Mavadkaran Company

Established in 1990, Mavadkaran Engineering has boasted more than two decades of consistent knowledge-based experience. It has based its key strategy on manufacturing and reconstructing hot section and blades in gas turbines’ air compressors that are used in power plant, oil & gas, and petrochemical industries.
 
Company’s first experience was engineering the first row moving blades of a 25 MW turbine in early 90s through efforts by its experts along with laboratory and manufactory facilities and equipment. In a few years, Mavadkaran succeeded in achieving technical knowledge to manufacture hot parts of turbines, particularly their blades.
 
As the first turbine blade manufacturer of the country, Mavadkaran has been the focus of attention of oil & gas, petrochemical, and power plant industries for years.
 

What we manufacture

• Fixed and moving blades of Rolls Royce Avon Turbines’ hot section
• Fixed and moving blades of Rolls Royce Avon Turbines’ compressor
• Fixed and moving blades of Ruston TA1750 Turbines’ hot section
• Fixed and moving blades of Ruston TB4000 Turbines’ hot section
• Fixed and moving blades of Ruston EM85 Turbines’ hot section
• Fixed and moving blades of Sulzer S7 Turbines’ hot section
• Moving blades of BBC D9 Turbines’ hot section
• Fixed and moving blades of BBC D13 Turbines’ hot section
• Moving blades of GE Frame 6 Turbines’ hot section
• Moving blades of GE Frame 5 (MS5001, MS 5002) Turbines’ hot section
• Fixed and moving blades of NP GE10-2 Turbines’ hot section
• Fixed and moving blades of SGT600 – Siemens Turbines’ hot section
• First-row moving blades of Acec (Fiat) turbines
• Combustion Chamber of GEF9, GEF6, Rolls Royce, Zorya Turbines
• TP Part of GE F9, GE F6 Turbines
• Shroud section of GE F9, GE F6, Zorya Turbines
• Rotating and fixed blades of Solar Scentaur turbine’s hot part
• Rotating and fixed blades of Zorya DU80 turbine’s hot part
• moving blades of GE MS 1002 turbine’s hot part

 
Services we undertake

• Reconstructing various components of rotating hot blades
• Reconstructing various components of fixed hot blades
• Reconstructing various components of combustion chamber, TP, and shroud