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By A. Strang, William M. Banks, R. D. Conroy, M. J. Goulette

ISBN-10: 1861250533

ISBN-13: 9781861250537

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14. The Trent 8104 IP Turbine blade will use Rolls-Royce's latest third generation single crystal alloy, RR3010. Developed to run about 45C hotter than the previous generation material this development will enable the intermediate pressure turbine blades to remain uncooled, offering significant benefits in terms of mechanical design, engine performance and cost, Fig. 15. Airbus Industrie have recently announced the four engined long range A340 aircraft powered by the Trent 500, Fig. 16, which is a 313 passenger/8300 nm aircraft.

Another rule relates to stage loading. i The values of stage loading and flow coefficient for peak efficiency are then deduced from these diagrams and a bladepath is designed in which each stage has the same stage reaction and the same stage loading and flow coefficient. Of course, both rules are very reasonable and yield entirely viable results. However, when plotting contour lines of stage efficiency in a stage reaction versus stage loading diagram, one has to specify geometrical parameters such as blade height, chord length, cylinder diameter etc.

24 Electrical power output Industrial Trent Generating Set. at 42% efficiency is the latest addition to the power generation portfolio of gas turbines, Fig. 23. It is interesting to note that 50 MW is typically sufficient power to satisfy the demands of 50 000 people. Proven Trent 800 engine components have been used extensively in the industrial Trent with the IP, and HP compressors and turbines common. A two stage low pressure (LP) compressor replaces the aero Trent fan. Minor changes to the LP compressor blades allow for LP generating speeds of either 3 000 or 3 500 rpm and hence 50 or 60 Hz electrical generating frequencies depending on the power generation application.

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Advances in turbine materials, design and manufacturing by A. Strang, William M. Banks, R. D. Conroy, M. J. Goulette


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