Patent Application
20240262053
The present invention relates to large lightweight molded fan blades, fan stacks and other fan components and methods for their manufacture.
Composite materials find wide use in many industries due to their numerous advantages, such as design flexibility, light weight, chemical resistance, and reduction of the number of components. Many industries have applied composite materials in their products, taking advantage of these characteristics, including automotive and transport, construction, infrastructure and architecture, aerospace, energy, marine, and sports industries. In the case of large commercial or industrial composite material parts, for example fan blades, fan stacks and other fan components used in large scale industrial cooling towers, the manufacture is often done in stages. For example, the process for manufacturing large scale fan blades with composite materials is usually done in steps, with the main structure made in two separate parts, the suction side of the blade, and the pressure side of the blade. Each blade piece is made separately in different molds by vacuum resin infusion, in which a liquid resin is injected into and through a fiber reinforced structure. To maintain the lightness of the part, the fiber content is kept high relative to the resin component of the composite. This is important because the structural properties of composite materials are derived mainly from the fiber reinforcement. A high content of fiber reinforcement improves the structural performance, enhancing tensile strength and stiffness, while minimizing weight. Following the independent manufacture of two different solid unitary composite parts, the two pieces are bonded together, resulting in seam lines and substantial bond areas, typically at the leading and trailing edges of the blade, and often along the central line of the component (see
Another method that has been applied with success to the manufacture of large lightweight composite parts such as wind turbine blades is the so-called one-shot infusion molding process. The result is a blade without seam lines, but the one-shot process requires the use of a large vacuum bag and flexible inserts that are placed inside the part being manufactured (see
Other composite molding technologies include resin transfer molding (“RTM”) and Vacuum-assisted RTM (“VRTM” or “RTM light”). In RTM, a resin is injected into a two-part rigid mold to impregnate the fiber reinforcement. This process involves placing the dry fiber layup on a mold surface, closing the mold over the fiber layup and injecting thermosetting resin into the mold under high pressure to impregnate the fiber layup. To avoid resin leakage, the mold is sealed by compression of a flange gasket on an outside surface of the mold. More often, the reinforcing fibers of the layup are non-oriented and are characterized by high permeability to make the resin flow easily; these material characteristics are necessary for RTM to permit the resin to flow sufficiently to fill the mold and impregnate all of the layup. Typically, the RTM process cannot be used to produce components having a fiber reinforcement content greater than 50%. Attempts at increasing fiber content in RTM molding processes above 50% reduces the permeability of the fiber reinforcement, leading to the need to increase injection pressure, which in turn requires increasing the mold structural stiffness to avoid mold distortion or failure. So, RTM is not suitable for molding very large lightweight products, products that have widely variable composite thickness, products with complicated geometries, or high-performance materials which require oriented fiber fabric reinforcement. Additionally, RTM requires very high mold strength and stiffness to prevent distortion or opening of the mold under the high injection pressure. This requirement for a heavy reinforced mold results in a size limitation for the use of RTM, as mold costs and weight become impractical for the molding of large structures.
VRTM (RTM light) is a variation of RTM that uses a vacuum to pull the resin through a lightweight mold, resulting in substantially lower costs. However, VRTM suffers from the same inability to mold lightweight products, products with variable composite thicknesses or products with complicated geometries as with RTM.
The bonding process of two (or more) part molded fan blades and components is a critical manufacturing step which, even if done correctly, generates weak points in the structure that can compromise the integrity of the part and its mechanical strength.
Where the RTM and VRTM molding process do not require a bonding step which results in seams, the reinforcement layup and part geometry are limited due to the process limitations. Therefore, when the structural requirements are higher as in the case of large lightweight fan blades, RTM and VRTM are not optimal.
