COMPLIANT INTERMEDIATE COMPONENT OF A GAS TURBINE ENGINE
Stress mitigation feature for composite airfoil leading edge
TURBINE ENGINE ASSEMBLY AND METHOD OF MANUFACTURING THEREOF
Turbine engine assembly and method of manufacturing thereof
Turbine engine assembly and method of manufacturing thereof
TURBINE ENGINE ASSEMBLY AND METHOD OF MANUFACTURING THEREOF
GUIDING RING FOR VARIABLE-PITCH BLADES AND METHOD OF MOUNTING SAID RING
Guiding ring for variable-pitch blades and method of mounting said ring