Rotor blade afterbody
An afterbody for a rotor blade of a rotorcraft is unitarily formed of a single material of construction. The afterbody includes an upper surface disposed from a lower surface, a concave leading edge connected to the upper surface and the lower surface, and a trailing edge formed at an intersection of the upper surface with the lower surface.
1. An afterbody for a rotor blade of a rotorcraft, comprising:
a body unitarily formed of a single material of construction including an upper surface disposed from a lower surface, a leading edge extending from the upper surface to the lower surface, and a trailing edge formed at an intersection of the upper surface with the lower surface, wherein the upper and lower surfaces extend in a chord direction from the leading edge to the trailing edge and the leading edge is curved inward in the chord direction toward the trailing edge; and
the body includes an internal structure encompassed by the leading edge, the upper surface, and the lower surface, the internal structure comprising at least one of a collection of ribs and stringers, or a lattice arrangement of cells.
2. The afterbody of claim 1 , wherein the internal structure provides force resistance in both the chord direction and a beam direction.
3. The afterbody of claim 1 , wherein the internal structure consists of the collection of ribs and stringers.
4. The afterbody of claim 1 , wherein the internal structure consists of the lattice arrangement of cells.
5. The afterbody of claim 1 , wherein the single material of construction is a thermoplastic material.
6. The afterbody of claim 1 , wherein the trailing edge is without a first skin bonded to a second skin.
7. The rotor blade of claim 1 , wherein the internal structure includes uniformly sized and shaped support structures.
8. The rotor blade of claim 1 , wherein the internal structure includes non-uniformly sized and shaped support structures.
9. A rotor blade for a rotorcraft, comprising:
a one-piece afterbody formed of a single material of construction without a separate upper skin and without a separate lower skin, the afterbody comprising an upper surface and a lower surface extending in a chord direction from a concave leading edge to a trailing edge formed at an intersection of the upper surface and the lower surface, wherein the concave leading edge is curved inward toward the trailing edge;
a trailing side of a spar adhered to the one-piece afterbody at the concave leading edge; and
an internal structure unitarily formed with the upper surface, the lower surface, the concave leading edge, and the trailing edge, wherein the structure includes non-uniformly sized and shaped support structures.
10. The rotor blade of claim 9 , wherein an entirety of the concave leading edge is adhered to the trailing side of the spar with a single bonded joint.
11. The rotor blade of claim 9 , wherein the internal structure is capable of transferring loads in both the chord direction and a beam direction.
12. The rotor blade of claim 9 , wherein the spar is manufactured of thermoset material and the one-piece afterbody is manufactured of thermoplastic material.
13. The rotor blade of claim 9 , wherein the internal structure comprises a collection of ribs and stringers.
14. The rotor blade of claim 9 , wherein the internal structure comprises a lattice arrangement of cells.
15. A rotor blade for a rotorcraft, comprising:
a spar including a root section, a tip section, a leading side, and a trailing side;
an afterbody including a curved leading edge, an entirety of the curved leading edge adhered to the trailing side of the spar with a single bonded joint; and
a chord-wise cross-sectional shape of the afterbody includes an upper surface extending in a chord direction from the curved leading edge to a trailing edge, a lower surface extending in the chord direction from the curved leading edge to the trailing edge, the trailing edge formed at an intersection of the upper surface with the lower surface and the curved leading edge curved inward in the chord direction toward the trailing edge, and an internal structure unitarily formed of a single material of construction with and encompassed by the upper surface, the lower surface, and the curved leading edge.
16. The rotor blade of claim 15 , wherein the afterbody comprises a plurality of segments connected spanwise between the root section and the tip section where each segment of the plurality of segments includes the chord-wise cross-sectional shape.
17. The rotor blade of claim 15 , wherein the internal structure comprises a collection of ribs and stringers.
18. The rotor blade of claim 15 , wherein the internal structure comprises a lattice arrangement of cells.