Gas turbine ring assembly comprising ring segments having integrated interconnecting seal
The present invention presents a ring assembly 1 disposed radially outwardly of an array of circumferentially arranged blades 38 of a gas turbine engine rotor R. The ring assembly 1 includes ring segments 2 disposed circumferentially one adjacent to another and having a first circumferential end 2 a and a second circumferential end 2 b circumferentially spaced apart from each other. The first end 2 a of a ring segment 2 and the second end 2 b of an adjacent ring segment 2 of the plurality of ring segments 2 are arranged facing each other. An integrally formed projecting seal part 92 is formed at the first end 2 a . An integrally formed receiving seal part 94 is formed at the second end 2 b facing the first end 2 a . The receiving seal part 94 receives the projecting seal part 92 to form a mating connection between the ring segment 2 and the adjacent ring segment 2 . A gas turbine engine including the ring assembly 1 is also provided. Furthermore, a method of manufacturing the ring segment 2 of the ring assembly 1 is also provided.
1. A ring assembly for being disposed radially outwardly of an array of circumferentially arranged blades of a rotor of a gas turbine engine, the ring assembly comprising:
a plurality of ring segments disposed circumferentially one adjacent to another, each ring segment having a first end and a second end circumferentially spaced apart from each other;
wherein the first end of a ring segment and the second end of an adjacent ring segment from among the plurality of ring segments are configured to be arranged facing each other,
wherein an integrally formed projecting seal part is formed at the first end,
wherein an integrally formed receiving seal part is formed at the second end facing the first end, and
wherein the receiving seal part is configured to receive the projecting seal part to form a mating connection between the ring segment and the adjacent ring segment.
2. The ring assembly according to claim 1 ,
wherein the integrally formed projecting seal part is formed at the first end of each of the ring segments; and
wherein the integrally formed receiving seal part is formed at the second end of each of the ring segments.
3. The ring assembly according to claim 1 ,
wherein the first end comprises a first axial edge and a second axial edge axially spaced apart from each other, and wherein at least a first part of the projecting seal part extends from the first axial edge to the second axial edge of the first end; and
wherein the second end comprises a first axial edge and a second axial edge axially spaced apart from each other, and wherein at least a first part of the receiving seal part extends from the first axial edge to the second axial edge of the second end, corresponding to the first part of the projecting seal part.
4. The ring assembly according to claim 1 ,
wherein the first end comprises a first radial edge and a second radial edge radially spaced apart from each other, and wherein at least a second part of the projecting seal part extends towards the first radial edge and/or towards the second radial edge of the first end; and
wherein the second end comprises a first radial edge and a second radial edge radially spaced apart from each other, and wherein at least a second part of the receiving seal part extends towards the first radial edge and/or towards the second radial edge of the second end, corresponding to the second part of the projecting seal part.
5. The ring assembly according to claim 4 ,
wherein the first part and the second part of the projecting seal part intersect or join each other; and
wherein the first part and the second part of the receiving seal part intersect or join each other, corresponding the first part and the second part of the projecting seal part.
6. The ring assembly according to claim 1 , wherein the projecting seal part and the receiving seal part are curved following a circumferential direction along which the plurality of ring segments are disposed.
7. The ring assembly according to claim 1 , wherein the projecting seal part is shaped corresponding to a topological skeleton of the first end, and wherein the receiving seal part is shaped corresponding to the shape of the projecting seal part.
8. The ring assembly according to claim 1 ,
wherein the projecting seal part comprises one or more protruding lips emanating outwardly from a circumferential side surface at the first end; and
wherein the receiving seal part comprises one or more receiving grooves recessed inwardly from a circumferential side surface at the second end, corresponding to the one or more protruding lips of the projecting seal part.
9. The ring assembly according to claim 8 ,
wherein at least one integrally formed opposing receiving groove is formed at the first end, being recessed inwardly from the circumferential side surface at the first end, and
wherein at least one integrally formed opposing protruding lip is formed at the second end, emanating outwardly from the circumferential side surface at the second end, corresponding to the at least one integrally formed opposing receiving groove.
