Offset collar delivery for swage tools

Patent metadata

Field	Value
Publication number	US-11033952-B2
Application number	US-201816140174-A
Country	US
Kind code	B2
Filing date	Sep 24, 2018
Priority date	Sep 24, 2018
Publication date	Jun 15, 2021
Grant date	Jun 15, 2021

Abstract

Systems and methods are provided for fastening via a swage tool. One embodiment is a method for fastening via a swage tool, the method including selecting a hole located at a part; aligning an axis of a lockbolt collar with a center of the hole; placing the lockbolt collar flush against the part at a first end of the hole; and swaging the lockbolt collar onto a lockbolt that has been driven through the hole.

First claim

What is claimed is:

1. A method comprising:
selecting a hole located at a part;
transporting a lockbolt collar through a collar arm;
transferring the lockbolt collar from the collar arm to fingers at a swage nose;
retracting the collar arm from the fingers while the fingers grip the lockbolt collar;
aligning an axis of the lockbolt collar with a center of the hole;
placing the lockbolt collar flush against the part at a first end of the hole prior to inserting a lockbolt through the hole;
driving the lockbolt through the hole and the lockbolt collar from a second end of the hole while the lockbolt collar is flush against the part; and
swaging the lockbolt collar onto the lockbolt after the lockbolt has been driven through the hole and the lockbolt collar, wherein direct contact of the swage nose against the fingers during the swaging causes the fingers to swing away from the lockbolt collar.

2. The method of claim 1 wherein:
aligning the axis of the lockbolt collar and the center of the hole comprises intersecting the axis and the center at an Inner Mold Line (IML) of the part.

3. The method of claim 1 further comprising:
driving the lockbolt causes the axis of the lockbolt collar to become collinear with the center of the hole and the lockbolt.

4. The method of claim 1 wherein:
swaging the lockbolt collar causes the lockbolt collar to engage an engagement feature on a pin of the lockbolt.

5. The method of claim 1 further comprising:
holding the lockbolt collar for placement via the fingers.

6. The method of claim 5 further comprising:
resting a flange of the lockbolt collar upon the fingers.

7. The method of claim 5 further comprising:
overlapping the fingers with a flange at the lockbolt collar to seat the lockbolt collar at the fingers.

8. The method of claim 5 wherein:
a motion of the swage nose against inclined ramps of the fingers causes the fingers to swing about hinges away from the lockbolt collar.

9. The method of claim 1 wherein:
aligning the axis of the lockbolt collar with the center of the hole is based on feedback provided by a sensor system, wherein the feedback is based on information acquired from components selected from the group consisting of: a camera system, a laser sensor, an ultrasonic sensor, and a light detection and ranging scanner.

10. The method of claim 9 wherein:
the fingers swing about hinges.

11. The method of claim 1 further comprising:
holding the lockbolt collar flush against the part by pressing a swage nose against the lockbolt collar.

12. The method of claim 1 further comprising:
reorienting the lockbolt collar as the lockbolt collar proceeds through the collar arm.

13. The method of claim 1 further comprising:
aligning an axis of the lockbolt collar to intersect the center of the hole at an Inner Mold Line (IML) surface of the part.

14. The method of claim 1 further comprising:
inserting the lockbolt in one motion through the lockbolt collar and the hole.

15. The method of claim 1 wherein:
the first end of the hole is located at an Inner Mold Line (IML) of the part; and
the second end of the hole is located at an Outer Mold Line (OML) of the part.

16. The method of claim 1 wherein:
swaging the lockbolt collar comprises gripping a pintail of the lockbolt.

17. The method of claim 1 wherein:
the part is a component of an aircraft.

18. The method of claim 1 further comprising:
operating a vacuum system to remove debris around the hole.

19. The method of claim 18 wherein:
removing the debris comprises removing particles that were generated by drilling the hole.

20. The method of claim 18 wherein:
removing the debris comprises removing a pintail of the lockbolt collar.

21. A non-transitory computer readable medium embodying programmed instructions which, when executed by a processor, are operable for performing a method comprising:
selecting a hole located at a part;
transporting a lockbolt collar through a collar arm;
transferring the lockbolt collar from the collar arm to fingers at a swage nose;
retracting the collar arm from the fingers while the fingers grip the lockbolt collar;
aligning an axis of the lockbolt collar with a center of the hole;
placing the lockbolt collar flush against the part at a first end of the hole prior to inserting a lockbolt through the hole;
driving the lockbolt through the hole and the lockbolt collar from a second end while the lockbolt collar is flush against the part; and
swaging the lockbolt collar onto the lockbolt after the lockbolt has been driven through the hole and the lockbolt collar, wherein direct contact of the swage nose against the fingers during the swaging causes the fingers to swing away from the lockbolt collar.

Assignees

• Boeing Co

Inventors

• Chan Kwok Tung
• Sisco Tanni
• Devlin Jeff
• Elmore Brendan

Classifications

• B21J15/38

  Accessories for use in connection with riveting, e.g. pliers for upsetting; Hand tools for riveting · CPC title

• B21J15/32 Primary

  Devices for inserting or holding rivets in position with or without feeding arrangements · CPC title

• B21J15/12

  with tools or tool parts having a movement additional to the feed movement, e.g. spin {(B21J15/027 takes precedence)} · CPC title

• B21J15/022 Primary

  Setting rivets by means of swaged-on locking collars, e.g. lockbolts · CPC title

• F16B19/05

  Bolts fastening by swaged-on collars (F16B19/08 takes precedence) · CPC title