Method for automated installation of semi-tubular fastener rivets

Patent metadata

Field	Value
Publication number	US-11453044-B2
Application number	US-202117502668-A
Country	US
Kind code	B2
Filing date	Oct 15, 2021
Priority date	Oct 29, 2019
Publication date	Sep 27, 2022
Grant date	Sep 27, 2022

Abstract

A method for automated installation of a semi-tubular fastener rivet is provided. The method includes controlling a numerical control drilling and riveting machine having an upper head and a lower head, to control movement of a lower pressure bushing, to apply a clamping force to hold a workpiece against an upper pressure bushing. The method includes controlling an upper drill spindle on the upper head, to drill a rivet-receiving hole from an upper side of the workpiece and to countersink the rivet-receiving hole. The method includes controlling a lower drill spindle on the lower head, to countersink the rivet-receiving hole from a lower side of the workpiece. The method includes controlling movement of an upper anvil from a retracted position to an installation position, and controlling movement of a lower anvil, to apply an upset force to a tail portion of the semi-tubular fastener rivet installed in the rivet-receiving hole.

First claim

What is claimed is:

1. A method for automated installation of a semi-tubular fastener rivet, the method comprising:
controlling, using a controller of a control system, a numerical control drilling and riveting machine having an upper head and a lower head, to position a workpiece in the numerical control drilling and riveting machine, to control movement of a lower pressure bushing on the lower head, and to apply a clamping force to hold the workpiece against an upper pressure bushing on the upper head;
controlling, using the controller, an upper drill spindle on the upper head, to drill a rivet-receiving hole from an upper side of the workpiece and to countersink the rivet-receiving hole, to obtain an upper countersink of the rivet-receiving hole;
controlling, using the controller, a lower drill spindle on the lower head, to countersink the rivet-receiving hole from a lower side of the workpiece, to obtain a lower countersink of the rivet-receiving hole;
controlling, using the controller, movement of an upper anvil on the upper head from a retracted position to an installation position, in which the upper anvil is aligned to insert the semi-tubular fastener rivet in the rivet-receiving hole; and
controlling, using the controller, movement of a lower anvil, to apply an upset force to a tail portion of the semi-tubular fastener rivet installed in the rivet-receiving hole, the controller monitoring a load cell for providing a signal indicative of a level of the upset force applied by the lower anvil,
wherein the controller is configured to control movement of the lower anvil to apply the upset force to the tail portion of the semi-tubular fastener rivet installed in the rivet-receiving hole, without exceeding a predetermined upset force, and
wherein the controller is configured to direct movement of a nose of the lower anvil within the lower countersink of the rivet-receiving hole to a nominal distance beyond a lower surface plane of a lower surface on the lower side of the workpiece, such that the nose of the lower anvil applies the upset force to the tail portion of the semi-tubular fastener rivet and forms a predetermined flare contour in the tail portion within the lower countersink, and such that the predetermined flare contour is beneath the lower surface of the workpiece.

2. The method of claim 1 , further comprising, prior to controlling movement of the lower anvil,
obtaining a measurement of a distance between the upper pressure bushing and the lower pressure bushing, representing a workpiece thickness, and determining, via the controller, the workpiece thickness within which a zone constraint is defined by the controller for limiting travel of the lower anvil, to avoid collision with the workpiece,
wherein the controller is configured to direct movement beyond the zone constraint of the nose of the lower anvil into the lower countersink of the rivet-receiving hole, to apply the upset force to the tail portion of the semi-tubular fastener rivet, such that the lower anvil causes flaring of the tail portion within the lower countersink of the rivet-receiving hole.

3. The method of claim 1 , wherein controlling movement of the lower anvil further comprises,
using a contoured rivet die with the lower anvil, the contoured rivet die being configured to form the predetermined flare contour comprising a generally trumpet-shaped flare contour in the tail portion of the semi-tubular fastener rivet.

