A cover plate adapted to axially overlie root or shank portions of one or more buckets or blades secured to a turbomachine wheel, includes an arcuate cover plate body adapted to be secured to the turbomachine wheel so as to cover a root portion of at least one of the turbine buckets or blades; and a
A cover plate adapted to axially overlie root or shank portions of one or more buckets or blades secured to a turbomachine wheel, includes an arcuate cover plate body adapted to be secured to the turbomachine wheel so as to cover a root portion of at least one of the turbine buckets or blades; and at least one arcuate angel-wing seal segment detachably secured to one side of the arcuate cover plate body.
대표청구항▼
1. A cover plate adapted to axially overlie root and/or shank portions of one or more buckets or blades secured to a turbomachine wheel, comprising: an arcuate cover plate body adapted to be secured to the turbomachine wheel so as to cover a root portion of at least one of the buckets or blades, whe
1. A cover plate adapted to axially overlie root and/or shank portions of one or more buckets or blades secured to a turbomachine wheel, comprising: an arcuate cover plate body adapted to be secured to the turbomachine wheel so as to cover a root portion of at least one of the buckets or blades, wherein said arcuate cover plate body is provided with a pair of radially-spaced arcuate hooks forming opposite sides of a track; andat least one arcuate angel-wing seal segment detachably secured to one side of said arcuate cover plate body, wherein the at least one arcuate angel-wing seal segment includes an angel wing seal projecting axially, and said at least one arcuate angel-wing seal segment is provided with an arcuate rail received within the track such that opposite edges of the arcuate rail each engage one of the arcuate hooks. 2. The cover plate according to claim 1 wherein the angel wing seal on the arcuate angel-wing seal segment comprises arcuate, radially-spaced angel wing seals. 3. The cover plate according to claim 1 wherein either or both of said arcuate cover plate body and said angel-wing seal overlap side edges of more than one of said buckets or blades. 4. A cover plate configured to axially overlie root and/or shank portions of one or more buckets or blades secured to a turbomachine wheel, the cover plate comprising: an arcuate cover plate body configured to be secured to the turbomachine wheel to cover a root portion of at least one of the buckets or blades, wherein said arcuate cover plate body is provided with a radially projecting arcuate hook forming a groove; andat least one arcuate angel-wing seal segment detachably secured to one side of said arcuate cover plate body,wherein the at least one angel-wing seal segment includes an angel wing seal projecting axially, andwherein said at least one arcuate angel-wing seal segment is provided with an arcuate rail having a first-inner edge received within said groove and a second-outer edge is provided with a radially inwardly facing hook seated on a radially outer edge of said arcuate cover plate body. 5. A cover plate configured to axially overlie root and/or shank portions of one or more buckets or blades secured to a turbomachine wheel, the cover plate comprising: an arcuate cover plate body configured to be secured to the turbomachine wheel so as to cover a root portion of at least one of the buckets or blades, wherein said arcuate cover plate body is provided with an arcuate hook configured to seat in an arcuate groove at a radially inner end of said arcuate angel-wing seal segment, andat least one arcuate angel-wing seal segment detachably secured to one side of said arcuate cover plate body,wherein the at least one angel-wing seal segment includes an angel wing seal projecting axially, andwherein a radially outer end of said angel-wing seal segment is configured to seat in a hook at a radially outer edge of said arcuate cover plate body. 6. A wheel for a turbomachine rotor rotatable about an axis, said wheel comprising: a plurality of circumferentially-spaced bucket or blade slots receiving generally complimentary shaped end portions of turbomachine buckets or blades,said buckets or blades each comprising a shank, a root portion and an airfoil portion;a circumferential array of cover plate segments axially overlying at least part of said shanks and said root portions of said buckets or blades, each of said cover plate segments comprising a cover plate body attached to said wheel, wherein said at least one of the cover plate segments includes an arcuate groove andsaid seal segment having at least one angel wing seal flange extending in a generally axial direction,wherein a radially inward edge region of the seal segment is detachably fastened to at least one of the cover plate segments and a radially outward edge region of the seal segment is fastened to the at least one of the cover plate segments, andwherein said at least one seal segment is provided with a rail with a first edge received within said arcuate groove and a second edge provided with a hook received over the radially outer edge of said cover plate segments. 