10. The ring assembly according to claim 8 ,
wherein portions of at least two protruding lips of the one or more protruding lips are parallelly disposed and spaced apart from each other; and
wherein portions of at least two receiving grooves of the one or more receiving grooves are parallelly disposed and spaced apart from each other, corresponding to the portions of the at least two protruding lips.
11. The ring assembly according to claim 8 ,
wherein the one or more protruding lips comprise at least one of a flat tip, a tapered tip, a rounded tip and a furcated tip; and
wherein the one or more receiving grooves are shaped correspondingly to the one more protruding lips.
12. The ring assembly according to claim 1 ,
wherein each of the ring segments has a radially inner gas path surface and a radially outer surface opposite to the gas path surface,
wherein at least one of the ring segments comprise one or more fixing parts extending radially outwardly from the outer surface of the ring segment for fixing the ring segment to a ring carrier of a stator of the gas turbine engine; and
wherein the projecting seal part and the receiving seal part are formed to extend along a surface of the one or more fixing parts.
13. A gas turbine engine comprising a ring assembly,
wherein the ring assembly for being disposed radially outwardly of an array of circumferentially arranged blades of a rotor of a gas turbine engine, the ring assembly comprising:
a plurality of ring segments disposed circumferentially one adjacent to another, each ring segment having a first end and a second end circumferentially spaced apart from each other;
wherein the first end of a ring segment and the second end of an adjacent ring segment from among the plurality of ring segments are configured to be arranged facing each other,
wherein an integrally formed projecting seal part is formed at the first end,
wherein an integrally formed receiving seal part is formed at the second end facing the first end, and
wherein the receiving seal part is configured to receive the projecting seal part to form a mating connection between the ring segment and the adjacent ring segment.
14. The gas turbine engine according to claim 13 ,
wherein the integrally formed projecting seal part is formed at the first end of each of the ring segments; and
wherein the integrally formed receiving seal part is formed at the second end of each of the ring segments.
15. The gas turbine engine according to claim 13 ,
wherein the first end comprises a first axial edge and a second axial edge axially spaced apart from each other, and wherein at least a first part of the projecting seal part extends from the first axial edge to the second axial edge of the first end; and
wherein the second end comprises a first axial edge and a second axial edge axially spaced apart from each other, and wherein at least a first part of the receiving seal part extends from the first axial edge to the second axial edge of the second end, corresponding to the first part of the projecting seal part.
16. The gas turbine engine according to claim 13 ,
wherein the first end comprises a first radial edge and a second radial edge radially spaced apart from each other, and wherein at least a second part of the projecting seal part extends towards the first radial edge and/or towards the second radial edge of the first end; and
wherein the second end comprises a first radial edge and a second radial edge radially spaced apart from each other, and wherein at least a second part of the receiving seal part extends towards the first radial edge and/or towards the second radial edge of the second end, corresponding to the second part of the projecting seal part.
17. The gas turbine engine according to claim 16 ,
wherein the first part and the second part of the projecting seal part intersect or join each other; and
wherein the first part and the second part of the receiving seal part intersect or join each other, corresponding the first part and the second part of the projecting seal part.
18. The gas turbine engine according to claim 13 , wherein the projecting seal part and the receiving seal part are curved following a circumferential direction along which the plurality of ring segments are disposed.
19. A ring segment of a ring assembly for being circumferentially disposed radially outwardly of an array of blades of a rotor of a gas turbine engine, the ring segment comprising:
a first end and a second end circumferentially spaced apart from each other;
wherein the first end comprises at least one integrally formed protruding lip emanating outwardly from a circumferential side surface at the first end,
wherein the second end comprises at least one integrally formed receiving groove recessed inwardly from a circumferential side surface at the second end, and
wherein the at least one integrally formed receiving groove is correspondingly shaped so that the shape of the at least one integrally formed receiving groove may mate with the shape of the at least one integrally formed protruding lip.
20. The ring segment according to claim 19 ,
wherein the at least one integrally formed protruding lip and the at least one integrally formed receiving groove are curved following a circumferential direction along which the ring assembly is disposed.