4. The method of claim 1 , wherein controlling the numerical control drilling and riveting machine, to control movement of the lower pressure bushing on the lower head, to apply the clamping force to hold the workpiece against the upper pressure bushing on the upper head further comprises,
controlling the numerical control drilling and riveting machine, to control movement of the lower pressure bushing on the lower head, to apply the clamping force to hold the workpiece comprising a composite workpiece.

5. The method of claim 1 , wherein controlling the numerical control drilling and riveting machine, to control movement of the lower pressure bushing on the lower head, to apply the clamping force to hold the workpiece against the upper pressure bushing on the upper head further comprises,
controlling the numerical control drilling and riveting machine, to control movement of the lower pressure bushing on the lower head, to apply the clamping force to hold the workpiece comprising a first composite aircraft component and a second composite aircraft component fastened together.

6. The method of claim 1 , wherein controlling the numerical control drilling and riveting machine, to control movement of the lower pressure bushing on the lower head, to apply the clamping force to hold the workpiece against the upper pressure bushing on the upper head further comprises,
controlling the numerical control drilling and riveting machine, to control movement of the lower pressure bushing on the lower head, to apply the clamping force to hold the workpiece comprising an aircraft trailing-edge control surface comprised of a first composite aircraft component fastened to a second composite aircraft component.

7. The method of claim 1 , wherein controlling the upper drill spindle to drill the rivet-receiving hole further comprises,
controlling the upper drill spindle to drill the rivet-receiving hole comprising a clearance fit rivet-receiving hole.

8. The method of claim 1 , wherein controlling the lower drill spindle to countersink the rivet-receiving hole, to obtain the lower countersink further comprises,
controlling the lower drill spindle to counterbore the rivet-receiving hole from the lower side of the workpiece, to obtain a counterbored countersink.

9. The method of claim 1 , wherein controlling movement of the upper anvil, in which the upper anvil is aligned to insert the semi-tubular fastener rivet in the rivet-receiving hole further comprises,
controlling movement of the upper anvil, in which the upper anvil is aligned to insert the semi-tubular fastener rivet comprising a head portion that is positioned in the upper countersink and is substantially flush with an upper surface plane of an upper surface on the upper side of the workpiece, when the semi-tubular fastener rivet is installed in the rivet-receiving hole.

10. The method of claim 1 , wherein controlling movement of the upper anvil, in which the upper anvil is aligned to insert the semi-tubular fastener rivet in the rivet-receiving hole further comprises,
controlling movement of the upper anvil, in which the upper anvil is aligned to insert the semi-tubular fastener rivet comprising a titanium semi-tubular fastener rivet.

11. A method for automated installation of a semi-tubular fastener rivet, the method comprising:
controlling, using a controller, a numerical control drilling and riveting machine having an upper head and a lower head, to control movement of a lower pressure bushing on the lower head, to apply a clamping force to hold a composite workpiece against an upper pressure bushing on the upper head;
controlling, using the controller, an upper drill spindle on the upper head, to drill a rivet-receiving hole from an upper side of the composite workpiece and to countersink the rivet-receiving hole, to obtain an upper countersink of the rivet-receiving hole;
controlling, using the controller, a lower drill spindle on the lower head, to countersink the rivet-receiving hole from a lower side of the composite workpiece, to obtain a lower countersink of the rivet-receiving hole;
controlling, using the controller, movement of an upper anvil on the upper head from a retracted position to an installation position, in which the upper anvi

Assignees

• Boeing Co

Inventors

• Kuldell Kip R
• Schaefer Christian E
• Kilwin Jeffrey J
• Goddard Tony S
• Burns Thomas E
• Darlak Eugene T
• Foore Jeffrey L

Classifications

• B23B39/22

  with working-spindles in opposite headstocks · CPC title

• B21J15/142

  Aerospace structures · CPC title

• B21J15/285

  for controlling the rivet upset cycle · CPC title

• B21J15/50

  Removing or cutting devices for rivets · CPC title

• B21J15/14

  specially adapted for riveting specific articles, e.g. brake lining machines · CPC title