High strength composite structure

• US 4,012,549 A
• Filed: 10/10/1974
• Issued: 03/15/1977
• Est. Priority Date: 10/10/1974
• Status: Expired due to Term

• Current Assignee: General Dynamics Corporation
• Original Assignee: General Dynamics Corporation
• Inventors: Slysh, Paul
• Primary Examiner(s): Lesmes, George F.
• Assistant Examiner(s): Epstein, Henry F.
• Application Number:
  US05/513,661
• Time in Patent Office: 887 Days
• Field of Search: 52/81, 52/82, 52/630, 52/729, 52/730, 52/732, 244/119, 244/129 R, 244/131, 244/133, 428/63, 428/163, 428/167, 428/268, 428/417, 428/418, 428/902, 428/911, 428/116, 428/119, 428/178, 428/179
• US Class Current: 428/116
• CPC Class Codes: B64C 1/08 Geodetic or other open-frame structures
• CPC Class Codes: E04C 2/38 with attached ribs, flanges, or the like, e.g. framed panels concerned with attaching to other panels or elements to form a structure, see the places for the relevant structure, e.g. E04B2/00
• CPC Class Codes: Y10S 273/23 High modulus filaments
• CPC Class Codes: Y10S 428/902 High modulus filament or fiber
• CPC Class Codes: Y10T 428/24149 Honeycomb-like
• CPC Class Codes: Y10T 428/24174 including sheet or component perpendicular to plane of web or sheet
• CPC Class Codes: Y10T 428/2457 Parallel ribs and/or grooves
• CPC Class Codes: Y10T 428/24661 Forming, or cooperating to form cells
• CPC Class Codes: Y10T 428/24669 Aligned or parallel nonplanarities

Abstract

An isogrid structure having inset strips of composite materials at the top and bottom of the grid webs. A preferably flanged isogrid basically consists of I-beam members arranged in an integral repeating pattern of substantially equilateral triangles. One flange may be integral with a skin sheet covering the structure. At least some of these flanges are provided with grooves running parallel to the beam webs, filled with advanced composite materials comprising high-strength fibers in a supporting matrix. Preferably, the fibers run parallel to the beam webs. Preferred arrangements of the fibers are described.

Claims

1. A composite structure comprising:

a skin sheet;

a uniform repeating triangular pattern of first upstanding ribs integral with said skin, across at least a portion of said skin;

a circular node at each corner of each triangle surrounded by a circular second rib;

each of said first and second ribs having a narrow first flange along the upper edge, lying substantially parallel to said skin and a narrow second flange formed by a thickened portion of said skin adjacent to said first and second ribs, whereby said first and second ribs have a substantially I-beam cross-section;

a groove in the outer surface of each flange on said first ribs filled with a composite material strip comprising high-strength fibers embedded in a supporting matrix;

said fibers being oriented substantially parallel to each other and to the supporting first rib, at least some of said fibers extending inwardly of said second rib at each node; and

said fiber strips being tapered at each end to a lesser cross-sectioned fiber density.

2. The structure according to claim 1 where said strip has a cross-section width-to-thickness ratio of at least 7 to 1.

3. The structure according to claim 1 wherein said strip comprises a plurality of fiber layers, each layer comprising a single layer of parallel contiguous fibers, said layers ending at different distances from said node to provide said taper.

4. The structure according to claim 1 wherein said fibers have a Young'"'"'s modulus of at least about 20 ×

10⁶ psi and tensile strength of at least about 300,000 psi.

5. The structure according to claim 4 wherein said fibers are selected from the group consisting of boron fibers, graphite fibers and mixtures thereof.

6. The structure according to claim 1 wherein said matrix material is selected from the group consisting of epoxy resins, polyester resins, aluminum and mixtures and combinations thereof.

7. In an isogrid structure comprising:

a uniform repeating triangular pattern of first upstanding ribs, each rib having an upper and a lower edge;

a circular node at each corner of each triangle;

each node being surrounded by a circular second rib;

narrow parallel upper and lower flanges along the upper and lower edges of each of said first and second ribs, respectively;

a skin sheet integral with said lower flanges;

the improvement comprising;

wide, shallow grooves in the upper surface of each upper flange on each first rib, said grooves filled with a composite material strip comprising fibers having a composition selected from the group consisting of boron, graphite and mixtures thereof, embedded in a supporting matrix;

said fibers lying substantially parallel to each other and to said first ribs;

at least some of said fibers extending inwardly at said nodes beyond said second ribs;

said fiber strip tapering at each end to a lesser cross-sectioned fiber density.

8. The structure according to claim 7 wherein said matrix material is selected from the group consisting of epoxy resins, polyester resins, aluminum and mixtures and combinations thereof.

9. The structure according to claim 7, wherein said strip has a cross-section width-to-thickness ratio of at least 7 to 1.

10. The structure according to claim 7 wherein said strip comprises a plurality of fiber layers, each layer comprising a single layer of parallel contiguous fibers, said layers ending at different distances from the center of said node to provide said taper.