The use of the vacuum bag/flexible insert of the one-shot process requires a large quantity of consumable (non-reusable) materials and presents limitations when the component geometry presents small details or narrow cavities where the vacuum bag cannot fit. Another drawback of the one-shot process is the requirement for an opening in the part large enough for removal of the insert and infusion consumables (see
Accordingly, there is a need for lower cost, less labor intensive methods for making large lightweight and seamless molded composite parts with variable composite thicknesses and complicated geometries.
The present invention overcomes the disadvantages of these prior art molding processes. According to one advantage of the invention, there is no seam line in the final product, which results in significant improvement in structural strength and in the time required for finishing processing. There is also a significant reduction in manufacturing time, both in the molding step and the elimination of the joining and finishing steps. Another important advantage is that there is no longer a need for consumable materials. The process according to the invention can be applied in the manufacture of any large lightweight composite material fan blade and fan components that would benefit from these advantages, for example, fan blades, hubs, stacks, ducts, chimneys, equipment casings and panels.
According to the process of the invention, a monolithic component is created by means of a single step infusion in a closed mold, creating a seamless structure. The interior of the part contains a core material that may be selected according to the structural, strength, and weight requirements for the finished component. Different materials can be used as the core, for example, a polymeric foam, or a natural material, such as balsa wood, among other possibilities. The core contains a series of channels on the surface that improve the infusion process allowing the resin to be infused into the component without need for additional consumable materials, and with use of a vacuum sufficient only to create lower pressure inside the mold allowing the atmospheric pressure to push the resin into the mold cavity. There is no requirement for positive pressure systems, as used in RTM methods, to force the resin into the cavity, although low positive pressure may be optionally used. The channels are designed with distribution patterns, depths, and spacing configured so that the entire mold cavity is entirely filled, even in parts with complicated geometries, for example, closed profiles with internal details and/or double curvatures (containing a change in direction in two or more planes), and the reinforcing fabric is completely wetted by the resin so that dry fabric spots that could compromise part quality are avoided. High performance reinforcement material such as, glass, carbon or aramid oriented fiber fabrics may be used, where the percentage of oriented fiber fabrics may make up from about 30% to about 100%, preferably about 60% to about 100%, and most preferably about 100% of the reinforcing material, further increasing composite strength and stiffness. The resulting improved manufacturing process reduces costs and improves the quality of the component, eliminating finishing adjustment operations and eliminating the need to perform additional lamination to reinforce the component. The resin infusion process of the invention can produce parts containing approximately 55% to 70% fiber reinforcement, preferably about 70%. This quantity of fiber reinforcement in the resin-fiber composite delivers high mechanical performance and, at the same time, low structural weight. According to the method of the invention, the size of the core relative to the finished product is selected to result in the same fiber content for the manufacture of the same part as with the vacuum resin infusion method, so that the same level of mechanical performance is achieved, with lower material and labor cost.
The foregoing summary, as well as the following detailed description of the preferred invention, will be better understood when read in conjunction with the appended drawings. For the purpose of illustrating the invention, the drawings depict embodiments which are presently preferred. It should be understood, however, that the invention is not limited to the precise arrangements and instrumentalities shown. In particular, while the manufacture of a large lightweight fan blade is referenced herein for the exemplary purpose of describing the invention, the invention may also be used for the manufacture of small fan blades and other fan components, including hubs, casings and stacks. In the drawings:
The invention begins with the manufacture of a core generally in the shape of the final article, but reduced in size sufficient for a molded overlay of reinforcing fabric and resin to result in the final article. The core is preferably a single unitary element.
The present invention results in a final article with the same or improved structural, strength, weight and surface features of prior art fan blades with substantially less material and labor costs.
It will be appreciated by those skilled in the art that changes could be made to the preferred embodiments described above without departing from the inventive concept thereof. It is understood, therefore, that this invention is not limited to the particular embodiments disclosed, but it is intended to cover modifications within the spirit and scope of the present invention as outlined in the present disclosure and defined according to the broadest reasonable reading of the claims that follow, read in light of the present specification.
| Number | Date | Country | |
|---|---|---|---|
| 63483724 | Feb 2023 | US |
