Combustor and rotating machine

A combustor comprising:

• a fuel nozzle comprising a pilot nozzle extending along an axis, and a plurality of main nozzles disposed in a circumferential direction of the axis at intervals and configured to inject fuel from at least one thereof;
• a combustor basket configured to surround the fuel nozzle from an outer circumferential side;
• and
• a plurality of connecting members provided on an upstream side of the axis with respect to the main nozzles, disposed such that a longitudinal direction of the connecting members is disposed in the axial direction of the combustor basket, and is fixed to be inclined in the circumferential direction as a short-length direction of the connecting members is disposed toward the outside in the radial direction of the combustor basket, installed in the circumferential direction at intervals to connect the rear end of the combustor basket and a casing, and configured to define a flow path through which compressed air introduced into the combustor basket flows,
• wherein the connecting member is formed with a fuel path,
• wherein a fuel injection hole is formed in a surface of the connecting member and is configured to inject fuel from the fuel path,
• wherein a circulation direction of the compressed air flowing through the flow path is configured to be reversed at a rear end of the combustor basket, and the compressed air is introduced into the main nozzles, and
• wherein the flow path is partially or entirely inclined in the circumferential direction to blow the compressed air.