Exhibitions
31/07/09 Aerospect System Launched for GE90 Turbine Engine!
What are the benefits to the MRO?Knowing if a set of components will or will not meet specification prior to assembly cannot be understated. The build process becomes more predictable allowing better scheduling and planning and even increasing throughput; use of the Aerospect system in nearly all cases reduces the build time by greater than 40%. Â |
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Benefits to the end userLike all transport industries fuel prices and more importantly environmental issues are forcing change to engine technology and in particular the aerospace industry. Â |
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Benefits to the environmentAs previously stated the more aligned the High Pressure compressor the more fuel efficient the engine becomes and in turn the lower the emissions, fractions of a percentage in efficiency relates to thousands of tonnes reduction in CO2 emissions. An accurate and smooth running engine will produce less vibration and as a consequence noise pollution is kept to a minimum. Aerospect system for stacking the GE90 High Pressure Compressor and turbine assemblies. The Aerospace industry has been using Aerospect systems to stack turbine components for over 10 years now, so when we were asked to develop a system for stacking GE90 components our engineers rose to the challenge. Â |
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The GE90 is the worlds most powerful turbofan engine with a thrust rating up to an incredible 115,000 lb, in fact the GE90 – 115B set the world record for thrust levels (commercial aircraft) by attaining 127,900 pounds of thrust during final certification back in 2002; the previous record was set by the same engine back in 2001. Not only does the GE90 engine hold the record for being the most powerful commercial jet engine it also holds the record for the longest flight by a commercial airliner. Powering a 777-200LR the flight from Hong Kong to London took 22Hours 42 minutes and covered 13,422 miles (21,601Km). Those that have flown from Hong Kong to London will realise that this was not the shortest route between these locations, in actual fact the flight went over the pacific, across the US and over the Atlantic. This is where the Aerospect stack prediction system comes in to use, the Aerospect system (see fig 1) allows engine MRO and manufacturers to build component parts of the engine in such a way that axial and radial rotational errors are kept to a minimum. The Aerospect employs a simple philosophy “if the part rotates then the best method of measurement is in rotationâ€. The system consists of a high load capacity air bearing spindle that allows component weights of up to 2500Lb. Made from hardened tool steel mounted on a granite plate the spindle provides a high degree of accuracy while maintaining the shop floor robustness required during the engine build and alignment process. Measurements are taken using multiple gauge heads conveniently located on adjustable columns and arms, these posts and arms provide easy access to relevant features and assemblies of the compressor. When it comes to stacking, the user can carry out a virtual build of the complete compressor or individual assemblies using pre-measured parts, each of which has been marked with an SP value (Stack Projection value) and angular position. The Aerospect stack prediction software will tell the user not only if these stacked parts will meet the defined axial tolerance but will also propose the best orientation of the components (see inset). The user can then start the build process but at the same time continue to measure the stacked components as their built. The first part of the high pressure compressor (stage 1 disk) is placed on a specially made hydraulic chuck; this fixture allows the user to grip the component on the inner shaft using a preset and specified load (see inset). Two gauges located at the base of the Aerospect system are then used to establish an axis of rotation on the shaft while all adjustable gauges are used to measure radial and axial run-out of the connecting portions of the compressor. These gauges allow measurement of lower and upper surfaces (flatness mode) as well as inner and outer diameters (roundness mode).The next stages of the compressor can be placed on the stage 1 disk and located in an angular position as specified by pre-defined calculations and measurements. Once these stages are put together its possible to re-establish a new stack prediction value and position ready for the next part of the build. This sort of process continues until the complete compressor is built up.  |
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The Aerospect system greatly reduces the likelihood of having to breakdown the compressor saving time and money. Not only does the GE90 HPC require good alignment but the point at which the compressor connects to the high pressure turbine is also critical. Misalignment of these joints can cause a banana or crank type action that greatly affects the performance of the combined parts. The Aerospect Stack prediction system ensures alignment of the compressor and turbine assembly is kept to an optimum. Â |
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