Rotorcraft glade grip

1. A method, comprising:

forming a laminated structure by applying a plurality of layers of laminating material and a bonding material to a molding fixture, wherein each layer of the plurality of layers of laminating material, other than the outermost layers of the plurality of layers of laminating material, has a different fiber orientation than a fiber orientation of at least one immediately adjacent layer of the plurality of layers of laminating material;

rolling at least one layer of the plurality of layers of laminating material;

vacuum pressing the laminated structure on the molding fixture;

forming a grip blank by setting the bonding material, wherein the grip blank comprises an upper sheet, a lower sheet and a connecting blank portion, wherein the connecting blank portion is disposed between, and connects, the upper sheet and the lower sheet, wherein the grip blank comprises a laminated composite extending contiguously from the upper sheet, through the connecting blank portion, to the lower sheet, and wherein the grip blank has a constant thickness along a length of the upper sheet, around the connecting portion, and along a length of the lower sheet;

removing the grip blank from molding fixture;

forming a reference feature in the grip blank;

mounting the grip blank on a tooling fixture; and

cutting a grip body from the grip blank with respect to the reference feature, wherein the grip body has an upper extension, a lower extension and a connecting portion, wherein the connecting portion is disposed between, and connects, an inboard end of the upper extension and an inboard end of the lower extension, and wherein an inside surface of the upper extension faces, and is substantially parallel to, an inside surface of the lower extension.

2. The method of claim 1 , wherein forming the grip blank comprises forming the grip blank with the constant thickness along the length of the upper sheet, around the connecting portion, and along a length of the lower sheet, with a constant thickness along the width of the upper sheet, and with a constant thickness along the width of the lower sheet; and

wherein the cutting of the grip body from the grip blank comprises cutting more than one grip body from the same grip blank.

3. The method of claim 1 , wherein, after cutting the grip body from the grip blank, an outboard end of the upper extension is wider than the inboard end of the upper extension, and an outboard end of the lower extension is wider than the inboard end of the lower extension.

4. The method of claim 1 , wherein cutting the grip body from the grip blank further comprises:

forming first attachment holes in the upper extension; and

forming second attachment holes in the lower extension that correspond to, and are aligned with, the first attachment holes.

5. The method of claim 4 , further comprising:

providing a first protective pad on an outside surface of the upper extension around the first attachment holes;

providing a second protective pad on an outside surface of the lower extension around the second attachment holes;

inserting first bushings into the first attachment hole and second bushings into the second attachment holes; and

affixing a polyester fiber material to an inside surface of connecting portion and an edge surface of the connecting portion.

6. The method of claim 4 , wherein cutting the grip body from the grip blank further comprises:

cutting the grip blank so that an outboard edge of an outboard end of the upper extension has first lobes corresponding to two or more of the first attachment holes and at least one first cove disposed between the first lobes, and so that an outboard edge of an outboard end of the lower extension has second lobes corresponding to two or more of the second attachment holes and at least one second cove disposed between the second lobes.

7. A method comprising:

forming a grip body of a grip assembly from a contiguous laminated composite such that the grip body has a substantially constant thickness, wherein the grip body is formed with an upper extension, a lower extension and a connecting portion connected between an inboard end of the upper extension and an inboard end of the lower extension, wherein an inside surface of the upper extension faces, and is substantially parallel to, an inside surface of the lower extension, and wherein the grip body is shaped to attach a rotor blade of a rotorcraft to a yoke;

providing first features on the upper extension and second features on the lower extension, wherein the second features are aligned with the first features, and wherein the first features and second features each comprise at least one of an edge contour, attachment holes, or protective pads; and

providing protective surfaces on the connecting portion, wherein providing the protective surfaces comprises affixing a first element of the protective surfaces on an outer surface of an inward facing portion of the connecting portion, wherein second elements of the protective surfaces are spaced apart from the first element of the protective surfaces and are affixed to edge surfaces of the connecting portion.

