TM333 2B2 / TM333 2M2 Engine (ALH MK I, II & Cheetal)

General Description
Product Specifications
Gallery & Media
Point of Contact for further follow up
Others
Product Manufacturer
Hindustan Aeronautics Limited (HAL)
Product Description

TM333 2B2 / TM333 2M2 Turbo shaft engine powers ALH MK I, II & Cheetal Helicopter
respectively. These engines are repaired / overhauled under license from M/s.
Turbomeca, France.
 

Features/Roles/Variants of the product
Modular construction with annular air intake, two stage axial compressor together with a centrifugal compressor driven by a single stage turbine.
Annular reverse flow combustion chamber.
Single stage free turbine with a through shaft driving a reduction gear unit.
Full authority digital engine control. (FADEC).
Simple installation and easy access for maintenance. Low specific fuel consumption.
Product Specification
Contact : prasenjit[at]hal-india[dot]co[dot]in