Claims
- 1. A ceramic seal for sealing between two structures that may experience relative radial and axial motion comprising:
a plurality of annular ceramic diaphragm members having an inner diameter portion and an outer diameter portion wherein said inner diameter portion is generally continuous and said outer diameter portion is segmented; said outer diameter portion having a plurality of radially extending finger elements defining an outer circumference and generally uniformly spaced apart having a gap formed therebetween; said ceramic diaphragm members laminated together and fastened along said inner diameter portion wherein adjacent ceramic diaphragm members are oriented such that said finger elements of one ceramic diaphragm member block said gaps of a second ceramic diaphragm member; and said ceramic diaphragm members disposed between a pair of spacers fixidly attached for attachment to a structure.
- 2. The ceramic seal as in claim 1 wherein said outer diameter portion having at a terminus end of said gaps a keyhole formed therein to reduce stress caused by flexure of said finger elements.
- 3. The ceramic seal as in claim 1 wherein said finger elements having a foot portion at an outermost end for sealing engagement with a structure.
- 4. The ceramic seal as in claim 1 wherein said ceramic annular diaphragm members are comprised of a plurality of diaphragm segments attached end to end by a high temperature joining compound.
- 5. The ceramic seal as in claim 1 wherein said ceramic diaphragm members and said spacers are fixedly attached between a pair of end plates for attachment to said structure.
- 6. The ceramic seal as in claim 5 wherein said ceramic diaphragm members, said spacers and said end plates are clamped to a housing for positioning of the seal adjacent a turbine combustor exit nozzle and said finger elements engage a combustor liner.
- 7. The ceramic seal as in claim 5 wherein said ceramic diaphragm members, said spacers and said end plates are clamped to a rotatable shaft and said finger elements engage a shaft housing.
- 8. A ceramic seal for sealing between two structures that may experience relative radial and axial motion comprising:
a plurality of annular ceramic diaphragm members having an inner diameter portion and an outer diameter portion wherein said inner diameter portion is segmented and said outer diameter portion is generally continuous; said inner diameter portion having a plurality of radially extending finger elements defining an inner circumference and generally uniformly spaced apart having a gap formed therebetween; said ceramic diaphragm members laminated together and fastened along said outer diameter portion wherein adjacent ceramic diaphragm members are oriented such that said finger elements of one ceramic diaphragm member block said gaps of a second ceramic diaphragm member; and said ceramic diaphragm members disposed between a pair of spacers fixedly attached for attachment to a structure.
- 9. The ceramic seal as in claim 8 wherein said inner diameter portion having at a terminus end of said gaps a keyhole formed therein to reduce stress caused by flexure of said finger elements.
- 10. The ceramic seal as in claim 8 wherein said finger elements having a foot portion at an outermost end for sealing engagement with said structure.
- 11. The ceramic seal as in claim 8 wherein said ceramic annular diaphragm members are comprised of a plurality of diaphragm segments attached end to end by a high temperature joining compound.
- 12. The ceramic seal as in claim 8 wherein said ceramic diaphragm members and said spacers are fixedly attached between a pair of end plates for attachment to said structure.
- 13. The ceramic seal as in claim 12 wherein said ceramic diaphragm members, said spacers and said end plates are clamped to a housing for positioning of the seal adjacent a combustor exit nozzle and said finger elements engage a combustor liner.
- 14. The ceramic seal as in claim 12 wherein said ceramic diaphragm members, said spacers and said end plates are clamped to a shaft housing and said finger elements engage a rotatable shaft.
- 15. A ceramic seal for air sealing between a housing and a combustor liner comprising:
a plurality of annular ceramic diaphragm members having an inner diameter portion and an outer diameter portion wherein said inner diameter portion is generally continuous and said outer diameter portion is segmented; said outer diameter portion having a plurality of radially extending finger elements defining an outer circumference, wherein said finger elements having a foot portion at an outermost end for sealing engagement with a combustor liner, and generally uniformly spaced apart having a gap formed therebetween wherein said outer diameter portion having at a terminus end of said gaps a keyhole formed therein; said ceramic diaphragm members laminated together and fastened along said inner diameter portion wherein adjacent ceramic diaphragm members are oriented such that said finger elements of one ceramic diaphragm member block said gaps of a second ceramic diaphragm member; and said ceramic diaphragm members disposed between a pair of spacers and the combination fixidly attached between a pair of end plates for attachment to a housing.