8. The method of claim 7 , wherein providing the first features and the second features comprise providing attachment holes; and

wherein the method further comprises providing bushings disposed in the attachment holes.

9. The method of claim 7 , wherein forming the grip body comprises:

forming one or more lobes corresponding to one or more of the attachment holes in an edge of outboard end of the upper extension and in an edge of an outboard end of the lower extension;

forming a cove in the edge of the outboard end of the upper extension between lobes of the upper extension; and

forming a cove in the edge of the outboard end of the lower extension between lobes of the lower extension.

10. The method of claim 7 , wherein providing the first features and the second features comprises providing attachment holes as the first features and the second features, and further comprises providing the protective pads as the first features and the second features;

wherein the protective pads comprise a first protective pad affixed on an outside surface of the upper extension around the attachment holes of the upper extension; and

wherein the protective pads further comprise a second protective pad affixed on an outside surface of the lower extension around the attachment holes of the lower extension.

11. The method of claim 7 , wherein the protective surfaces comprise a polyester fiber material.

12. The method of claim 7 , further comprising installing the grip body on the rotorcraft with a pitch horn extending between the inside surface of the upper extension and the rotor blade and further extending between the inside surface of the lower extension and the rotor blade.

13. The method of claim 7 , wherein an inside radius of the connecting portion has a substantially contiguous curve extending from the upper extension to the lower extension.

14. A method, comprising:

providing a grip body having an upper extension, a lower extension and a connecting portion, wherein the connecting portion is disposed between and connects an inboard end of the upper extension and an inboard end of the lower extension, and wherein the grip body is formed from a laminated composite extending contiguously from the upper extension, through the connecting portion, to the lower extension, wherein the laminated composite has a plurality of layers, each layer of the plurality of layers extending contiguously along a length of the upper extension, around the connecting portion, and along a length of the lower extensions, wherein the grip body has a constant thickness along the length of the upper extension, around the connecting portion, and along the length of the lower extension, wherein an inside surface of the upper extension faces, and is substantially parallel to, an inside surface of the lower extension, wherein an inward facing portion of the connecting portion has a contiguous curvature between the upper extension and lower extension; and

providing protective surfaces on the connecting portion, and wherein a first element of the protective surfaces is affixed to an outer surface of the inward facing portion of the connecting portion, wherein second elements of the protective surfaces are spaced apart from the first element of the protective surfaces and are affixed to edge surfaces of the connecting portion.

15. The method of claim 14 , wherein each layer of the plurality of layers has a different fiber orientation than a fiber orientation of an immediately adjacent layer of the plurality of layers.

16. The method of claim 14 , further comprising:

forming first attachment holes in the upper extension; and

forming second attachment holes in the lower extension, wherein the second attachment holes correspond to, and are aligned with, the first attachment holes.

17. The method of claim 16 , further comprising:

providing bushings disposed in the first attachment holes and the second attachment holes;

providing a first protective pad on an outside surface of the upper extension and around a first one of the first attachment holes; and

providing a second protective pad on an outside surface of the lower extension and around a second one of the second attachment holes.

18. The method of claim 17 , wherein the first protective pad extends contiguously around additional ones of the first attachment holes; and

wherein the second protective pad extends contiguously around additional ones of the second attachment holes.

19. The method of claim 16 , wherein an outboard end of the upper extension is wider than the inboard end of the upper extension, and wherein an outboard end of the lower extension is wider than the inboard end of the lower extension; and

wherein an outboard edge of the outboard end of the upper extension has first lobes corresponding to two or more of the first attachment holes and at least one first cove disposed between the first lobes, and wherein an outboard edge of the outboard end of the lower extension has second lobes corresponding to two or more of the second attachment holes and at least one second cove disposed between the second lobes.

20. The method of claim 14 , further comprising:

providing a first polyester fiber material disposed on the inside surface of the connecting portion; and

providing a second polyester fiber material disposed on an edge surface of the connecting portion.