Geared turbofan with fan and core mounted accessory gearboxes

作者: Claude Mercier , Robert L. Gukeisen , Thomas G. Cloft

DOI:

关键词:

摘要: A disclosed accessory drive system provides for the reduction in overall diameter of outer nacelle by splitting number components between a first gear box mounted within and second gearbox to core engine. The fan case gas turbine engine drives plurality components.

参考文章(7)
William G. Sheridan, Split accessory drive system ,(2012)
John M. Cundy, Paul M. Hield, Arthur L. Rowe, Ronald A. Midgley, Arnold C. Newton, Shaft power transfer in gas turbine engines with machines operable as generators or motors ,(1994)
Gabriel L. Suciu, Christopher M. Dye, Michael F. Cass, James S. Elder, Brian D. Merry, Gas turbine engine with stacked accessory components ,(2010)
Raymond Felix Patt, Thomas Ory Moniz, Jan Christopher Schilling, Robert Joseph Orlando, Power take-off system and gas turbine engine assembly including same ,(2007)
Todd Godleski, Jr. Robert A. Ress, Gas turbine engine accessory system ,(2009)
Zarffir A. Chaudhry, Split gearbox and nacelle arrangement ,(2007)
David S. Knott, Gareth E. Moore, David P. Scothern, David R. Trainer, Paul Simms, Gas turbine engine arrangement ,(2009)