Apparatus and methods for bonding laminate structures

US9610728B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9610728-B2
Application numberUS-201414335426-A
CountryUS
Kind codeB2
Filing dateJul 18, 2014
Priority dateJul 18, 2014
Publication dateApr 4, 2017
Grant dateApr 4, 2017

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A composite laminate reinforcing tool may be used to form a reinforced joint at a bond line of a composite laminate structure. The tool may hold one or more clips having posts, and the tool may be positioned along the bond line between at least two composite laminate elements. Joint sections of the clip may be heated to increase a pliability of the joint section, and the tool may be actuated to drive the post through the at least two composite laminate elements. The posts, may deflect toward a base of the clip, thereby to seat the clip. The reinforced composite laminate structure may then be cured.

First claim

Opening claim text (preview).

What is claimed is: 1. A method for forming a reinforced joint at a bond line in a composite laminate structure, the method comprising: loading a composite laminate reinforcing tool with a clip, having a first post coupled to a base at a first joint section between the first post and the base, the first post extending at an initial angle relative to the base and defining a first-post inner surface, facing toward the base, and a first-post outer surface, facing away from the base, the first-post outer surface comprising an inwardly tapered section at a tip of the first post; positioning the composite laminate reinforcing tool along the bond line between at least two composite laminate elements; heating the first joint section sufficiently above an ambient temperature to increase a pliability of the first joint section; actuating the composite laminate reinforcing tool so that the first post pierces through the at least two composite laminate elements; and while the first joint section is heated above the ambient temperature and as the first post pierces through the at least two composite laminate elements, engaging the tapered section of the first-post outer surface with a backing surface to deflect the first post toward the base at the first joint section until the first post extends at a deflected angle relative to the base, the deflected angle being different from the initial angle, thereby to seat the clip. 2. The method of claim 1 , in which: the clip further comprises a second post, coupled to the base at a second joint section between the second post and the base, the second post extending at a second initial angle relative to the base and defining a second-post inner surface, facing toward the base, and a second-post outer surface, facing away from the base, the second-post outer surface comprising an inwardly tapered section at a tip of the second post; heating the joint section comprises heating the first and second joint sections sufficiently above the ambient temperature to increase pliability of the first and second joint sections; actuating the composite laminate reinforcing tool comprises driving the first and second posts through the at least two composite laminate elements; and deflecting the post comprises, while the first and second joint sections are heated above the ambient temperature and as the first and second posts are driven through the at least two composite elements, engaging the tapered section of the first-post outer surface and the tapered section of the second-post outer surface with a backing surface to deflect the first and second posts at the first and second joint sections, respectively, until the first and second posts extend at first and second deflected angles relative to the base, the first and second deflected angles being different from the first and second initial angles, respectively. 3. The method of claim 1 , in which the clip is formed of a clip material, selected from a group of clip materials consisting of uni-directional fiber reinforced thermoplastic, non-oriented chopped fiber thermoplastic, and neat thermoplastic resin. 4. The method of claim 1 , in which a plurality of clips is loaded into the composite laminate reinforcing tool and driven into the bond line. 5. The method of claim 4 , further comprising coupling adjacent pairs of the plurality of clips with a link. 6. The method of claim 1 , in which the initial angle is approximately 90 degrees. 7. The method of claim 1 , in which the composite laminate reinforcing tool comprises a plunger head positioned to engage a base of the clip, and in which heating the first joint section comprises heating the plunger head. 8. The method of claim 7 , in which the plunger head is movable from a retracted position to an extended position, and in which actuating the composite laminate reinforcing tool comprises actuating the plunger head from the retracted position to the extended position. 9. The method of claim 1 , in which at least one of the at least two composite laminate elements comprises a pre-impregnated laminate element. 10. The method of claim 1 , further comprising, after deflecting the first post, heating the clip that was seated and the at least two composite laminate elements to cure the composite laminate structure. 11. A method for forming a reinforced joint at a bond line in a composite laminate structure, comprising: loading a composite laminate reinforcing tool with a plurality of clips, each of the plurality of clips having a first post, coupled to a base at a first joint section between the first post and the base, and a second post coupled to the base at a second joint section between the second post and the base, the first and second posts extending at first and second initial angles, respectively, relative to the base, the first and second initial angles being approximately 90 degrees so that each of the plurality of clips has a U-shape, the first post defining a first-post inner surface, facing toward the base, and a first-post outer surface, facing away from the base, with the first-post outer surface comprising an inwardly tapered section at a tip of the first post, and the second post defining a second-post inner surface, facing toward the base, and a second-post outer surface, facing away from the base, with the second-post outer surface comprising an inwardly tapered section at a tip of the second post; positioning the composite laminate reinforcing tool along the bond line between at least two composite laminate elements; heating the first and second joint sections of a selected one of the plurality of clips sufficiently above an ambient temperature to increase a pliability of the first and second joint sections; actuating the composite laminate reinforcing tool so that the first and second posts of the selected one of the plurality of clips pierce through the at least two composite laminate elements; and while the first and second joint sections are heated above the ambient temperature and as the first and second posts pierce through the at least two composite laminate elements, engaging the tapered section of the first-post outer surface and the tapered section of the second-post outer surface with a backing surface to deflect the first and second posts of the selected one of the plurality of clips toward the base at the first and second joint sections, respectively, until the first and second posts extend at first and second deflected angles relative to the base, the first and second deflected angles being different from the first and second initial angles, respectively, thereby to seat the selected one of the plurality of clips. 12. The method of claim 11 , further comprising coupling adjacent pairs of the plurality of clips with a link. 13. The method of claim 11 , in which each of the plurality of clips is formed of a clip material, selected from a group of clip materials consisting of uni-directional fiber reinforced thermoplastic, non-oriented chopped fiber thermoplastic, and neat thermoplastic resin. 14. The method of claim 11 , in which the composite laminate reinforcing tool comprises a plunger head, positioned to engage a base of the clip, and in which heating the first and second joint sections of the selected one of the plurality of clips comprises heating the plunger head. 15. The method of claim 14 , in which the plunger head is movable from a retracted position to an extended position, and in which actuating the composite laminate reinforcing tool comprises actuating the plunger head from the retracted position to the extended position. 16. The method of cl

Assignees

Inventors

Classifications

  • Other pressure application arrangements · CPC title

  • Fibre-reinforced materials (B29C66/729 takes precedence) · CPC title

  • to metals or their alloys · CPC title

  • being hollow-walled or honeycombs · CPC title

  • Single lap to lap joints, i.e. overlap joints (B29C66/45, B29C66/472, B29C66/52272 take precedence) · CPC title

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What does patent US9610728B2 cover?
A composite laminate reinforcing tool may be used to form a reinforced joint at a bond line of a composite laminate structure. The tool may hold one or more clips having posts, and the tool may be positioned along the bond line between at least two composite laminate elements. Joint sections of the clip may be heated to increase a pliability of the joint section, and the tool may be actuated to…
Who is the assignee on this patent?
Boeing Co
What technology area does this patent fall under?
Primary CPC classification B29C65/562. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Apr 04 2017 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 2 related publications on this page (citations in our corpus or others sharing the same primary CPC).