초록 ▼

An inter stage seal housing for a turbine engine having upper and lower half inter stage seal housings in which a contact sealing surface of the seal housing is restored after an interval of engine operation. The contact sealing surface is restored by fitting a replaceable wear strip on the downstre

An inter stage seal housing for a turbine engine having upper and lower half inter stage seal housings in which a contact sealing surface of the seal housing is restored after an interval of engine operation. The contact sealing surface is restored by fitting a replaceable wear strip on the downstream sealing surface of the seal housing. In order to fit the replaceable wear strip, a circumferential groove is machined along an outer peripheral edge of the seal housing. The groove is machined to include axial location and radial retention such that the wear strips can be slid into the upper half and lower half inter stage seal housing circumferentially from the horizontal joint. The groove includes through holes and the wear strips include corresponding threaded holes such that the wear strips can be fastened in the groove by fasteners and fastener retention hardware.

대표청구항 ▼

1. A seal assembly for a turbine engine, comprising: a seal housing having a circumferential groove located along an edge of said seal housing, said circumferential groove having a plurality of through holes;a plurality of segments strips, each having at least one threaded hole, an upstream sealing

1. A seal assembly for a turbine engine, comprising: a seal housing having a circumferential groove located along an edge of said seal housing, said circumferential groove having a plurality of through holes;a plurality of segments strips, each having at least one threaded hole, an upstream sealing surface, a downstream sealing surface, a right circumferential sealing surface and a left circumferential sealing surface, anda plurality of fasteners for securing each of said plurality of segments strips in said circumferential groove in an annular manner to form a seal,wherein said circumferential groove is configured to accept the geometry of each of said plurality of secured segments strips,said upstream sealing surface of each of said plurality of secured segment strips forms an upstream contact sealing surface with said seal housing,said downstream sealing surface of each of said plurality of secured segment strips is arranged to form a downstream contact sealing surface with a stationary member of said turbine engine,said right circumferential sealing surface of a first of said plurality of secured segment strips forms a first circumferential contact sealing surface with a left circumferential sealing surface of a second of said plurality of secured segment strips, andsaid left circumferential sealing surface of said first of said plurality of secured segment strips forms a second circumferential contact sealing surface with a right circumferential sealing surface of the second of said plurality of secured segment strips. 2. The seal assembly according to claim 1, wherein said seal housing further comprises: a downstream surface;wherein said downstream sealing surface of each of said plurality of secured segment strips forms a substantially planar surface with said downstream surface of said seal housing and serves as a replaceable contact surface strip for said seal housing. 3. The seal assembly according to claim 1, wherein said seal housing further comprises: an upstream surface;wherein each of said plurality of through holes extend from said upstream surface to said circumferential groove. 4. The seal assembly of claim 1, wherein said first and second circumferential contact sealing surfaces are configured to prevent leakage between said first and second secured segment strips. 5. The seal assembly of claim 4, wherein said first circumferential contact sealing surface includes a step portion. 6. The seal assembly according to claim 1, wherein said plurality of fasteners prevent unwanted relative movement and wear between said seal housing and each of said plurality of secured segment strips. 7. The seal assembly according to claim 1, further comprising: fastener retention means for minimizing disbanding of the fasteners during turbine engine operation. 8. The seal assembly according to claim 1, wherein said circumferential groove includes a radial retention mechanism for retaining each of said plurality of secured segment strips in a radial direction. 9. The seal assembly of claim 8, wherein said circumferential groove includes an axial locating mechanism for positioning each of said plurality of secured segment strips in an axial direction. 10. The seal assembly according to claim 1, wherein the seal housing further comprises: an upper half seal housing;a lower half seal housing; anda horizontal split formed between said upper and lower half seal housing. 11. A method of installing segment strips in the sealing assembly of claim 10, wherein each segment strip is slid into said groove from the horizontal split of said upper and said lower seal housing and said threaded holes of each segment strip is aligned with corresponding through holes of said grooves where fasteners and fastener retention components are threaded and torque is applied. 12. A seal assembly for a turbine engine, comprising: a seal housing having a circumferential groove located along an edge of said seal housing, said circumferential groove having a plurality of through holes;at least one segment strip, each having at least one threaded hole, an upstream sealing surface, a downstream sealing surface, a right circumferential sealing surface and a left circumferential sealing surface, anda plurality of fasteners for securing said at least one segment strip in said circumferential groove,wherein said circumferential groove is configured to accept the geometry of the said at least one segment strip,wherein said plurality of fasteners comprises:a first fastener for securing and circumferentially locating said segment strip to said circumferential groove by engaging a first threaded hole of said segment strip via a first through hole of circumferential groove;a second fastener for securing said segment strip to said circumferential groove by engaging a second threaded hole of said segment strip via a second through hole of circumferential groove,wherein said second fastener has a reduced diameter portion relative to the first fastener, which creates a larger clearance between said second fastener and said second through hole than between said first fastener and said first through hole. 13. The seal assembly of claim 12, wherein said first fastener provides additional clamping force between said seal housing and said secured segment strip relative to said second fastener, and said larger clearance between said second fastener and said second through hole allows for thermal expansion of said seal housing during operation of said turbine engine. 