Patent ID: 11891957
Assignee: MITSUBISHI ELECTRIC CORPORATION
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC F | IPC F

Claim 6:
7. A gas turbine comprising:
the outlet seal according to claim 1;
the combustor; and
the turbine, wherein
the combustor includes a combustion tube extending in a direction including a directional component of the axial direction, a burner that sprays fuel into a combustion space that is a space on an inner peripheral side of the combustion tube, and the outlet flange extending from an end on the axial second side of the combustion tube in the radial direction,
the turbine includes a turbine rotor that rotates around the axis, a turbine casing covering the turbine rotor, and a plurality of stator vane rows attached to the turbine casing,
the turbine rotor includes a rotor shaft around the axis and a plurality of rotor blade rows attached to the rotor shaft,
the plurality of rotor blade rows are arranged in the axial direction,
each of the plurality of stator vane rows is disposed on the axial first side with respect to one rotor blade row of the plurality of rotor blade rows,
each of the plurality of stator vane rows includes a plurality of stator vanes arranged in the circumferential direction,
each of the plurality of stator vanes includes a vane body extending in the radial direction and a shroud formed at an end of the vane body in the radial direction, and
the outlet seal connects the outlet flange of the combustion tube and a shroud of a first stage stator vane provided in a first stage stator vane row on a most axial first side among the plurality of stator vane rows.