7. The wheel according to claim 6 wherein said at least one of the cover plate segments includes a radially outwardly facing arcuate shaped hook and a radially inwardly facing arcuate shaped hook, wherein a track is defined between the hooks, and said at least one seal segment includes a rail configured to be seated within said track. 8. The wheel according to claim 6 wherein said angel wing seal flange includes a plurality of radially-spaced angel wing seal flanges. 9. The wheel according to claim 6 wherein either or both of said arcuate cover plate body and said seal segment overlap side edges of more than one of said buckets or blades. 10. The wheel according to claim 7 wherein said rail is provided with side edges overlapping at least one side edge of an underlying cover plate body. 11. A wheel for a turbomachine rotor rotatable about an axis, said wheel comprising: a plurality of circumferentially-spaced bucket or blade slots receiving generally complimentary shaped end portions of turbomachine buckets or blades,said buckets or blades each comprising a shank, a root portion and an airfoil portion;a circumferential array of cover plate segments axially overlying at least part of said shanks and said root portions of said buckets or blades,each of said cover plate segments comprising a cover plate body attached to said wheel, wherein said cover plate segments each include an arcuate shaped hook and the seal segment includes an arcuate groove seated in the hook, andsaid seal segment having at least one angel wing seal flange extending in a generally axial direction,wherein a radially inward edge region of the seal segment is detachably fastened to at least one of the cover plate segments and a radially outward edge region of the seal segment is fastened to the at least one of the cover plate segments, andwherein a radially outer end of said seal segment is provided with a hook seated on a radially outer edge of at least one of said cover plate segments. 12. A wheel for a turbomachine rotor rotatable about an axis, said wheel comprising: a plurality of circumferentially-spaced, substantially axially-extending bucket or blade slots receiving generally complementary shaped mounting portions of turbomachine buckets or blades;a circumferential array of a cover plate segments overlying end portions of said buckets or blades and portions of a face surface of said wheel;each cover plate segment comprising a cover plate body attached to said wheel, wherein said cover plate body includes a pair of radially-spaced arcuate hooks defining there between a track; anda plurality of arcuate angel-wing seal segments detachably secured to respective cover plate bodies, wherein each of the arcuate angel-wing seal segments includes an angel wing seal flange projecting in an axial direction with respect to a rotational axis of the wheel, wherein said plurality of angel-wing seal segments are each provided with a rail received within the track. 13. The wheel according to claim 12 wherein said angel-wing seal flange includes plural angel-wing seal flanges. 14. The wheel according to claim 12 wherein each of said cover plate segments overlaps side edges of one or more adjacent buckets or blades, and each of said angel-wing seal segments is provided with side edges aligned with side edges of its respective cover plate segment. 15. The wheel according to claim 12 wherein each of said cover plate segments overlaps side edges of at least one of said buckets or blades, and each of said angel-wing seal segments overlaps at least one side edge of its respective cover plate segment. 16. The cover plate of claim 1 wherein said arcuate cover plate body and said at least one arcuate angel-wing seal segment are comprised of materials having the same or different temperature-capable properties. 17. A wheel for a turbomachine rotor rotatable about an axis, said wheel comprising: circumferentially-spaced, substantially axially-extending bucket or blade slots configured to receive complementary shaped mounting portions of turbomachine buckets or blades;a circumferential array of a cover plate segments overlying end portions of said buckets or blades and portions of a face surface of said wheel, wherein each cover plate segment includes a cover plate body attached to said wheel; andarcuate angel-wing seal segments detachably secured to respective ones of the cover plate bodies, wherein each of the arcuate angel-wing seal segments includes an angel wing seal flange projecting in an axial direction with respect to a rotational axis of the wheel, andwherein each of said angel-wing seal segments is provided with a rail with a first edge received within an arcuate groove in said cover plate segment and a second edge provided with a hook received over a radially outer edge of said cover plate body.
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이 특허에 인용된 특허 (6)
Zelesky Mark F., Cooled rotor assembly for a turbine engine.
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