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PIONEERING THE POWER THAT MATTERS RR 2018 Gas turbine technology Introduction

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PIONEERING THE POWER THAT MATTERS RR 2018 Gas turbine technology Introduction ( pioneeringpower-that-matters-rr-2018-gas-turbine-technology- )

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8 Gas turbine technology Introduction to a jet engine The fan The driving force The fan module is the assembly of the fan disc, the low pressure (LP) fan shaft and the fan blades. Gas turbine technology 9 Introduction to a jet engine Its primary jobs are drawing air into the engine, compressing the bypass stream to produce 80 per cent of the engine’s thrust, and feeding air to the gas turbine core. The fan system must be strong, light and quiet. Modern fan blades are hollow for lighter weight and have a wide chord for better stiffness and strength. The engine must pass intense and rigorous testing before being certified as safe to fly. One such test is the fan blade-off test, which is conducted to demonstrate the ability of the fan casing to contain a fan blade should it become detached during engine running. Another test is the bird ingestion test, which examines the ability of the fan to withstand the impact of birds during flight. As fan intake diameter increases so too does the number of birds used to demonstrate that the engine retains its integrity and the capability to continue supplying thrust, until ultimately, it can be shut down safely. The primary purpose of the compressor is to increase the pressure of the air through the gas turbine core. It then delivers this compressed air to the combustion system. The pressure rise is created as air flows through the stages of rotating blades and static vanes. The blades accelerate the air increasing its dynamic pressure, and then the vanes decelerate the air transferring kinetic energy into static pressure rises. Our latest Trent XWB, powering the Airbus A350, uses blisks, a single component comprising both blades and a disc. These reduce the weight and improve the efficiency of the compressor by removing the need for blade roots and disc slots. The compressor Applying the pressure The compressor is made up of the fan and alternating stages of rotating blades and static vanes. The compression system of a Trent engine comprises the fan, eight intermediate pressure stages and six high pressure stages. Static Total pressure Temperature Increasing pressure and temperature through compressors Blisk The Trent 900 draws in enough air to inflate 72,000 party balloons in one second The tip of the fan blades can be travelling at speeds of over 1000mph Increasing

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