Combustor and gas turbine

A combustor comprising:

• a nozzle main body that includes:
• a shaft body which extends along an axis and has, inside the shaft body, a purge air flow path, which extends along the axis to a tip portion of the shaft body and is configured to allow a compressed air flow, an air spraying hole formed in the tip portion of the shaft body, and a fuel flow path which is configured to allow a fuel flow,
• a swirling blade, which overhangs from an outer surface of the shaft body in a radial direction of the shaft body, wherein the radial direction is perpendicular to the axis, and which swirls a fluid flowing along the axis from an upstream end of the shaft body to a downstream end of the shaft body along an axial direction, and
• a fuel spraying hole which is formed in the swirling blade, the fuel spraying hole connected to the fuel flow path and configured to inject the fuel flow;
• and
• a sealing member that seals the air spraying hole,
• wherein the sealing member is formed of a metal having a melting point lower than a melting point of a metal forming the nozzle main body,
• wherein the tip portion of the shaft body is formed in a tapered shape tapering off toward the downstream end of the shaft body,
• wherein the air spraying hole is configured to connect the purge air flow path to the outer surface of the shaft body upon being opened by melting of the scaling member, and
• wherein the air spraying hole is angled with respect to the axis, and is configured to inject the compressed air flow toward the downstream end of the shaft body.