Secondary groove for work piece retention during machining
View Patent ↗A cure tool assembly and method of manufacturing a composite part. The cure tool assembly may include a rigid cure tool having a cutter groove and a securing groove formed therein. The cutter groove may be spaced apart from and formed around the cutter groove. The securing groove may be slanted inward, away from a peripheral edge of the rigid cure tool. The cure tool assembly may also include a first sacrificial material located in the cutter groove and a second sacrificial material located in the securing groove. Composite material placed onto the outer surface of the rigid cure tool may bond with the second sacrificial material during cure, creating a desired hold-down force to keep the composite material in place. The resulting cured part may be cut along the cutter groove, thus cutting through the composite material and into the first sacrificial material.
1. A cure tool assembly comprising:
a rigid cure tool having an outer surface, at least one peripheral edge, a cutter groove formed into the outer surface, and a securing groove formed into the outer surface and located outward of the cutter groove and substantially surrounding the cutter groove;
a first sacrificial material located in and cured within the cutter groove; and
a second sacrificial material located in the securing groove, wherein the first and second sacrificial materials have a lower shear strength than the rigid cure tool,
wherein the first sacrificial material in the cutter groove is coated with a release agent sufficient to prevent a composite material from bonding to the first sacrificial material during cure, and the second sacrificial material is configured to bond to the composite material during cure.
2. The cure tool assembly of claim 1 , wherein the cutter groove is substantially continuous, and the securing groove is substantially continuous and extends around the cutter groove, wherein the securing groove is positioned between the cutter groove and the peripheral edge of the rigid cure tool.
3. The cure tool assembly of claim 1 , wherein the securing groove is substantially slanted from the outer surface of the rigid cure tool in a direction inward, away from the peripheral edge of the rigid cure tool.
4. The cure tool assembly of claim 1 , wherein the cutter groove has a cross-sectional shape that is a dove-tail configuration, an inverse dove-tail configuration, a curved configuration, a square configuration, or a rectangular configuration.
5. The cure tool assembly of claim 1 , further comprising a release agent between the securing groove and the second sacrificial material.
6. The cure tool assembly of claim 1 , wherein the first sacrificial material has a lower strength than the second sacrificial material.
7. A cure tool assembly comprising:
a rigid cure tool having an outer surface, at least one peripheral edge, a cutter groove formed into the outer surface, and a securing groove formed into the outer surface and located outward of the cutter groove and substantially surrounding the cutter groove;
a first sacrificial material located in and cured within the cutter groove;
a second sacrificial material located in the securing groove, wherein the first and second sacrificial materials have a lower shear strength than the rigid cure tool; and
a release agent between the securing groove and the second sacrificial material.
8. A cure tool assembly comprising:
a rigid cure tool having an outer surface and peripheral edges, wherein the outer surface has a continuous cutter groove formed therein and a continuous securing groove formed therein, wherein the securing groove is located between the peripheral edges and the cutter groove and surrounding the cutter groove, wherein the securing groove comprises two side walls slanted from the outer surface of the rigid cure tool in a direction angled into the rigid cure tool and away from the peripheral edge of the rigid cure tool;
a first sacrificial material located in and cured within the cutter groove; and
a second sacrificial material located in the securing groove, wherein the first and second sacrificial materials have a lower shear strength than the rigid cure tool,
wherein the first sacrificial material in the cutter groove is coated with a release agent sufficient to prevent a composite material from bonding to the first sacrificial material during cure, wherein the second sacrificial material is configured to bond to the composite material during cure, wherein the release agent is further located between the securing groove and the second sacrificial material.
9. The cure tool assembly of claim 8 , wherein the cutter groove has a cross-sectional shape that is a dove-tail configuration, an inverse dove-tail configuration, a curved configuration, a square configuration, or a rectangular configuration.
10. The cure tool assembly of claim 8 , wherein the first sacrificial material has a lower strength than the second sacrificial material.
11. The cure tool assembly of claim 8 , wherein the securing groove comprises opposing segments angled in opposite directions from each other.
12. The cure tool assembly of claim 11 , wherein the opposing segments are sides of a substantially square or rectangular configuration formed by the continuous securing groove.
13. A method for curing uncured composite material, the method comprising:
placing a first sacrificial material into a cutter groove formed into an outer surface of a rigid cure tool;
applying a release agent over the first sacrificial material;
placing a second sacrificial material into a securing groove formed into the outer surface of the rigid cure tool at a location between the cutter groove and a peripheral edge of the rigid cure tool;
placing the uncured composite material onto the rigid cure tool, covering the first sacrificial material, the release agent, and the second sacrificial material with the uncured composite material;
curing the composite material into a cured composite part, wherein the second sacrificial material is configured to bond to the composite material during cure and the first sacrificial material is prevented from bonding to the uncured composite material via the release agent during curing; and
cutting into the cured composite part and the first sacrificial material at the cutter groove, thereby releasing a portion of the cured composite part from the rigid cure tool.
14. The method of claim 13 , wherein the securing groove is substantially slanted, extending, from the outer surface of the rigid cure tool, inward in a direction angled away from the peripheral edge of the rigid cure tool.
15. The method of claim 13 , wherein the second sacrificial material is stronger than the first sacrificial material.
16. The method of claim 13 , wherein the shear strength of the cure tool is greater than the shear strength of the first sacrificial material.
17. The method of claim 13 , further comprising removing the first and second sacrificial materials from the cutter groove and the securing groove after the step of cutting the cured composite part.
18. The method of claim 13 , further comprising applying a release agent in the securing groove prior to placement of the second sacrificial material.
19. A method for curing uncured composite material, the method comprising:
placing a first sacrificial material into a cutter groove formed into an outer surface of a rigid cure tool;
applying a release agent in a securing groove formed into the outer surface of the rigid cure tool at a location between the cutter groove and a peripheral edge of the rigid cure tool;
placing a second sacrificial material into the securing groove after application of the release agent therein;
placing the uncured composite material onto the rigid cure tool, covering the first sacrificial material and the second sacrificial material with the uncured composite material;
curing the composite material into a cured composite part, wherein the second sacrificial material is configured to bond to the composite material during cure; and
cutting into the cured composite part and the first sacrificial material at the cutter groove, thereby releasing a portion of the cured composite part from the rigid cure tool.