14. A seal assembly for a turbine engine, comprising: a seal housing having a circumferential groove located along an edge of said seal housing, said circumferential groove having a plurality of through holes;a plurality of segments strips, each having at least one threaded hole, an upstream sealing surface, a downstream sealing surface, a right circumferential sealing surface and a left circumferential sealing surface, anda plurality of fasteners for securing each of said plurality of segments strips in said circumferential groove in an annular manner to form a seal,wherein said circumferential groove is configured to accept the geometry of each of said plurality of secured segments strips,said upstream sealing surface of each of said plurality of secured segment strips forms an upstream contact sealing surface with said seal housing,said downstream sealing surface of each of said plurality of secured segment strips is arranged to form a downstream contact sealing surface with a stationary member of said turbine engine,said right circumferential sealing surface of a first of said plurality of secured segment strips forms a first circumferential contact sealing surface with a left circumferential sealing surface of a second of said plurality of secured segment strips, andsaid left circumferential sealing surface of said first of said plurality of secured segment strips forms a second circumferential contact sealing surface with a right circumferential sealing surface of a third of said plurality of secured segment strips. 15. The seal assembly according to claim 14, wherein said seal housing further comprises: a downstream surface;wherein said downstream sealing surface of each of said plurality of secured segment strips forms a substantially planar surface with said downstream surface of said seal housing and serves as a replaceable contact surface strip for said seal housing. 16. The seal assembly according to claim 14, wherein said seal housing further comprises: an upstream surface;wherein each of said plurality of through holes extend from said upstream surface to said circumferential groove. 17. The seal assembly of claim 14, wherein said first and second circumferential contact sealing surfaces are configured to prevent leakage between said first and second secured segment strips and said first and third secured segment strips, respectively. 18. The seal assembly of claim 14, wherein said first circumferential contact sealing surface includes a step portion. 19. The seal assembly of claim 14, wherein said plurality of fasteners comprises: a plurality of first fasteners for securing and circumferentially locating each of said plurality of secured segment strips to said circumferential groove by engaging a first threaded hole of each of said plurality of secured segment strips via corresponding first through holes of said circumferential groove;a plurality of second fasteners for securing each of said plurality of secured segment strips to said circumferential groove by engaging a second threaded hole of each of said plurality of secured segment strips via corresponding second through holes of said circumferential groove,wherein each of said plurality of second fasteners has a reduced diameter portion relative to each of said plurality of first fasteners, which creates a larger clearance between each of said plurality of second fasteners and said corresponding second through holes than between each of said plurality of first fasteners and said corresponding first through holes. 20. The seal assembly of claim 18, wherein each said plurality of first fasteners provides additional clamping force between said seal housing and each of said plurality of secured segment strips relative to each of said plurality of second fasteners, and said larger clearance between each of said plurality of second fasteners and said corresponding second through holes allows for thermal expansion of said seal housing during operation of said turbine engine. 21. The seal assembly according to claim 14, wherein said plurality of fasteners prevent unwanted relative movement and wear between said seal housing and each of said plurality of secured segment strips. 22. The seal assembly according to claim 14, further comprising: fastener retention means for minimizing disbanding of the fasteners during turbine engine operation. 23. The seal assembly of claim 21, wherein said circumferential groove includes and a radial retention mechanism for retaining said plurality of secured segment strips in a radial direction, and an axial locating mechanism for positioning said plurality of secured segment strips in an axial direction. 24. The seal assembly according to claim 14, wherein the seal housing further comprises: an upper half seal housing;a lower half seal housing; anda horizontal split formed between said upper and lower half seal housing. 25. A method of installing segment strips in the sealing assembly of claim 14, wherein each of the plurality of segment strips is slid into said circumferential groove from the horizontal split of said upper and said lower seal housing and said threaded holes of each segment strip is aligned with corresponding through holes of said circumferential groove where fasteners and fastener retention components are threaded and torque is applied.