Strato streak flush patch

• US 5,023,987 A
• Filed: 05/30/1990
• Issued: 06/18/1991
• Est. Priority Date: 08/28/1989
• Status: Expired due to Fees

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Hartz, Dale E., Swanson, Jerald L., Wuepper, Karl J.
• Primary Examiner(s): Gorski, Joseph M.
• Application Number:
  US07/530,432
• Time in Patent Office: 384 Days
• Field of Search: 29/402.09, 29/402.11, 29/402.12, 29/402.13, 29/402.14, 29/402.15, 29/402.16, 29/402.17, 29/525.1, 29/525.2, 114/227, 114/228, 114/229, 264/36, 52/514, 156/94, 156/98
• US Class Current: 29/402.11
• CPC Class Codes: B23P 6/00 Restoring or reconditioning objects straightening or restoring form of sheet metal, metal rods, metal tubes, metal profiles, or specific articles made therefrom B21D1/00, B21D3/00; repairing defective or damaged objects by casting techniques B22D19/10
• CPC Class Codes: B29C 73/10 using patches sealing on the surface of the article B29C73/14 takes precedence
• CPC Class Codes: B29K 2105/06 containing reinforcements, fillers or inserts
• CPC Class Codes: B29K 2995/0044 Anisotropic
• CPC Class Codes: B64F 5/40 Maintaining or repairing aircraft
• CPC Class Codes: Y10T 29/49734 and removing damaged material
• CPC Class Codes: Y10T 29/49735 Mechanically attaching preform with separate fastener
• CPC Class Codes: Y10T 29/49739 Mechanically attaching preform by separate fastener

Abstract

A method and apparatus for repairing composite skin structures from a blind side. The method includes using an elongated patch with a compression jig to hold the patch in place while the patch is either bonded in place or fixed in place with countersunk fasteners or both. The patch, when used on composite materials, is constructed and positioned so as to have the same anisotropic load-carrying characteristics as does the material to be repaired. A blind side repair can be completely made in the field without requiring extensive facilities.

Claims

1. A field repair method for forming a structural blind patch in a sheet of anisotropic load-bearing material having a known thickness, comprising the steps of:

providing an anisotropic flush patch having a major axis and a minor axis of substantially different dimensions, a filler portion having a thickness equal to the thickness of the material to be patched, and a circumferential backing lip extending from the perimeter of the filler portion so as to form a circumferential shoulder therewith;

providing a grasping member extending from the filler portion;

trimming a damaged area of the material to be patched to the same shape as that of the filler portion, thereby providing a trimmed area having a major axis and a minor axis;

aligning the major axis of the flush patch with the minor axis of the trimmed area;

inserting the minor axis of the flush patch through the major axis of the trimmed area, thereby inserting the patch through the trimmed area;

aligning the filler portion with the trimmed area after the flush patch has been inserted so that the trimmed area is flushly filled by the filler portion, and so that the circumferential shoulder is closely received by the trimmed area, and so that the backing lip abuts the material adjacent to the trimmed area;

fixing the backing lip to the material while holding the flush patch in place with the grasping member; and

removing the grasping member, whereby compressive loads are transferred across the trimmed area through the filler portion and tensile loads are transferred across the trimmed area through the backing lip.

2. The method of claim 1 wherein the sheet of material is a fully cured composite of reinforcing fibers oriented in preselected directions and a binding resin, and wherein the flush patch is a partially cured composite of reinforcing fibers oriented in the same preselected directions and a partially cured binding resin.

3. The method of claim 2, including the step of curing the flush patch in place under temperature and pressure elevated substantially above ambient temperature and pressure.

4. The method of claim 1 wherein the fixing step includes passing blind side fasteners into the backing lip from one side of the material only and wherein the backing lip extends radially at least approximately four times the diameter of the blind side fasteners.

5. The method of claim 4 including prior to the trimming step, positioning a drilling and tracing template, having an interior tracing guide defining the shape to be trimmed and a drilling guide for drilling holes for the fasteners, over the damaged area, whereafter tracing the area to be trimmed using the tracing guide, removing the template, and removing the traced area.

6. The method of claim 5 including the step of repositioning the template around the trimmed area after the inserting step.

7. The method of claim 6 including engaging a compression jig having pulling means for pulling on the grasping member, compression means for pushing against the material to be patched, and positioning means for positively repositioning the template around the trimmed area with the grasping member, the template, and the material to be patched after repositioning the template.

8. The method of claim 7, including the steps of drilling coaxial holes through the material to be patched and the backing lip using the drilling guide, and including the step of positioning and tightening said blind side fasteners in the holes.

9. The method of claim 8 wherein the fixing step includes bonding the flush patch to the material to be patched.

10. The method of claim 1 wherein the flush patch has a body portion integral with the filler portion and the backing lip.