Composites made of fiber reinforced resin elements joined by adhesive

• US 4,966,802 A
• Filed: 05/16/1989
• Issued: 10/30/1990
• Est. Priority Date: 05/10/1985
• Status: Expired due to Term

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Hertzberg, Paul E.
• Primary Examiner(s): Robinson, Ellis P.
• Assistant Examiner(s): Watkins, III, William P.
• Application Number:
  US07/355,129
• Time in Patent Office: 532 Days
• Field of Search: 428/102, 428/119, 428/120, 428/113, 428/114, 244/132, 244/131, 156/92, 156/93, 112/423, 112/440
• US Class Current: 428/119
• CPC Class Codes: B29C 65/4835 Heat curing adhesives
• CPC Class Codes: B29C 65/601 using extra riveting elements, i.e. the rivets being non-integral with the parts to be joined
• CPC Class Codes: B29C 65/72 by combined operations or combined techniques, e.g. welding and stitching
• CPC Class Codes: B29C 66/112 Single lapped joints
• CPC Class Codes: B29C 66/131 Single flanged joints, i.e. one of the parts to be joined being rigid and flanged in the joint area
• CPC Class Codes: B29C 66/474 said single elements being substantially non-flat
• CPC Class Codes: B29C 66/71 characterised by the composition of the plastics material of the parts to be joined welding bar compositions B29C65/125
• CPC Class Codes: B29C 66/721 Fibre-reinforced materials B29C66/729 takes precedence
• CPC Class Codes: B29C 70/30 Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
• CPC Class Codes: B29D 99/0003 Producing profiled members, e.g. beams
• CPC Class Codes: B29D 99/0014 provided with ridges or ribs, e.g. joined ribs
• CPC Class Codes: B29K 2101/10 Thermosetting resins
• CPC Class Codes: B29K 2105/06 containing reinforcements, fillers or inserts
• CPC Class Codes: B29K 2105/24 crosslinked or vulcanised
• CPC Class Codes: C08J 5/124 using adhesives based on a macromolecular component
• CPC Class Codes: Y02T 50/40 Weight reduction
• CPC Class Codes: Y10T 428/24033 including stitching and discrete fastener[s], coating or bond
• CPC Class Codes: Y10T 428/24124 Fibers
• CPC Class Codes: Y10T 428/24132 including grain, strips, or filamentary elements in different layers or components parallel
• CPC Class Codes: Y10T 428/24174 including sheet or component perpendicular to plane of web or sheet
• CPC Class Codes: Y10T 428/24182 : Inward from edge of web or sheet

Abstract

Fiber reinforced resin composites formed by elements joined by a high shear strength, high fracture toughness adhesive are disclosed. The elements are created in easily produceable cross-sectional shapes such as flat, C-shaped, Z-shaped or T-shaped. When joined, the elements form delamination resistant fiber reinforced resin composites having more complex shapes. The strength of the junctions between a pair of elements, such as a panel and its associated reinforcing members, can be enhanced by fasteners, such as rivets, if desired.

Claims

1. A delamination resistant fiber reinforced resin composite comprising:

a fiber reinforced resin composite panel formed of a lay-up of fiber plies and a resin matrix;

at least one elongate fiber reinforced resin composite reinforcing member formed of a lay-up of fiber plies and a resin matrix; and

a high shear strength, high toughness, thermosetting resin adhesive layer consisting essentially of a thermosetting resin located between juxtaposed surfaces of said fiber reinforced resin composite panel and said fiber reinforced composite reinforcing member for bonding said fiber reinforced resin composite panel to said fiber reinforced resin composite reinforcing member, said thermosetting resin having a higher shear strength and being different from the resin used to form said resin matrix of said fiber reinforced resin composite panel and said fiber reinforced resin composite reinforcing member, said thermosetting resin substantially entirely filling the space between said fiber reinforced resin composite panel and said fiber reinforced composite reinforcing member.

2. A delamination resistant fiber reinforced resin composite as claimed in claim 1, wherein:

said fiber reinforced resin composite reinforcing member has a T-shaped cross-sectional configuration; and

,

the outer surface of the cross member flanges of said T-shaped fiber reinforced resin composite reinforcing member are bonded to said fiber reinforced resin composite panel by said high shear strength, high toughness, thermosetting resin adhesive layer.

3. A delamination resistant fiber reinforced resin composite as claimed in claim 1, wherein:

said fiber reinforced resin composite reinforcing member has an I-shaped cross-sectional configuration; and

,

the outer surface of one of the cross member flanges of said I-shaped fiber reinforced resin composite reinforcing member are bonded to said fiber reinforced resin composite panel by said high shear strength, high toughness strength, thermosetting resin adhesive layer.

4. A delamination resistant fiber reinforced resin composite as claimed in claim 3, wherein:

said I-shaped fiber reinforced resin composite reinforcing member is formed of a pair of back-to-back oriented C-shaped elements each formed of a lay-up of fiber plies and a resin matrix; and

,

said C-shaped elements are bonded together by a second high shear strength, high toughness, thermosetting resin adhesive layer consisting essentially of a thermosetting resin located between the backs of C-shaped elements, said second thermosetting resin being different from the resin used to form said C-shaped elements, said second thermosetting resin substantially entirely filling the space between the backs of said C-shaped elements.

