Honeycomb spliced multilayer foam core aircraft composite parts and method for making same

• US 4,687,691 A
• Filed: 04/28/1986
• Issued: 08/18/1987
• Est. Priority Date: 04/28/1986
• Status: Expired due to Fees

• Current Assignee: United Technologies Corporation (Rtx Corporation)
• Original Assignee: United Technologies Corporation (Rtx Corporation)
• Inventors: Kay, Bruce F.
• Primary Examiner(s): MASSIE, JEROME W
• Application Number:
  US06/856,896
• Time in Patent Office: 477 Days
• Field of Search: 156/78, 156/303.1, 156/197, 156/307.3, 156/307.7, 156/252, 428/71, 428/73, 428/76, 428/117, 428/315.9, 428/316.6, 428/218, 428/138, 181/288, 181/290, 181/294
• US Class Current: 428/73
• CPC Class Codes: B29C 44/1266 the preformed part being completely encapsulated, e.g. for packaging purposes or as reinforcement
• CPC Class Codes: B29C 44/186 Filling multiple cavities B29C44/181, B29C44/182 and B29C44/188 takes precedence
• CPC Class Codes: B32B 2266/08 Closed cell foam
• CPC Class Codes: B32B 2305/024 Honeycomb
• CPC Class Codes: B32B 2307/718 Weight, e.g. weight per square meter
• CPC Class Codes: B32B 2605/18 Aircraft
• CPC Class Codes: B32B 3/12 characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
• CPC Class Codes: B32B 5/18 characterised by features of a layer of foamed material
• CPC Class Codes: B32B 7/022 Mechanical properties
• CPC Class Codes: B64C 2027/4736 from composite materials
• CPC Class Codes: B64C 27/473 Constructional features
• CPC Class Codes: B64C 3/20 Integral or sandwich constructions
• CPC Class Codes: E04C 2/205 of foamed plastics, or of plastics and foamed plastics, optionally reinforced
• CPC Class Codes: Y10T 156/1056 Perforating lamina
• CPC Class Codes: Y10T 428/236 Honeycomb type cells extend perpendicularly to nonthickness layer
• CPC Class Codes: Y10T 428/239 Complete cover or casing
• CPC Class Codes: Y10T 428/24157 Filled honeycomb cells [e.g., solid substance in cavities, etc.]
• CPC Class Codes: Y10T 428/24331 including nonapertured component
• CPC Class Codes: Y10T 428/24992 Density or compression of components
• CPC Class Codes: Y10T 428/24998 Composite has more than two layers
• CPC Class Codes: Y10T 428/249981 : Plural void-containing components

Abstract

Aircraft composite components having foam cores comprising at least two foam sheets joined with a sheet of honeycomb to form a foam-honeycomb-foam sandwich. The layers of sheet foam are in contact with each other and the honeycomb cells extend a substantially equal depth into and generally perpendicular to the sheet foam layers. The composite component has increased shear strength. The aircraft composite component can be made by aligning a layer of honeycomb between and generally perpendicular to two layers of sheet foam. A compressive force is applied generally perpendicular to at least one layer of sheet foam so that the honeycomb cells penetrate each of the two layers of sheet foam to a substantially equal depth so that the layers of foam contact each other to form a foam-honeycomb-foam sandwich. The foam core is surrounded by resin impregnated fibers and cured.

Claims

1. Aircraft composite components, comprising a composite skin surrounding a foam core wherein the improvement comprises:

a. said foam core comprising alternating layers of at least two layers of sheet foam and at least one layer of honeycomb having cells;

b. said honeycomb layer having a greater compressive strength than said layers of sheet foam;

c. said layers of sheet foam having substantially equal compressive strength;

d. said layers of sheet foam in contact with each other at least through each of the honeycomb openings; and

e. said layer of honeycomb cells extending a substantially equal depth into and generally perpendicular to each of said two layers of sheet foam but not penetrating entirely through said sheet foam layers to form a foam-honeycomb-foam sandwich;

wherein the composite component has increased shear strength.

2. The aircraft composite components as recited in claim 1 wherein said sheet foam is about 0.4 inch to about 4 inches in thickness and said cells are about 0.0625 inch to about 1 inch in thickness and said layer of honeycomb cells extend a depth of about 0.2 inch to about 1 inch into each of said two layers of sheet foam.

6. The aircraft composite component of claim 1 wherein said layers of sheet foam are adhesively bonded together.

3. A method of making an aircraft composite component comprising joining at least two foam sheets to make a foam core, surrounding the foam core with resin impregnated fibers, and curing said resin impregnated fibers wherein the improvement comprises joining said foam sheets by

a. aligning a layer of honeycomb having cells so that said cells are between and generally perpendicular to two layers of sheet foam, and said honeycomb cells having a compressive strength greater than that of the sheet foam;

and

b. applying a compressive force generally perpendicular to at least one layer of sheet foam so that the honeycomb cells pentrate each of the two layers of sheet foam to a substantially equal depth where said layers of foam contact each other at least through each of the honeycomb openings to form a foam-honeycomb-foam sandwich said honeycomb not penetrating entirely through said foam sheets;

resulting in a composite component that has increased shear strength in comparison to adhesively bonded foam sheets.

4. The method of making an aircraft composite component as recited in claim 3 wherein said layer of honeycomb is about 0.0625 inch to about 1 inch in thickness and said layer of sheet foam is about 0.4 inch to about 4 inches in thickness and said honeycomb cells penetrate each of said layers of sheet foam to a substantially equal depth of about 0.2 inch to about 1 inch.

7. The method of making an aircraft composite component of claim 3 wherein said two layers of sheet foam are adhesively bonded together.

5. A method of making an aircraft composite component comprising joining at least two foam sheets to make a foam core, surrounding the foam core with resin impregnated fibers, and curing said resin impregnated fibers wherein the improvement comprises joining said foam sheets by

a. aligning a layer of honeycomb having cells so that the cells are generally perpendicular to a first layer of sheet foam;

b. applying a compressive force generally perpendicular to said layer of sheet foam so that the honeycomb cells penetrate said layer of sheet foam;

c. aligning a second layer of sheet foam, having a compressive strength substantially less than said first layer, generally perpendicular so said layer of honeycomb against said honeycomb layer'"'"'s exposed side; and

d. applying a compressive strength generally perpendicular to at least one layer of sheet foam so that the honeycomb cells penetrate said layers of sheet foam to a depth where said layers of foam contact each other at least through each of the honeycomb openings to form a foam-honeycomb-foam sandwich said honeycomb not in contact with said resin impregnated fibers;

resulting in a composite component that has increased shear strength.

8. The method of making an aircraft composite component of claim 5 wherein said two layers of sheet foam are adhesively bonded together.

9. Aircraft composite comopnents, comprising a composite skin surrounding foam core wherein the improvement comprises:

a. said foam core comprising alternating layers of at least two layers of sheet foam and at least one layer of honeycomb having cells;

b. said honeycomb layer having a greater compressive strength than said layers of sheet foam;

c. said layers of sheet foam in contact with each other at least through each of the honeycomb openings; and

d. said layer of honeycomb cells extending into and generally perpendicular to each of said two layers of sheet foam but not penetrating entirely through said sheet foam layer to form a foam-honeycomb-foam sandwich;

wherein the composite component has increased shear strength.

10. The aircraft composite component as recited in claim 9 wherein said layers of sheet foam are adhesively bonded together.