Seal member
A seal member is between a combustor around a rotor axis and a vane on a downstream side in an axial direction and defining a part of a combustion gas flow passage through which combustion gas is configured to flow, the seal member being configured to seal a gap between the combustor and the vane. The seal member has: an end face that faces the downstream side in the axial direction so as to face a lateral end face of the vane facing an upstream side in the axial direction; cooling channels through which cooling air is configured to be discharged from a plurality of openings defined in the end face in an array in a circumferential direction based on the rotor axis; and a clearance forming portion that protrudes further toward the downstream side in the axial direction than the end face in which the openings are defined.
1. A seal member that is configured to be between a combustor that is disposed around a rotor axis and a vane that is disposed on a downstream side in an axial direction and define a part of a combustion gas flow passage through which combustion gas is configured to flow, the seal member being configured to seal a gap between the combustor and the vane, and the seal member comprising:
an end face that faces the downstream side in the axial direction so as to face a lateral end face of the vane facing an upstream side in the axial direction;
cooling channels through which cooling air is configured to be discharged toward the lateral end face of the vane from a plurality of openings defined in the end face of the seal member in an array in a circumferential direction based on the rotor axis; and
a clearance forming portion that protrudes further toward the downstream side in the axial direction than the end face of the seal member in which the openings are defined,
wherein:
a plurality of slits is recessed in a radial direction based on the rotor axis;
each of the plurality of slits is defined in a region adjacent to at least one of the plurality of openings;
each of the plurality of slits extends only partially into the seal member in the radial direction such that a respective end of each of the respective plurality of slits is located medially in the seal member in the radial direction; and
each of the plurality of slits is at a position sandwiched between the cooling channels in the circumferential direction when viewed from the radial direction such that only one of the plurality of slits is disposed between each adjacent pair of the cooling channels in the circumferential direction.
2. The seal member according to claim 1 , wherein the seal member is configured to be further on an outer side than the combustion gas flow passage.
3. The seal member according to claim 1 , wherein the cooling channels are defined in a region in the circumferential direction including a position on the upstream side in the axial direction at which the cooling channels are configured to face a leading edge of the vane that faces the upstream side in the axial direction.
4. The seal member according to claim 1 , wherein the clearance forming portion is adjacent to at least one of the plurality of openings in the circumferential direction.
5. The seal member according to claim 1 , further comprising:
a first engaging part configured to be connected to the combustor; and
a second engaging part located downstream of the first engaging part in the axial direction and configured to be connected to an annular projection of the vane that extends upstream from the lateral end face of the vane in the axial direction,
wherein:
the second engaging part has an annular seal surface configured to be between the second engaging part and the annular projection of the vane, and
a respective end of each of the respective plurality of slits defined on an outer side relative to the combustion gas flow passage is configured to be at a position closer to the combustion gas flow passage than a position at which the annular seal surface is defined.