Integrating a fuel plenum into the burner base eliminates complex sealing surfaces and reduces manufacturing costs.
A gas turbine injector features a rotatable injection head driven by an actuator to adjust fluid spray orientation along the longitudinal axis.
Integrating a cooling channel into the stud structure directs airflow to the stud root, preventing hot spots and maintaining structural integrity.
Segmented wear strips with interlocking projections isolate shell wear, eliminating L-ring flaking to extend component service life.
Segmented front and rear block compressors transition between high and low power modes to maintain engine pressure ratios.