such as the cavity; the pipeline and the cold pipe are cut with laser according to the three-dimensional model of the individual part; the on-line monitoring system 23 monitors the surface performance, shape and dimension of the workpiece; the real-time tracking and feedback system 21 feeds back the data monitored by the on-line monitoring system to the laser beam power adjustment device to automatically compensate the relevant parameters, thereby eliminating the collaborative influence of the 3D printing forming and the synchronous shock forging, improving the surface accuracy of the workpiece and improving the machining efficiency to an extremely large extent. In addition, by cooperation of the computer 16 and the plurality of modules, the error is analyzed for the acquired data to select the optimal working solution to continuously optimize the workpiece until the machining requirements are met or to select the optimal working solution to continuously optimize the formed part until the machining requirements are met.

    [0061] The above embodiments are preferred implementation modes of the present invention, but the implementation modes of the present invention are not limited by the above embodiments. Any other changes, modifications, substitutions, combination and simplifications that are made without departing from the spiritual essence and principle of the present invention shall be equivalent replacements and fall within the protection scope of the present invention.