Variable pitch rotor with remote counterweight
A counterweight, pitch angle technology, applied in non-variable volume pumps, components of pumping devices for elastic fluids, pump components, etc., can solve problems such as limiting design flexibility
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[0037] Referring to the drawings in which like reference numerals denote like elements in the various figures, figure 1 A gas turbine engine 10 is depicted. Engine 10 has a longitudinal axis 11 and includes a fan 12 and a low pressure turbine ("LPT") 16, collectively referred to as the "low pressure system". LPT 16 drives fan 12 via an internal shaft 18, also referred to as the "LP shaft". Engine 10 also includes a high pressure compressor ("HPC") 20, a combustor 22, and a high pressure turbine ("HPT") 24, collectively referred to as a "gas generator" or "core". HPT 24 drives HPC 20 via external shaft 26, also referred to as the "HP shaft". In summary, the high and low pressure systems can be operated in a known manner to produce primary or core flow, as well as fan or bypass flow. Although engine 10 is shown as a high-bypass turbofan engine, the principles described herein are equally applicable to any other type of engine requiring variable pitch blades, including turbopr...
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