技术功效语段：
The present patent is about a system and method for vacuum forming wind turbine components, such as rotor blades, using a modular mold assembly. The system includes a base and multiple removable mold segments that form a mold cavity for forming the component. Each mold segment has a vacuum chamber that is fluidly isolated from the others, and the mold segments are heated to a forming temperature before a thermoplastic sheet is placed over the mold and a vacuum is applied to the mold to form the outer skin of the component. The technical effect of this patent is to improve the vacuum forming process for wind turbine components by reducing vacuum leaks and wrinkles in the thermoplastic sheet, resulting in better quality components.
权利要求：
WHAT IS CLAIMED IS:
1. A system for vacuum forming a component, the system comprising: a plurality of mold segments removably coupled together to define a mold cavity configured for forming the component, the plurality of the mold segments defining a a plurality of vacuum chambers of the system, at least one of the vacuum chambers being fluidly isolated from the other vacuum chambers, one or more of the plurality of mold segments further defining a plurality of vacuum passages fluidly coupling the mold cavity and the corresponding vacuum chamber.
2. The system of claim 1, further comprising:
one or more valves configured to selectively apply a vacuum created by one or more vacuum pumps to each vacuum chamber; and,
a controller communicatively coupled to the one or more valves, the controller being configured to control the one or more valves such that the vacuum is applied to one or more of the vacuum chambers independently of each other vacuum chamber.
3. The system of claim 1, wherein one or more of the plurality of mold segments extend vertically between a bottom surface and a top surface, the bottom surface partially defining the corresponding vacuum cavity, the top surface including a first portion partially defining the mold cavity and a second portion positioned outside of the mold cavity.
4. The system of claim 3, wherein the second portion of the top surface of one or more of the plurality of mold segments is fluidly isolated from the
corresponding vacuum chamber.
5. The system of claim 1, wherein one or more of the plurality of mold segments comprise one or more alignment features configured to position a thermoplastic sheet for forming the one or more components within the mold cavity, the thermoplastic sheet comprising at least a thermoplastic resin.
6. The system of claim 1, further comprising:
one or more pressure sensors, each pressure sensor being in operative association with one of the vacuum chambers, each pressure sensor being configured to detect a parameter associated with the pressure in the corresponding vacuum chamber.
7. The system of claim 1, wherein one or more of the plurality of mold segments comprises a heating element configured to selectively heat the
corresponding one or more mold segments.
8. The system of claim 1, wherein one or more of the plurality of mold segments defines one or more fluid passages.
9. The system of claim 1, wherein the component is a rotor blade segment of a wind turbine.
10. A method for forming a rotor blade segment for a wind turbine, the method comprising:
removably coupling a plurality of mold segments together to form a mold of the rotor blade panel, one or more of the plurality of mold segments defining a portion of a mold cavity of the mold, the mold cavity being configured to form an outer skin of the rotor blade panel, the plurality of mold segments at least partially defining a plurality of vacuum chambers of the mold, one or more of the plurality of vacuum chambers being fluidly isolated from each other vacuum chamber, one or more of the plurality of mold segments further defining a plurality of vacuum passages fluidly coupling the mold cavity and the corresponding vacuum chamber;
heating each of the plurality of mold segments to a forming temperature;
positioning a thermoplastic sheet on the mold such that at least a portion of the thermoplastic sheet is positioned within or over the mold cavity, the thermoplastic sheet comprising at least a thermoplastic resin; and,
selectively applying a vacuum to one or more of the plurality of vacuum chambers such that the thermoplastic sheet conforms to the mold cavity to form the outer skin of the rotor blade segment.
11. The method of claim 10, further comprising:
aligning the thermoplastic sheet with one or more alignment features when positioning a thermoplastic sheet on the mold.
12. The method of claim 11, further comprising:
trimming the outer skin of the rotor blade segment.
13. The method of claim 10, wherein selectively applying the vacuum to each vacuum chamber comprises selectively applying the vacuum to each vacuum chamber in a sequential manner.
14. The method of claim 10, wherein applying the vacuum to each vacuum chamber comprises selectively applying the vacuum to each vacuum chamber in a non- sequential manner.
15. The method of claim 10, further comprising:
placing the mold relative to a computer numeric control (CNC) device;
maintaining the outer skin of the rotor blade segment at the forming temperature after forming the outer skin; and,
printing, with the CNC device, a first number of layers of a structural member on the outer skin when the outer skin of the rotor blade segment is at or above a glass transition temperature.
16. The method of claim 16, further comprising:
terminating or reducing heating of the mold after printing and depositing the first number of layers of the structural member onto the outer skin; and,
printing, with the CNC device, a second number of layers of a structural member onto the first number of layers of the structural member after terminating or reducing heating provided by the heating element.
17. The method of claim 10, wherein each mold segment comprises a top surface including a first portion partially defining the mold cavity and a second portion positioned outside of the mold cavity, the method further comprising:
printing, with the CNC device, an extension onto the outer skin of the rotor blade segment and the second portion of one or more of the plurality of mold segments.
18. The method of claim 10, further comprising:
cooling the outer skin of rotor blade segment by circulating a coolant through one or more fluid passages defined by one or more of the mold segments.
19. The method of claim 10, further comprising:
monitoring, with one or more pressure sensors, a pressure within one or more of the vacuum chambers of the mold.
20. A method for vacuum forming a component using a vacuum forming mold assembly, the vacuum forming mold assembly including a plurality of mold segments removably coupled together to form a mold of the rotor blade panel, one or more of the plurality of mold segments defining a portion of a mold cavity of the
mold, the mold cavity being configured to form an outer skin of the rotor blade panel, one or more of the plurality of mold segments at least partially defining a plurality of vacuum chambers of the mold, one or more of the plurality of vacuum chambers being fluidly isolated from each other vacuum chamber, one or more of the plurality of mold segments further defining a plurality of vacuum passages fluidly coupling the mold cavity and the corresponding vacuum chamber, the method comprising:
heating each of the plurality of mold segments to a forming temperature; positioning a thermoplastic sheet on the mold such that at least a portion of the thermoplastic sheet is positioned within or over the mold cavity, the thermoplastic sheet comprising at least a thermoplastic resin; and,
selectively applying a vacuum to one or more of the plurality of vacuum chambers such that, when the thermoplastic sheet conforms to the mold cavity, the thermoplastic sheet is substantially free of wrinkles.