Crossed I-beam structural strut

Claim 2

A strut for a bearing support structure for a gas turbine engine, said support structure comprising an annular inner support, a concentric annular outer support, and a plurality of said struts extending therebetween and attached thereto, each strut comprising: (a) a base portion for attachment to said inner support structure; (b) a tip portion for attachment to said outer support structure; (c) a forward edge extending between said base portion and said tip portion; (d) a rearward edge extending between said base portion and said tip portion; (e) a first web integral with said forward and rearward edges, and extending between said base and tip portions; and (f) a second web integral with said first web and extending between said base and tip portions transversely to said first web, said second web including spaced apart flanges substantially perpendicular to said second web, each flange extending between said base and tip portions on each side of said first web.

Claim 3

The strut according to claim 1, further comprising face sheets attached to said forward and rearward edges and to said flanges, said face sheets extending from said strut base to said strut tip.

Claim 4

The strut according to claim 1, wherein said forward and rearward edges are integral with said flanges at said base portion, and define a wall which circumscribes said strut.

Claim 5

The strut according to claim 3, wherein said first web includes a V-shaped transition web having legs which are integral with said wall.

Claim 6

The strut according to claim 4, further comprising ribs which extend transversely between said wall.

Claim 7

The strut according to claim 1, wherein said first web includes lightening holes.

Claim 8

An airfoil shaped cast strut for a gas turbine engine intermediate case, the engine having an axis of rotation, wherein the intermediate case comprises a case centerbody, a case outer ring, and a plurality of said struts, each strut comprising: (a) a base portion for attachment to said case centerbody; (b) a tip portion for attachment to said case outer ring; (c) a leading edge and a trailing edge, each edge extending from said base portion to said tip portion, said edges defining a major strut axis extending therebetween, wherein said leading edge includes lip means extending towards said trailing edge, and said trailing edge includes lip means extending towards said leading edge; (d) a major axis web integral with said leading and trailing edges, and extending between said base and tip portions along said major strut axis; (e) an I-beam integral with said major axis web, and extending between said base portion and said tip portion, wherein said I-beam includes an I-beam web extending transversely to said major axis web, said I-beam web having opposed ends on each side of said major axis web and a flange at each of said I-beam web ends, each flange extending substantially perpendicular to said I-beam web; and (f) face sheets on each side of said major axis web, each face sheet attached to one of said leading edge lip means and to one of said trailing edge lip means, wherein each face sheet is in abutting relation to one of said flanges.

Claim 9

An airfoil shaped cast strut for a gas turbine engine intermediate case, the engine having an axis of rotation, wherein the intermediate case comprises a case centerbody, a case outer ring, and a plurality of said struts, each strut comprising: (a) a base portion for attachment to said case centerbody; (b) a tip portion for attachment to said case outer ring; (c) a leading edge and a trailing edge, each edge extending from said base portion to said tip portion, said edges defining a major strut axis extending therebetween, wherein said leading edge includes lip means extending towards said trailing edge, and said trailing edge includes lip means extending towards said leading edge; (d) a major axis web integral with said leading and trailing edges, and extending between said base and tip portions along said major strut axis; (e) an I-beam integral with said major axis web, and extending between said base portion and said tip portion, wherein said I-beam includes an I-beam web extending transversely to said major axis web, said I-beam web having opposed ends on each side of said major axis web and a flange at each of said I-beam web ends, each flange extending substantially perpendicular to said I-beam web; and (f) face sheets on each side of said major axis web, each face sheet attached to one of said leading edge lip means and to one of said trailing edge lip means, wherein each face sheet is in abutting relation to one of said flanges.

Claim 10

The strut according to claim 7, wherein said leading and trailing edge lip means are integral with said I-beam flanges at said strut base portion, and define a wall which circumscribes said strut.

Claim 11

The strut according to claim 8, wherein said major axis web includes a V-shaped transition web having legs which extend towards said base portion, wherein said legs are integral with said wall.

Claim 12

The strut according to claim 9, further comprising ribs which extend transversely between said wall.

Claim 13

The strut according to claim 7, wherein said face sheets are a composite material.

Claim 14

The strut according to claim 11, wherein said face sheets are an acoustically damping composite material.

Claim 15

The strut according to claim 7, further including lightening holes in said major axis web means.

Claim 16

An intermediate case for a high bypass ratio gas turbine engine having an axis of rotation, wherein said case comprises a centerbody and an outer ring concentric thereto and radially outwardly therefrom, and a plurality of circumferentially spaced apart airfoil shaped struts extending radially between said centerbody and said outer ring, wherein each of said struts comprises: (a) a base portion attached to said centerbody; (b) a tip portion attached to said outer ring; (c) a leading edge and trailing edge, each edge extending from said base portion to said tip portion, wherein said edges define a major strut axis extending therebetween, and wherein said leading edge includes lip means extending towards said trailing edge, and said trailing edge includes lip means extending towards said leading edge; (d) a major axis web integral with said leading and trailing edges and extending between said base and tip portions along said major strut axis; (e) an I-beam integral with said major axis web, and extending between said base and tip portions, said I-beam comprising an I-beam web extending transversely to said major axis web, said I-beam web having opposed ends on each side of said major axis web and a flange at each of said I-beam web ends, each flange extending substantially perpendicular to said I-beam web; (f) acoustic damping face sheets, extending from said leading edge lip means to said trailing edge lip means, each face sheet means attached to said lip means and to one of said I-beam flanges.

Claim 17

An intermediate case for a high bypass ratio gas turbine engine having an axis of rotation, wherein said case comprises a centerbody and an outer ring concentric thereto and radially outwardly therefrom, and a plurality of circumferentially spaced apart airfoil shaped struts extending radially between said centerbody and said outer ring, wherein each of said struts comprises: (a) a base portion attached to said centerbody; (b) a tip portion attached to said outer ring; (c) a leading edge and trailing edge, each edge extending from said base portion to said tip portion, wherein said edges define a major strut axis extending therebetween, and wherein said leading edge includes lip means extending towards said trailing edge, and said trailing edge includes lip means extending towards said leading edge; (d) a major axis web integral with said leading and trailing edges and extending between said base and tip portions along said major strut axis; (e) an I-beam integral with said major axis web, and extending between said base and tip portions, said I-beam comprising an I-beam web extending transversely to said major axis web, said I-beam web having opposed ends on each side of said major axis web and a flange at each of said I-beam web ends, each flange extending substantially perpendicular to said I-beam web; (f) acoustic damping face sheets, extending from said leading edge lip means to said trailing edge lip means, each face sheet means attached to said lip means and to one of said I-beam flanges.

Claim 18

The intermediate case according to claim 14, wherein the strut face sheets are made of a composite material.