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US 12,215,062 B2Granted
Multi-stage consolidation process for ceramic matrix composite prepreg material
AssigneeROLLS-ROYCE plc
InventorsVirtudes Rubio Diaz, Matthew Hocking
Life of this patent
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Abstract
A method used for forming ceramic matrix composite components includes several steps. The method comprises arranging a layup of a predetermined number of prepreg ceramic plies on a layup too and a plurality of different stages to debulk and consolidate the layup.
Claims20
A method comprising:
- arranging a layup of a predetermined number of impregnated ceramic plies on a layup tool, performing a preliminary consolidation stage comprising:
- assembling a set of preliminary consolidation consumables over the layup, applying a vacuum pressure to withdraw air between the set of preliminary consolidation consumables and the layup, and heating the layup to a first predetermined temperature for a predetermined preliminary consolidation period to partially cure the layup, performing a final consolidation stage comprising:
- assembling a set of final consolidation consumables over the layup once the set of preliminary consolidation consumables are removed from the layup, the set of final consolidation consumables having a lower flexibility and a higher temperature capability than the set of preliminary consolidation consumables, applying a vacuum pressure to withdraw air between the set of final consolidation consumables and the layup, and heating the layup to a second predetermined temperature greater than the first predetermined temperature for a predetermined final consolidation period to fully cure the layup, wherein the set of preliminary consolidation consumables includes a perforated release film layer, a plurality of thin breather layers, a thick breather layer, and a vacuum stretch bag and wherein assembling the set of preliminary consolidation consumables over the layup comprises overlaying the perforated release film layer directly over an exposed surface of the layup, overlaying the plurality of thin breather layers directly over the perforated release film layer, overlaying the thick breather layer directly over the thin breather layers, and overlaying the vacuum stretch bag directly over the thick breather layer, and wherein the set of final consolidation consumables includes a perforated release film layer, a release film layer, first and second thick breather layers, and a high-temperature stretch bag and wherein assembling the set of final consolidation consumables over the layup comprises overlaying the perforated release film layer directly over an exposed surface of the layup, overlaying the first thick breather layer directly over the perforated release film layer, overlaying the release film layer directly over the first thick breather layer, overlaying the second thick breather layer directly over the release film layer, and overlaying the high-temperature stretch bag directly over the second thick breather layer.
A method comprising arranging a layup of a predetermined number of prepreg ceramic plies on a layup tool;
- performing an intermediate debulk stage comprising the steps of:
- assembling a set of intermediate stage consumables over the layup, infiltrating the layup with a matrix material, and applying a vacuum pressure for a predetermined intermediate debulk period to withdraw air between the set of intermediate stage consumables and the layup to bleed excess matrix material over an entire surface of the layup;
- performing an extended debulk stage comprising the steps of:
- assembling a set of extended stage consumables over the layup once the set of intermediate stage consumables are removed from the layup, the set of extended stage consumables is different from the set of intermediate stage consumables, infiltrating the layup with the matrix material, and applying a vacuum pressure for a predetermined extended debulk period that is greater than the predetermined intermediate debulk period to withdraw air between the set of extended stage consumables and the layup to bleed excess matrix material over the entire surface of the layup;
- performing a preliminary consolidation stage comprising:
- assembling a set of preliminary consolidation consumables over the layup, applying a vacuum pressure to withdraw air between the set of preliminary consolidation consumables and the layup, and heating the layup to a first predetermined temperature for a predetermined preliminary consolidation period to partially cure the layup, performing a final consolidation stage comprising:
- assembling a set of final consolidation consumables over the layup once the set of preliminary consolidation consumables are removed from the layup, the set of final consolidation consumables having a lower flexibility and a higher temperature capability than the set of preliminary consolidation consumables, applying a vacuum pressure to withdraw air between the set of final consolidation consumables and the layup, and heating the layup to a second predetermined temperature greater than the first predetermined temperature for a predetermined final consolidation period to fully cure the layup.
4 more elements
Dependencies are inferred from the claim text.