Process method to repair bismaleimide (BMI) composite structures
AssigneeThe Boeing Company
InventorsRussell L. Keller, Wesley S. Owen
Life of this patent
Estimating the term…
Abstract
A method for repairing a damaged area, referred to as the repair area, of a composite structure comprises steps of: making alignment markings on the repair area; fabricating a pair of alignment templates; preparing the repair area for a hot bonded, vacuum bagged repair; assembling a repair patch; consolidating the repair patch; heating the repair patch; transferring and aligning the repair patch to the repair area; vacuum bagging, heating, and cooling the repair patch for a partial cure at the repair area; heating and cooling the repair patch in an oven; and bonding the repair patch to the repair area.
Claims22
A method for repairing a damaged repair area of a composite structure, comprising steps of:
- making alignment markings on the repair area;
- fabricating a pair of alignment templates;
- preparing the repair area for a hot bonded, vacuum bagged repair;
- assembling a repair patch;
- consolidating said assembled repair patch;
- heating said consolidated repair patch;
- transferring and aligning said consolidated and heated repair patch to the repair area;
- vacuum bagging, heating, and cooling said transferred and aligned repair patch at the repair area;
- removing said vacuum bagged, heated and cooled repair patch from the repair area heating and cooling said removed repair patch in an oven;
- and
- bonding said oven heated and cooled repair patch to the repair area.
A method for repairing a damaged repair area of a composite structure, comprising steps of:
- making alignment markings on the repair area;
- fabricating a pair of alignment templates;
- preparing the repair area for a hot bonded, vacuum bagged repair by:
- installing thermocouples in the repair area,
- removing a flash tape in a bond area of the repair area and leaving the flash tape outside of the bond area, and
- covering the repair area with a solid separator film;
- assembling a repair patch by:
- cutting to size plies of fiber-reinforced bismaleimide repair material,
- fabricating a ply lay-up template,
- taping a first of said pair of alignment templates on said ply lay-up template,
- laying up said plies on said first of said pair of alignment templates, and
- affixing a second of said pair of alignment templates to said repair material;
- consolidating said assembled repair patch;
- heating said consolidated repair patch;
- transferring and aligning said consolidated and heated repair patch to the repair area by:
- transferring said repair patch to the repair area,
- aligning one of said pair of alignment templates with said alignment markings on the repair area,
- rotating said repair patch to contact said solid separator film covering the repair area, and
- removing said one of said pair of alignment templates from said repair patch;
- vacuum bagging, heating, and cooling said transferred and aligned repair patch at the repair area;
- removing said bagged, heated and cooled repair patch from the repair area heating and cooling said removed repair patch in an oven;
- and
- bonding said oven heated and cooled repair patch to the repair area.
A method for repairing a damaged repair area of a composite structure, comprising steps of:
- making alignment markings on the repair area;
- fabricating a pair of alignment templates by centering a piece of transparent bagging film over the repair area and tracing said alignment markings onto said transparent bagging film;
- preparing the repair area for a hot bonded, vacuum bagged repair by:
- installing thermocouples in the repair area,
- removing a flash tape in a bond area of the repair area and leaving the flash tape outside of the bond area, and
- covering the repair area with a solid separator film;
- assembling a repair patch by:
- cutting to size plies of fiber-reinforced bismaleimide repair material,
- fabricating a ply lay-up template,
- taping a first of said pair of alignment templates on said ply lay-up template,
- laying up said plies on said alignment template, and
- affixing a second of said pair of alignment templates in an alignment template assembly to said repair material;
- consolidating said assembled repair patch by:
- covering a center area of a plate with insulation,
- covering said insulation with a heating blanket,
- placing a thin copper sheet over said heating blanket,
- covering said copper sheet with a non-porous separator film,
- transferring said repair patch onto said non-porous separator film, largest ply down,
- removing one of said pair of alignment templates from said repair patch,
- placing thermocouples around said repair patch,
- placing a porous separator film onto said repair patch,
- placing a pricked non-porous separator film onto said porous separator film,
- placing a first fiberglass cloth over said pricked non-porous separator film,
- vacuum bagging said insulation, said heating blanket, said copper sheet, said non-porous separator film, said repair patch with said alignment template assembly, said thermocouples, said porous separator film, said pricked non-porous separator film, and said first fiberglass cloth using a lower vacuum bag,
- applying a first vacuum to said lower vacuum bag,
- placing a second fiberglass cloth onto said lower vacuum bag,
- placing a rigid box onto said second fiberglass cloth wherein said rigid box is substantially centered over said repair patch,
- placing a third fiberglass cloth over said rigid box,
- vacuum bagging said rigid box using an upper vacuum bag, and
- applying a second vacuum to said upper vacuum bag, wherein said second vacuum is at a level ranging between zero inches through approximately one inch of mercury less than said first vacuum;
- heating said consolidated repair patch by:
- heating said repair patch at a rate of 3° F. per minute to approximately 250° F.,
- holding said repair patch at approximately 250° F. for approximately 15 minutes,
- releasing said second vacuum from said upper vacuum bag, opening said upper vacuum bag, and removing said rigid box;
- said third fiberglass cloth, and said second fiberglass cloth,
- holding said repair patch at approximately 250° F. for approximately 15 minutes, and
- removing said repair patch from said lower vacuum bag;
- transferring and aligning said consolidated and heated repair patch to the repair area by:
- transferring said repair patch to the repair area,
- aligning said alignment template assembly with said alignment markings on the repair area,
- rotating said repair patch to contact said solid separator film covering the repair area, and
- removing said alignment template assembly from said repair patch;
- vacuum bagging, heating, and cooling said transferred and aligned repair patch at the repair area by:
- placing a precut perforated separator film over the repair patch,
- placing a fourth fiberglass cloth over said precut perforated separator film,
- placing a second solid separator film over said fourth fiberglass cloth,
- placing a heat blanket over said second solid separator film,
- placing a fifth fiberglass cloth over said heat blanket,
- vacuum bagging said repair patch,
- heating said repair patch at a rate of 3° F. per minute to approximately 350° F.,
- holding said repair patch at approximately 350° F. for approximately 3 hours, and
- cooling said repair patch at a rate of 3° F. per minute to approximately ambient temperature;
- removing said vacuum bagged, heated and cooled repair patch from the repair area heating and cooling said removed repair patch in an oven by:
- marking orientation on the repair patch;
- removing the repair patch from the repair area,
- placing the repair patch in an oven,
- heating said repair patch at a rate of 3° F. per minute to approximately 375° F.,
- holding said repair patch at approximately 375° F. for approximately 3 hours,
- heating said repair patch at a rate of 3° F. per minute to approximately 440° F.,
- holding said repair patch at approximately 440° F. for approximately 6 hours, and
- cooling said repair patch at a rate of 3° F. per minute to approximately ambient temperature;
- and
- bonding said oven heated and cooled repair patch to the repair area.
Dependencies are inferred from the claim text.