Reheat assembly for a gas turbine engine

A reheat assembly for a gas turbine engine, the reheat assembly comprising:

• a support duct section comprising a core side for facing a core reheat region, and a bypass side for facing a bypass reheat region;
• the support duct comprising a plurality of circumferentially spaced inlets, each inlet being configured to communicate the bypass reheat region with the core reheat region;
• a fuel supply system comprising a plurality of bypass fuel injection ports, each bypass fuel injection port being associated with an inlet of the plurality of inlets;
• wherein each bypass fuel injection port is configured to discharge fuel into the bypass reheat region for transit through the associated inlet into the core reheat region, wherein each inlet comprises a chute that extends through the support duct section at an oblique angle to an axial direction of the support duct.