18492837. TURBINE ENGINE HAVING A VARIABLE PITCH AIRFOIL ASSEMBLY (General Electric Company)
TURBINE ENGINE HAVING A VARIABLE PITCH AIRFOIL ASSEMBLY
Organization Name
Inventor(s)
Abhijeet Jayshingrao Yadav of Bangalore (IN)
Nicholas Joseph Kray of Mason OH (US)
TURBINE ENGINE HAVING A VARIABLE PITCH AIRFOIL ASSEMBLY
This abstract first appeared for US patent application 18492837 titled 'TURBINE ENGINE HAVING A VARIABLE PITCH AIRFOIL ASSEMBLY
Original Abstract Submitted
A turbine engine comprising a fan section, a compressor section, a combustion section, and a turbine section in serial flow arrangement and defining a stator portion and a rotor portion, which rotates about an engine centerline. The rotor portion comprising a variable pitch airfoil assembly. The variable pitch airfoil assembly having an airfoil and a balancing insert.