Collar positioning system

Patent metadata

Field	Value
Publication number	US-10926316-B2
Application number	US-201815923297-A
Country	US
Kind code	B2
Filing date	Mar 16, 2018
Priority date	Mar 16, 2018
Publication date	Feb 23, 2021
Grant date	Feb 23, 2021

Abstract

A method and system for installing a fastener system. A collar in the fastener system is automatically positioned on a hole on a first side of a structure prior to an insertion of a pin in the fastener system into the hole from a second side of the structure in which the pin has a pin tail. The pin with the pin tail is inserted through the collar in which the pin extends through the hole and the collar. A force is applied on at least one of the collar or the pin tail along a centerline extending centrally though the collar until the pin tail becomes separated from the pin such that the collar engages an engagement feature on the pin when the pin with pin tail is inserted into the hole from the second side.

First claim

What is claimed is:

1. A method for installing a fastener system, the method comprising:
automatically positioning, by an inner mold line machine, a collar of the fastener system on a hole on a first side of a structure prior to an insertion of a pin of the fastener system into the hole from a second side of the structure in which the pin has a pin tail, wherein the collar of the fastener system is positioned on the hole when the collar is concentrically aligned with the hole on the first side of the structure, wherein positioning the collar of the fastener system on the hole on the first side of the structure prior to the insertion of the pin of the fastener system into the hole enables installing the collar on the pin in the hole when the hole deviates from normal with respect to a surface of the structure, automatically positioning the collar of the fastener system on the hole on the first side of the structure comprising:
holding the collar in a collar holder in a swage assembly of the inner mold line machine;
identifying a location of the hole on the first side using a sensor system of the inner mold line machine; and
moving the swage assembly such that the collar held by the collar holder is positioned on the hole on the first side of the structure prior to the insertion of the pin with the pin tail into the hole from the second side;

inserting the pin with the pin tail through the collar, by an outer mold line machine, in which the pin extends through the hole and the collar, wherein the outer mold line machine is moveable across the second side of the structure independently of the inner mold line machine; and
applying a force on at least one of the collar or the pin tail along a centerline extending centrally though the collar until the pin tail becomes separated from the pin such that the collar engages an engagement feature on the pin when the pin with pin tail is inserted into the hole from the second side.

2. The method of claim 1 , wherein the inserting step comprises:
inserting the pin with the pin tail through the hole and the collar in a single motion, wherein the pin extends through the hole and the collar.

3. The method of claim 1 , wherein automatically positioning the collar on the hole on the first side of the structure prior to the insertion of the pin into the hole from the second side further comprises:
normalizing the collar to the first side by positioning the collar with the swage assembly.

4. The method of claim 1 wherein the sensor system includes a camera system and a laser range finder.

5. The method of claim 1 further comprising:
inserting the pin with the pin tail into the hole from the second side after the collar is positioned on the hole on the first side of the structure.

6. The method of claim 1 , wherein the swage assembly is an offset swage assembly such that the collar holder is offset from a rotation axis of the inner mold line machine.

7. The method of claim 1 , wherein the first side is an inner mold line side and the automatically positioning step and the applying step are performed by a swage assembly for an inner mold line machine.

8. The method of claim 7 , wherein the inner mold line machine is selected from a group comprising a flex track crawler and a robotic arm.

9. The method of claim 1 , wherein the structure is selected from a group comprising a metal structure, a composite structure, a metal and composite work piece, a splice, a butt splice, and a splice for two fuselage sections.

10. The method of claim 1 further comprising:
drilling the hole into the structure by the outer mold line machine through the second side.

11. The method of claim 1 further comprising:
removing debris from around the hole by a vacuum system of the inner mold line machine.

12. The method of claim 11 further comprising:
moving the vacuum system away from the hole such that a sensor of the sensor system has a line of sight to the hole.

13. The method of claim 12 further comprising:
maintaining the sensor in a stationary elevation within the inner mold line machine.

14. The method of claim 1 further comprising:
detecting a distance from a laser sensor of the sensor system to the first side; and
generating an image of the hole using a camera of the sensor system.

15. The method of claim 14 , wherein the camera maintains a greater distance from the first side than a distance of the collar holder to the first side during all operations of the inner mold line machine including while generating the image and during automatically positioning the collar of the fastener system on the hole.

16. The method of claim 1 further comprising:
rotating the swage assembly within the inner mold line machine to position the swage assembly over the hole.

17. The method of claim 1 further comprising:
removing the pin tail using a vacuum system of the inner mold line machine after the pin tail becomes separated from the pin.

18. A method for installing a fastener system, the method comprising:
drilling a hole into a structure through a second side of the structure by an outer mold line machine;
removing debris from around the hole by a vacuum system of an inner mold line machine;
automatically positioning, by the inner mold line machine, a collar of the fastener system on a hole on a first side of a structure prior to an insertion of a pin of the fastener system into the hole from a second side of the structure in which the pin has a pin tail, wherein the collar of the fastener system is positioned on the hole when the collar is concentrically aligned with the hole on the first side of the structure, wherein positioning the collar of the fastener system on the hole on the first side of the structure prior to the insertion of the pin of the fastener system into the hole enables installing the collar on the pin in the hole when the hole deviates from normal with respect to a surface of the structure, automatically positioning the collar of the fastener system on the hole on the first side of the structure comprising:
holding the collar in a collar holder in a swage assembly of the inner mold line machine;
identifying a location of the hole on the first side using a sensor system of the inner mold line machine; and
moving the swage assembly such that the collar held by the collar holder is positioned on the hole on the first side of the structure prior to the insertion of the pin with the pin tail into the hole from the second side;

inserting the pin with the pin tail through the collar, by the outer mold line machine, in which the pin extends through the hole and the collar, wherein the outer mold line machine is moveable across the second side of the structure independently of the inner mold line machine; and
applying a force on at least one of the collar or the pin tail along a centerline extending centrally through the collar until the pin tail becomes separated from the pin such that the collar engages an engagement feature on the pin when the pin with pin tail is inserted into the hole from the second side.

19. The method of claim 18 further comprising:
removing the pin tail using the vacuum system of the inner mold line machine after the pin tail becomes separated from the pin.

20. The method of claim 18 , wherein the inserting step comprises:
inserting the pin with the pin tail through the hole and the collar in a single motion, wherein the pin extends through the hole and the collar.

Assignees

• Boeing Co

Inventors

• Chan Kwok Tung
• Sisco Tanni
• Reid Eric M
• Devlin Jeffrey Martin
• Jenkins Skye Sutherland

Classifications

• B23P19/007 Primary

  Picking-up and placing mechanisms · CPC title

• B23P19/003

  Escapement mechanisms used therewith · CPC title

• B23P19/06

  Screw or nut setting or loosening machines · CPC title

• B21J15/022 Primary

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

• F16B5/04

  by means of riveting (rivets F16B19/04) · CPC title