Method for joining a plurality of workpiece parts and joining tool

Abstract

A method is provided for joining a plurality of workpiece parts, in particular body parts, in which: a) the workpiece parts are inserted into a joining tool, b) the workpiece parts in the joining tool are monitored for damages, c) the workpiece parts are joined by the joining tool, and d) the joined workpiece is monitored for damages in the joining tool.

Claims

1. A method for joining a plurality of workpiece parts, the method comprising the steps of: a) inserting the workpiece parts into a joining tool; b) checking the workpiece parts to be joined for damage by a testing device provided in the joining tool while the workpiece parts to be joined are in the joining tool prior to a joining process; c) joining the workpiece parts by the joining tool; and d) checking the joined workpiece for damage by the testing device while the joined workpiece is in the joining tool, wherein the testing device is configured to check both the damage of the workpiece parts to be joined and the damage of the joined workpiece while the workpiece parts prior to the joining process and the joined workpiece are in the joining tool without requiring additional transport steps.

2. The method according to claim 1, wherein the workpiece parts are vehicle body components.

3. The method according to claim 1, wherein the workpiece parts are checked just before the joining and the joined workpiece is checked immediately after the joining.

4. The method according to claim 1, wherein at least one of the plurality of workpiece parts is made of a fiber-reinforced plastic material.

5. The method according to claim 1, wherein when critical damage to one of the workpiece parts or to the joined workpiece is detected, separating out the critically damaged workpiece part or the critically damaged joined workpiece.

6. The method according to claim 1, further comprising the steps of: comparing damage to the workpiece parts before the joining with damage to the joined workpiece after the joining; determining damage caused by the joining of the workpiece parts; and separating-out the joined workpiece if the damage caused by the joining is critical.

7. The method according to claim 1, wherein at least one of the checking steps is carried out via air ultrasound, contact ultrasound, acoustic emission, thermography, and/or another non-destructive method.

8. The method according to claim 1, wherein: the joining tool comprises a die and a die plate, and the workpiece parts are checked for damage when the die is disposed on one of the workpiece parts and/or the joined workpiece is checked for damage when the joining tool is completely closed.

9. The method according to claim 1, wherein: the joining tool comprises a die, and the joining tool checks the workpiece parts for damage when the die is disposed on one of the workpiece parts or is positioned at a distance of less than 3.0 mm from one of the workpiece parts.

10. The method according to claim 8, wherein, before step b), a coupling agent is supplied in an automated manner between the die and one of the workpiece parts.

11. The method according to claim 9, wherein, before step b), a coupling agent is supplied in an automated manner between the die and one of the workpiece parts.

12. The method according to claim 10, wherein, after step d), the coupling agent between the die and the joined workpiece is removed in an automated manner.

13. The method according to claim 11, wherein, after step d), the coupling agent between the die and the joined workpiece is removed in an automated manner.

14. The method according to claim 1, wherein an assessment as to whether damage is critical occurs in an automated manner by comparing samples with one another and/or with a limit sample.

15. The method according to claim 14, wherein the samples, together with information concerning a final product in which the joined workpiece is used, are stored in a database.

16. A joining tool for joining a plurality of workpiece parts made of a fiber-reinforced plastic material, comprising: at least one testing device constructed on one workpiece contact surface of the joining tool, wherein the testing device is configured to check the workpiece parts to be joined for damage while the workpiece parts to be joined are in the joining tool prior to a joining process, and the testing device is configured to check the joined workpiece for damage while the joined workpiece is in the joining tool, wherein the testing device is configured to check both the damage of the workpiece parts to be joined and the damage of the joined workpiece while the workpiece parts prior to the joining process and the joined workpiece are in the joining tool without requiring additional transport steps.

17. The joining tool according to claim 16, wherein the testing device is configured to test via air ultrasound, contact ultrasound, acoustic emission, and/or another non-destructive testing method.

18. The joining tool according to claim 16, wherein the testing device is a phased array ultrasonic probe.

19. The joining tool according to claim 16, wherein the joining tool is a semi-tubular punch riveter having a die and a die plate, the testing device being provided in one or more of the die and the die plate.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is a sectional view of a joining tool according to an embodiment of the invention in the open position;

(2) FIG. 2 is a view of the joining tool according to FIG. 1 with inserted workpiece parts; and

(3) FIG. 3 is a view of the joining tool according to FIG. 1 in the completely closed position.

DETAILED DESCRIPTION OF THE DRAWINGS

(4) FIG. 1 is a schematic sectional view of a joining tool 10 for joining a plurality of workpiece parts, particularly vehicle body components.

(5) The joining tool 10 may be a forming tool, for example, a semi-tubular punch riveter.

(6) The joining tool 10 for joining workpiece parts may also be constructed of fiber-reinforced plastic material.

(7) The joining tool 10 has a die 12 and a die plate 14, the die 12 being displaceable with respect to the die plate 14.

(8) The die 12 has a cylindrical and, for example, hollow construction and is used for guiding a bolt 16 (FIG. 3).

(9) The surface of the die 12 facing the die plate as well as the side of the die plate 14 facing the die 12 form workpiece contact surfaces 20 on which the workpiece parts 22, 24 (FIG. 2) to be joined or the joined workpiece 26 (FIG. 3) come to rest when the joining tool 10 is used.

(10) At least one testing device 28 is provided on the workpiece contact surfaces 20 on the die 12 as well as on the die plate 14.

(11) The testing device 28 is designed for examination by air ultrasound, contact ultrasound, acoustic emission and/or another nondestructive method.

(12) The testing device 28, for example, is a phased array ultrasonic probe.

(13) It is naturally also contemplated for a testing device 28 to be provided only on the die 12 or only on the die plate 14.

