Method and mold for manufacturing fiber-reinforced plastic structure
In the manufacturing method of the present invention, as preparation for providing a mold 30 with protrusions 31 and 32 to be printed on an FRP material of a skin 1 in co-bold molding, which requires resetting of the skin 1 to the mold 30 , a long protrusion 32 A and a short protrusion 32 B are interchangeable as one protrusion 32 . The long protrusion 32 A is printed to form a second recessed part 12 in the skin 1 , and before the skin 1 is reset, the long protrusion 32 A is replaced with the short protrusion 32 B. In this way, as the short protrusion 32 B is housed in the second recessed part 12 formed during elongation of the mold 30 , the skin 1 can be reset in the state of being positioned relative to the mold 30 by the first protrusion 31 and the short protrusion 32 B.
1. A method for manufacturing a fiber-reinforced plastic structure, comprising:
providing a mold with a first printing part at a reference location and a second printing part at a second location spaced apart from the reference location in a predetermined direction, wherein the second printing part is a long protrusion extending in the predetermined direction;
a first molding step wherein a first fiber-reinforced plastic member is molded on the mold with heating such that the first printing part forms a first print on the fiber-reinforced plastic member and the second printing part forms a second print on the fiber-reinforced plastic member;
removing the first fiber-reinforced plastic member from the mold;
replacing the second printing part with a short protrusion;
a resetting step wherein the first fiber-reinforced plastic member is reset on the mold so that the short protrusion is located in the second print formed by the second printing part; and
a second molding step wherein a second fiber-reinforced plastic member is molded onto the reset first fiber-reinforced plastic member with heating.
2. The method for manufacturing the fiber-reinforced plastic structure according to claim 1 , wherein
the long protrusion and the short protrusion have different lengths in the predetermined direction,
in the first molding step, the mold is heated such that long projection moves from a first region to a second region along the predetermined direction, and
in the resetting step, the short protrusion is located within a range of overlap between the first region and the second region.
3. The method for manufacturing the fiber-reinforced plastic structure according to claim 1 , wherein
the long protrusion and the short protrusion are formed in equal widths and maintained in a direction along the predetermined direction, and
a length of the long protrusion is longer than a width of the long protrusion.
4. The method for manufacturing the fiber-reinforced plastic structure according to claim 1 , wherein
as preparation the first molding step, an end portion of a fiber base material, which constitutes a material of the first fiber-reinforced plastic member and is disposed on the second printing part, is cut off on a side away from the first printing part to expose the second printing part from the fiber base material.
5. The method for manufacturing the fiber-reinforced plastic structure according to claim 1 , wherein
the first fiber-reinforced plastic member is a skin of an aircraft, and
the second fiber-reinforced plastic member is a stringer of the aircraft.
6. The method for manufacturing the fiber-reinforced plastic structure according to claim 1 , wherein the first fiber-reinforced plastic member and the second fiber-reinforced plastic member are constituent members of an aircraft.
7. A method for manufacturing a fiber-reinforced plastic structure, comprising:
providing a mold with a first printing part at a reference location and a second printing part at a second location spaced apart from the reference location in a predetermined direction;
a first molding step wherein a first fiber-reinforced plastic member is molded on the mold with heating such that the first printing part forms a first print on the fiber-reinforced plastic member and the second printing part forms a second print on the fiber-reinforced plastic member;
removing the first fiber-reinforced plastic member from the mold;
removing the second printing part from the mold and providing the mold with a protrusion, wherein the protrusion is provided at a different portion of the mold than the second printing part; and
a resetting step wherein the first fiber-reinforced plastic member is reset on the mold so that the protrusion is located in the second print formed by the second printing part.
8. The method for manufacturing the fiber-reinforced plastic structure according to claim 7 , further comprising a second molding step wherein a second fiber-reinforced plastic member is molded onto the reset first fiber-reinforced plastic member with heating.
9. The method for manufacturing the fiber-reinforced plastic structure according to claim 8 , wherein
the first fiber-reinforced plastic member is a skin of an aircraft, and
the second fiber-reinforced plastic member is a stringer of the aircraft.
10. The method for manufacturing the fiber-reinforced plastic structure according to claim 8 , wherein the first fiber-reinforced plastic member and the second fiber-reinforced plastic member are constituent members of an aircraft.
11. The method for manufacturing the fiber-reinforced plastic structure according to claim 7 , wherein
the second printing part and the protrusion have different lengths in the predetermined direction,
in the first molding step, the mold is heated such that the second printing part moves from a first region to a second region along the predetermined direction, and
in the resetting step, the protrusion is located within a range of overlap between the first region and the second region.
12. The method for manufacturing the fiber-reinforced plastic structure according to claim 7 , wherein
the second printing part and the protrusion are formed in equal widths and maintained in a direction along the predetermined direction, and
a length of the second printing part is longer than a width of the second printing part.
13. The method for manufacturing the fiber-reinforced plastic structure according to claim 7 , wherein
as preparation for the first molding step, an end portion of a fiber base material, which constitutes a material of the first fiber-reinforced plastic member and is disposed on the second printing part, is cut off on a side away from the first printing part to expose the second printing part from the fiber base material.
14. A method for manufacturing a fiber-reinforced plastic structure, comprising:
providing a mold with a first printing part at a reference location and a second printing part at a second location spaced apart from the reference location in a predetermined direction;
a first molding step wherein a first fiber-reinforced plastic member is molded on the mold with heating such that the first printing part forms a first print on the fiber-reinforced plastic member and the second printing part forms a second print on the fiber-reinforced plastic member;
removing the first fiber-reinforced plastic member from the mold;
removing the second printing part from the mold and providing the mold with a protrusion, wherein the second printing part and the protrusion have different lengths in the predetermined direction; and
a resetting step wherein the first fiber-reinforced plastic member is reset on the mold so that the protrusion is located in the second print formed by the second printing part.
15. The method for manufacturing the fiber-reinforced plastic structure according to claim 14 , further comprising a second molding step wherein a second fiber-reinforced plastic member is molded onto the reset first fiber-reinforced plastic member with heating.
16. The method for manufacturing the fiber-reinforced plastic structure according to claim 15 , wherein
the first fiber-reinforced plastic member is a skin of an aircraft, and
the second fiber-reinforced plastic member is a stringer of the aircraft.
17. The method for manufacturing the fiber-reinforced plastic structure according to claim 15 , wherein the first fiber-reinforced plastic member and the second fiber-reinforced plastic member are constituent members of an aircraft.
18. The method for manufacturing the fiber-reinforced plastic structure according to claim 14 , wherein:
in the first molding step, the mold is heated such that the second printing part moves from a first region to a second region along the predetermined direction, and
in the resetting step, the protrusion is located within a range of overlap between the first region and the second region.
19. The method for manufacturing the fiber-reinforced plastic structure according to claim 14 , wherein
the second printing part and the protrusion are formed in equal widths and maintained in a direction along the predetermined direction, and
a length of the second printing part is longer than a width of the second printing part.
20. The method for manufacturing the fiber-reinforced plastic structure according to claim 14 , wherein
as preparation for the first molding step, an end portion of a fiber base material, which constitutes a material of the first fiber-reinforced plastic member and is disposed on the second printing part, is cut off on a side away from the first printing part to expose the second printing part from the fiber base material.