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Something I've learned from this thread is the evolution of Rolls Royce turbofans from Conway to Medway to Spey. Each step reduced LP compressor and increased HP compressor stages; 7-9, 6-11 & 5-12 and ever increasing bypass ratio; 30% (60% in final VC10 version), 70% & 100%.


In my mind this means that the Spey wasn't simply a smaller version of the Medway, it had 1 less LP compressor stage, 1 more HP compressor stage and a greater bypass ratio. Perhaps the Spey used Medway components like the combustion cans, turbines etc.


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