This utility model discloses a high-temperature resistant fuel
nozzle for aero-engines, relating to the field of fuel
nozzle technology. It includes a mounting ring and an air guide
assembly. The top of the air guide
assembly is fixedly connected to the bottom of the mounting ring, and a cooling
assembly is fixedly connected to the inner wall of the air guide assembly. The cooling assembly includes an inner air tube, and a
honeycomb plate is fixedly connected to the inner wall of the inner air tube. The fuel
nozzle is fixed to the outer wall of the inner air tube by a spiral ring, guiding the cooling
airflow to form a
spiral flow, increasing the contact area and turbulence intensity between the
airflow and the inner air tube, improving heat exchange efficiency, reducing the fuel passage temperature, and preventing fuel
vaporization at high temperatures from affecting injection performance. The
honeycomb plate is arranged in a ring array on the inner wall of the inner air tube, dividing the cooling
airflow into multiple fine streams that evenly cover the inner wall of the inner air tube, avoiding localized overheating. This fuel nozzle achieves the purpose of a high-temperature resistant fuel nozzle for aero-engines.