- 16. The seals as in claim 15 wherein said ceramic diaphragm members, said spacers and said end plates are clamped to the housing for positioning the ceramic seal adjacent a combustor exit nozzle and said finger elements engage a combustor liner.
- 17. A ceramic seal for fluid sealing between a housing and a rotatable shaft comprising:
a plurality of annular ceramic diaphragm members having an inner diameter portion and an outer diameter portion wherein said inner diameter portion is segmented and said outer diameter portion is generally continuous; said inner diameter portion having a plurality of radially extending finger elements defining an inner circumference, wherein said finger elements having a foot portion at an outermost end for sealing engagement with a rotatable shaft, and generally uniformly spaced apart having a gap formed therebetween wherein said inner diameter portion having at a terminus end of said gaps a keyhole formed therein; said ceramic diaphragm members laminated together and fastened along said outer diameter portion wherein adjacent ceramic diaphragm members are oriented such that said finger elements of one ceramic diaphragm member block said gaps of a second ceramic diaphragm member; and said ceramic diaphragm members disposed between a pair of spacers and the combination fixedly attached between a pair of end plates for attachment to a housing.
- 18. The seal as in claim 17 wherein said ceramic diaphragm members, said spacers and said end plates are clamped to the housing and said finger elements engage a rotatable shaft.
- 19. A method for fabrication of a ceramic seal for sealing between two structures that experience relative radial and axial motion, the steps comprising:
preparing thin ceramic sheets of a ceramic material using a high shear roll compaction process; cutting by use of a laser a plurality of annular ceramic diaphragm members and further cutting a plurality of finger elements and a plurality of apertures defined therein resulting in a rolled edge on the finger; laminating a plurality of ceramic diaphragm members having a generally continuous diameter portion and a segmented diameter portion; orienting the ceramic diaphragm members such that the segmented diameter portion comprising a plurality of radial extending finger elements having a gap formed therebetween have the finger elements of one ceramic diaphragm member covering the gaps of an adjacent ceramic diaphragm member; and assembling the ceramic diaphragm members between a pair of spacers and attaching the assembly between a pair of endplates to form an annular seal.
- 20. The method as in claim 19 wherein the laminating further comprises the step of:
bonding of adjacent ceramic diaphragm members with a high temperature joining compound on the continuous diameter portion of each.
- 21. The method as in claim 19 wherein the ceramic material is selected from one of the group of materials: silicon nitride, silicon carbine, aluminum oxide and zirconia.
- 22. The method as in claim 19 wherein the thin ceramic sheets are approximately between 0.020 inches and 0.040 inches thick.
- 23. The method as in claim 19 wherein the annular ceramic diaphragm members are comprised of a plurality of ceramic diaphragm segments attached end to end by bonding using a high temperature joining compound.
- 24. A method for fabricating of a ceramic seal for sealing between two structures that experience relative radial and axial motion, the steps comprising:
preparing thin ceramic sheets of a ceramic material; cutting by use of a laser a plurality of ceramic diaphragm segments and further cutting a plurality of finger elements and a plurality of apertures defined therein; laminating a plurality of ceramic diaphragm segments end to end by bonding using a ceramic cement thereby forming a plurality of annular ceramic diaphragm members; laminating a plurality of ceramic diaphragm members having a generally continuous diameter portion and a segment diameter portion; orienting the ceramic diaphragm members such that the segmented diameter portion comprising a plurality of radial extending finger elements having a gap formed therebetween have the finger elements of one ceramic diaphragm member covering the gaps of an adjacent ceramic diaphragm member; and assembling the annular ceramic diaphragm members between a pair of spacers and attaching the assembly between a pair of endplates to form an annular seal.
- 25. The method as in claim 24 wherein the laminating further comprises the step of:
bonding of adjacent ceramic diaphragm members with a high temperature joining compound on the continuous diameter portion of each.
- 26. The method as in claim 24 wherein the ceramic material is selected from one of the group of materials: silicon nitride, silicon carbine, aluminum oxide and zirconia.
- 27. The method as in claim 24 wherein the thin ceramic sheets are approximately between 0.020 inches and 0.040 inches thick.
GOVERNMENT RIGHTS
[0001] This invention was made with Government support under Contract No. N00421-97-C-1049 awarded by the U.S. Navy, BAA High Temperature Rise Combustor Program. The Government has certain rights in this invention.