5. A delamination resistant fiber reinforced resin composite as claimed in claim 4, including:

a flat plate formed of a lay-up of fiber plies and a resin matrix, one surface of said flat plate overlying the flanges by said C-shaped elements remote from the flanges bonded to said fiber reinforced resin composite panel; and

,

a third high shear strength, high toughness, thermosetting resin adhesive layer consisting essentially of a thermosetting resin located between said flat plate and said flanges of said C-shaped elements remote from the flanges bonded to said fiber reinforced resin composite panel for bonding said flat plate to said flanges of said C-shaped elements remote from the flanges bonded to said fiber reinforced resin composite panel, said third thermosetting resin being different from the resin used to form said C-shaped elements and said flat plate, said third thermosetting resin substantially entirely filling the space between the flanges of said C-shaped elements and said flat plate.

6. A delamination resistant fiber reinforced resin composite as claimed in claim 5, including mechanical fasteners located in holes passing through said panel and the flanges of said C-shaped elements bonded to said panel.

7. A delamination resistant fiber reinforced resin composite as claimed in claim 1, wherein:

said fiber reinforced resin composite reinforcing member has a generally t-shaped cross-sectional configuration; and

,

the outer surfaces of the cross member flanges of said generally t-shaped fiber reinforced resin composite reinforcing member are bonded to said fiber reinforced resin composite panel by said high shear strength, high toughness, thermosetting resin adhesive layer.

8. A delamination resistant fiber reinforced resin composite as claimed in claim 7, wherein said generally t-shaped fiber reinforced resin composite reinforcing member is formed of two elements, one of said elements having a Z-shaped cross-sectional configuration and the other of said elements having a C-shaped cross-sectional configuration, said C-shaped element lying in the corner created by the center leg and one of the outwardly projecting legs of said Z-shaped element such that the back of said C-shaped element faces the center leg of said C-shaped element and the outer surface of one of the legs of said C-shaped element faces the inner surface of one of the legs of said Z-shaped element;

and, including second and third high shear strength, high toughness, thermosetting resin adhesive layers consisting essentially of a thermosetting resin for bonding the facing surfaces of said C-shaped element to the facing surfaces of said Z-shaped element, the outer surface of the other leg of said C-shaped element lying coplanar with the outer surface of said other leg of said Z-shaped element, the outer surfaces of said other legs of said Z- and C-shaped elements being bonded to said panel by said first high shear strength, high toughness, thermosetting resin adhesive layer, said second and third thermosetting resins being different from the resin used to form said C-shaped and Z-shaped elements, said second and third thermosetting resins substantially entirely filling the space between the facing surfaces of said C-shaped and Z-shaped elements.

9. A delamination resistant fiber reinforced resin composite as claimed in claim 8, including a flat plate located between the outer surface of said one of said legs of said C-shaped element facing the inner surface of said one of said legs of said Z-shaped element;

said third high shear strength, high toughness, thermosetting resin adhesive layer joining said flat plate to said inner surface of said one leg of said Z-shaped element; and

, including a fourth high shear strength, high toughness, thermosetting resin adhesive layer consisting essentially of a thermosetting resin located between said flat plate and said outer surface of said one leg of said C-shaped element for bonding said flat plate to said outer surface of said one leg of said C-shaped element, said fourth thermosetting resin being different from the resin used to form said C-shaped element and said flat plate, said fourth thermosetting resin substantially entirely filling the space between said flat plate and said one leg of said C-shaped element.

10. A delamination resistant fiber reinforced resin composite as claimed in claim 9, including mechanical fasteners extending through holes formed in said fiber reinforced resin composite panel and the legs of said Z-shaped and C-shaped elements bonded to said fiber reinforced resin composite panel by said first high shear strength, high toughness, thermosetting resin adhesive layer.

11. A delamination resistant fiber reinforced resin composite as claimed in claim 1, wherein said fiber reinforced resin composite reinforcing member has a Z-shaped cross-sectional configuration.

12. A delamination resistant fiber reinforced resin composite as claimed in claim 1, wherein said fiber reinforced resin composite reinforcing member has a hat-shaped cross-sectional configuration.

13. A delamination resistant fiber reinforced resin composite as claimed in claim 12, wherein the cross member of said hat-shaped fiber reinforced resin composite reinforcing member is bonded to said panel by said first high shear strength, high toughness, thermosetting resin adhesive layer.

14. A delamination resistant fiber reinforced resin composite as claimed in claim 13, wherein the outwardly projecting legs of said hat-shaped fiber reinforced resin composite reinforcing member are attached to said panel by said high shear strength, high toughness, theremosetting resin adhesive layer.

15. A delamination resistant fiber reinforced resin composite as claimed in claim 1, wherein said fiber reinforced resin composite reinforcing member has a wide U-shaped cross-sectional configuration and wherein the cross member of said wide U-shaped fiber reinforced resin composite reinforcing members are bonded to said panel by said high shear strength, high toughness, thermosetting resin adhesive layer.