Laminated composite rotor yoke

Claim 2

A yoke for coupling helicopter blades to a mast, the longitudinal axis of the blades coupled transversely to the longitudinal axis of the mast, comprising: a plurality of first layers formed of continuous filaments defining flat loops, each of said first layers having a width in cross section greater than the depth in cross section, and where the width of each layer lies substantially along the longitudinal axis of the blades and the depth of each layer at the mast lies substantially along the longitudinal axis of the mast; and a plurality of second layers formed of cross-wise filaments interposed between the layers formed by continuous filaments, each of said second layers having a width in cross section greater than a depth in cross section and where the width of each of the second layers lies substantially along the longitudinal axis of the blades and the depth of each of the second layers at the mast lies substantially along the longitudinal axis of the mast; said layers being substantially parallel and defining a flat, elongated loop with side and outboard end portions.

Claim 3

The yoke of claim 1, wherein the filaments defining said first layers comprise glass fibers embedded in adhesive.

Claim 4

The yoke of claim 1, wherein the filaments defining said first layers comprise glass fiber rovings embedded in adhesive.

Claim 5

The yoke of claim 1, wherein the filaments defining said second layers comprise bias ply glass fibers embedded in adhesive.

Claim 6

The yoke of claim 1, wherein at least some of said second layers extend between the side portions of the loop to define a central transverse portion, and further including: a plurality of filler layers interposed between said second layers in the transverse portion of the yoke.

Claim 7

The yoke of claim 1, wherein at least some of the second layers are discontinuous in the side portions to form predetermined gaps to provide flexure areas of reduced cross section in the side portions of the loop.

Claim 8

A composite yoke for coupling a pair of helicopter blades to a rotatable support mast, the longitudinal axis of each blade of the pair coupled transversely to the longitudinal axis of the rotatable support mast, comprising: a plurality of layers formed of continuous fibers coursing in unidirectional fashion to define flat, elongated loops having spaced apart side sections, each of the layers having a width in cross section greater that the depth in cross section, and where the width of each layer lies substantially along the longitudinal axis of the blades and the depth of each layer at the mast lies substantially along the longitudinal axis of the mast; a plurality of layers formed of bias ply fibers and interposed between the continuous fiber layers, each of the layers of bias ply fibers having a width in cross section greater than the depth in cross section, and where the width of each layer lies substantially along the longitudinal axis of the blades and the depth of each layer of bias ply fibers at the mast lies substantially along the longitudinal axis of the mast; said bias ply layers interdigitated with the layers of continuous fibers between the side sections of the loop to form a central transverse section; and a plurality of filler layers of cross section substantially the same as the cross section of the layers of continuous fibers interposed between said bias ply layers in the transverse section; said continuous fiber layers, bias ply layers, and filler layers being substantially parallel in at least the central section of the yoke.

Claim 9

A composite yoke for coupling a pair of helicopter blades to a rotatable support mast, the longitudinal axis of each blade of the pair coupled transversely to the longitudinal axis of the rotatable support mast, comprising: a plurality of layers formed of continuous fibers coursing in unidirectional fashion to define flat, elongated loops having spaced apart side sections, each of the layers having a width in cross section greater that the depth in cross section, and where the width of each layer lies substantially along the longitudinal axis of the blades and the depth of each layer at the mast lies substantially along the longitudinal axis of the mast; a plurality of layers formed of bias ply fibers and interposed between the continuous fiber layers, each of the layers of bias ply fibers having a width in cross section greater than the depth in cross section, and where the width of each layer lies substantially along the longitudinal axis of the blades and the depth of each layer of bias ply fibers at the mast lies substantially along the longitudinal axis of the mast; said bias ply layers interdigitated with the layers of continuous fibers between the side sections of the loop to form a central transverse section; and a plurality of filler layers of cross section substantially the same as the cross section of the layers of continuous fibers interposed between said bias ply layers in the transverse section; said continuous fiber layers, bias ply layers, and filler layers being substantially parallel in at least the central section of the yoke.

Claim 10

The yoke of claim 7, wherein the fibers defining said continuous fiber layers comprise glass fibers embedded in adhesive.

Claim 11

The yoke of claim 7, wherein the fibers defining said bias ply layers comprise glass fibers embedded in adhesive.

Claim 12

The yoke of claim 7, wherein said filler layers are comprised of bias ply fibers.

Claim 13

The yoke of claim 7, wherein the transverse section includes an opening formed therethrough for receiving the mast.

Claim 14

The yoke of claim 7, wherein at least some of the bias ply layers are discontinuous in the side portions to form predetermined gaps to provide flexure areas of reduced cross-section in the side sections of the yoke.