IMPROVED FUEL MANIFOLD ASSEMBLY FOR COLD STARTING & HIGH ALTITUDE OPERATION OF AERO ENGINE FOR HELICOPTER

摘要

This invention relates to improved Fuel Manifold Assembly for cold starting and high altitude operation of Aero Engine for helicopter application. Thus in accordance with this invention, the Fuel Manifold assembly comprises of Principle/Main Manifold-Right Half and Principle/Main Manifold-Left Half to supply fuel to the helicopter engine during cold and altitude conditions. These parts were subjected to pressure test of 15585 kPa for 5 minutes to demonstrate 'No leakage, No Crack & No Distortion' on the geometry.