System and method for manufacture of airfoil components
Embodiments of the present disclosure relate generally to systems and methods for manufacturing an airfoil component. The system can include: a geometrical mold; an elongated flexible sleeve having a closed-off interior and positioned within the geometrical mold, wherein the elongated flexible sleeve is further positioned to have a desired geometry; an infusing channel in fluid communication with the closed-off interior of the elongated flexible sleeve and configured to communicate a resinous material thereto; a vacuum channel in fluid communication with the closed-off interior of the elongated flexible sleeve and configured to vacuum seal the closed-off interior of the elongated flexible sleeve; and a glass fiber layer positioned within the closed-off interior of the elongated flexible sleeve.
1. A system for manufacturing a turbine blade, the system comprising:
an elongated flexible sleeve having a closed-off interior and positioned within a geometrical mold, wherein the elongated flexible sleeve is further positioned to have a desired geometry including a leading edge portion and a trailing edge portion, and wherein the geometrical mold further comprises a plurality of pegs in contact with the elongated flexible sleeve, the plurality of pegs being configured to shape the elongated flexible sleeve into the desired geometry;
an infusing channel in fluid communication with the closed-off interior of the elongated flexible sleeve and configured to communicate a resinous material thereto at the trailing edge portion of the desired geometry;
a vacuum channel in fluid communication with the closed-off interior of the elongated flexible sleeve and configured to vacuum seal the closed-off interior of the elongated flexible sleeve at the trailing edge portion of the desired geometry, such that the infusing channel is positioned directly adjacent to the vacuum channel; and
a glass fiber layer positioned within the closed-off interior of the elongated flexible sleeve.
2. The system of claim 1 , further comprising a stiffening material positioned within the closed-off interior of the elongated flexible sleeve.
3. The system of claim 1 , wherein the infusing channel is further configured to communicate a thermal setting polymer to the closed-off interior of the elongated flexible sleeve.
4. The system of claim 1 , further comprising a pultruded composite member configured to have the desired geometry and positioned within the closed-off interior of the elongated flexible sleeve.
5. The system of claim 4 , wherein the pultruded composite member comprises a composite fibrous material.
6. The system of claim 4 , wherein the desired geometry includes at least one region of curvature, and the pultruded composite member is positioned radially distal to the glass fiber layer throughout the at least one region of curvature.
7. The system of claim 1 , wherein one of the plurality of pegs projects from the geometrical mold at a non-perpendicular angle with respect to the geometrical mold.
8. A system for manufacturing a turbine blade, the system comprising:
an elongated flexible sleeve positioned within a geometrical mold, the elongated flexible sleeve having a first end, a second end, and a closed-off interior, wherein the elongated flexible sleeve is configured to have a desired geometry including a leading edge portion and a trailing edge portion for the turbine blade, and wherein the geometrical mold further comprises a plurality of pegs in contact with the elongated flexible sleeve, the plurality of pegs being configured to shape the elongated flexible sleeve into the desired geometry;
an infusing channel coupled to the first end of the elongated flexible sleeve at the trailing edge portion of the desired geometry and in fluid communication with the closed-off interior of the elongated flexible sleeve, wherein the infusing channel is configured to communicate a liquid-based resinous material to the closed-off interior of the elongated flexible sleeve;
a vacuum channel coupled to the second end of the elongated flexible sleeve at the trailing edge portion of the desired geometry and in fluid communication with the closed-off interior of the elongated flexible sleeve, wherein the vacuum channel is configured to vacuum-seal the closed-off interior of the elongated flexible sleeve, wherein the infusing channel is positioned directly adjacent to the vacuum channel proximal to the trailing edge portion;
a pultruded composite member having first and second opposing ends, the pultruded composite member being configured to have the desired geometry and positioned within the closed-off interior of the elongated flexible sleeve such that the first and second opposing ends are proximal to the trailing edge portion; and
a glass fiber layer positioned adjacent to the pultruded composite member and positioned within the closed-off interior of the elongated flexible sleeve.
9. The system of claim 8 , wherein the desired geometry includes at least one region of curvature, and the pultruded composite member is positioned radially distal to the glass fiber layer throughout the at least one region of curvature.