Patent ID: 9121351
Filing Date: 2015-09-01
Classification: F02C,F02K,F05D

Abstract:
1. An apparatus comprising: a gas turbine engine having a shaft operable to transmit mechanical power; a first flow path disposed internal to the gas turbine engine and defined by an inner first flow path wall and an outer first flow path wall; a second flow path disposed radially inward of the first flow path in the gas turbine engine and defined by an inner second flow path wall and an outer second flow path wall; a gearing operably coupled to the shaft and disposed between the first flow path and the second flow path wherein the gearing is operable to integrate with an accessory system; and a multi-pad accessory mount disposed between the inner first flow path wall of the first flow path and the outer second flow path wall of the second flow path, the multi-pad accessory mount coupled to the gearing; wherein the multi-pad accessory mount is located in a fan frame of the gas turbine engine.