(14) In addition, the size, position and/or orientation of the testing devices 28 are the result of the geometry of the workpiece contact surfaces 20 and of the workpiece parts 22, 24 to be examined or of the joining points.

(15) The testing devices 28 are connected with an analysis unit 30, for example, a microprocessor-based control unit of the joining tool 10. This is outlined in the drawings by a broken line.

(16) Together with the analysis unit 30, the testing device 28 can examine the workpiece parts 22, 24 to be joined and/or the joined workpiece 26 for damage.

(17) For joining a plurality of workpieces 22, 24, the workpiece parts 22, 24 to be joined are inserted into the joining tool 10. In this case, at least one of the workpiece parts 22, 24 can be made of a fiber-reinforced plastic material.

(18) A coupling agent (not shown), for example, a contact gel, can now be supplied in an automated manner between the die 12 and one of the workpiece parts 22, 24.

(19) The applied coupling agent can be removed in an automated manner after the joining. The joining tool 10 will now be closed to such an extent that the die 12 is disposed on the workpiece part 22 that is closer to it. This position is illustrated in FIG. 2. In this position, the testing devices 28 now rest against the workpiece parts 22 and 24, respectively, and can test the workpiece parts 22, 24 in the joining tool 10 for damage.

(20) The examination of the workpiece parts 22, 24 therefore takes place just before the joining.

(21) The checking of the workpiece parts 22, 24 and, subsequently, of the joined workpiece 26 takes place by way of air ultrasound, contact ultrasound, acoustic emission, thermography and/or another nondestructive method.

(22) In the event that the testing devices 28 are phased array ultrasonic probes, for example, a sample of the checked workpiece part 22, 24 is obtained by the testing, which can then be transmitted to the analysis unit 30.

(23) The samples of the workpiece parts 22, 24 obtained during the testing are placed in the analysis unit 30.

(24) An assessment as to whether damage, i.e. an irregularity of the workpiece parts 22, 24, is critical may be carried out, for example, in that the obtained sample is compared with a limit sample, which is stored in the memory of the analysis unit 30, and the damage will be considered critical if the obtained sample differs from the corresponding limit sample beyond a defined extent.

(25) This assessment can be carried out by the analysis unit 30 in an automated manner.

(26) When critical damage is detected in the case of one of the workpiece parts 22, 24, this workpiece part 22, 24 will be separated out.

(27) This means that the joining tool 10 is opened up again and the damaged workpiece part 22, 24 is removed and replaced.

(28) When the two workpiece parts 22, 24 have no critical damage, the workpiece parts 22, 24 will be joined by the joining tool 10.

(29) In the illustrated embodiment, a rivet 32 is introduced into the workpiece parts 22, 24 by means of a bolt 16, as shown in FIG. 3.

(30) In this manner, the joined workpiece 26 is obtained which consists of the two workpiece parts 22, 24.

(31) The position of the joining tool 10 illustrated in FIG. 3 corresponds to the completely closed position, in which the joined workpiece 26 is checked for damage by the testing devices 28.

(32) The examination of the joined workpiece 26 therefore takes place immediately after the joining.

(33) The samples obtained during the examination of the joined workpiece 26 can also be transmitted to the analysis unit 30, in which they are compared with a limit sample for joined workpieces, which is stored in the analysis unit 30.

(34) When the sample obtained during the examination deviates excessively from the limit sample, a conclusion is drawn that the damage to the joined workpiece 26 is critical and the joined workpiece 26 is separated out, which means that it will no longer be used.

(35) Also, the samples of the individual workpiece parts 22, 24 can be compared in the analysis unit 30 with the sample of the joined workpiece 26, and a conclusion can be drawn from the differences of the samples as to the damage resulting from the joining.

(36) The comparison of the obtained samples with one another and/or with a limit sample can take place by use of image processing software, in which case the magnitude of the differences between the obtained samples with respect to one another or between the obtained samples and the limit sample can be used for measuring the damage.

(37) If the damage caused during the joining exceeds a predefined limit, the joined workpiece 26 will also be separated out. Particularly, the ratio of magnitudes of the two damage cases with respect to one another can be defined as the limit value.

(38) For example, damage will be considered to be critical when the damage caused by the joining exceeds the magnitude of the initial damage to a critical extent, particularly when the initial damage, classified as non-critical, has increased in its magnitude more than two-fold as a result of the damage caused by the joining.

(39) Typical damages in fiber-reinforced plastic material caused during joining are delamination or inter-fiber failures.

(40) The obtained sample of the joined workpiece 26 can also be stored in the analysis unit 30.

(41) In addition, the obtained sample of the joined workpiece 26 together with the samples of the individual workpiece parts 22, 24 can be stored in a database and can be linked to information concerning the final product in which the joined workpiece 26 was used. The information concerning the product may, for example, be the chassis number of the vehicle in which the joined workpiece 26 was installed, so that, in the event of later claims, the samples of the workpiece parts 22, 24 and of the joined workpiece can be used.

(42) It is naturally also contemplated that the joining tool 10 is a different joining tool than the illustrated semi-tubular punch riveter.

(43) Naturally, also more than the illustrated two workpiece parts can be mutually connected without deviating from the idea of the invention.

(44) It is also contemplated that, in the case of one-sided joining methods, the joining tool 10 checks the workpiece parts 22, 24 for damage when the die 12 is disposed on one of the workpiece parts 22, 24 or is positioned at a distance of less than 3.0 mm from one of the workpiece parts 22, 24.

(45) The foregoing disclosure has been set forth merely to illustrate the invention and is not intended to be limiting. Since modifications of the disclosed embodiments incorporating the spirit and substance of the invention may occur to persons skilled in the art, the invention should be construed to include everything within the scope of the appended claims and equivalents thereof.