초록 ▼

A method for servicing a gas turbine engine includes providing access from a forward section of the gas turbine engine to a gearbox contained within a bearing compartment. A gas turbine is also disclosed in which a bearing package is mounted to a front center body support and a low spool. A front wa

A method for servicing a gas turbine engine includes providing access from a forward section of the gas turbine engine to a gearbox contained within a bearing compartment. A gas turbine is also disclosed in which a bearing package is mounted to a front center body support and a low spool. A front wall is removable from the front center body support to provide access to the gearbox.

대표청구항 ▼

1. A gas turbine engine comprising: a gearbox defined along an engine axis;a low spool arranged aft of the gearbox and operable to drive said gearbox:a front center body support defined around said engine axis;a front wall mounted to said front center body support, said front wall removable from sai

1. A gas turbine engine comprising: a gearbox defined along an engine axis;a low spool arranged aft of the gearbox and operable to drive said gearbox:a front center body support defined around said engine axis;a front wall mounted to said front center body support, said front wall removable from said front center body support to access said gearbox;a bearing package mounted to said front center body support and said low spool. 2. The gas turbine engine as recited in claim 1, wherein said front center body support is defined about an engine longitudinal axis. 3. The gas turbine engine as recited in claim 1, further comprising a seal package mounted to said front center body support. 4. The gas turbine engine as recited in claim 3, wherein the seal package is located aft of the bearing package. 5. The gas turbine engine as recited in claim 4, wherein the low spool includes a low pressure compressor hub providing a spline engagable with the bearing package, and the seal package mounted to the low pressure compressor hub. 6. The gas turbine engine as recited in claim 1, wherein said front center body support includes a flange which abuts a flange of said front wall. 7. The gas turbine engine as recited in claim 6, further comprising a multiple of fasteners which attach said flange of said front wall to said flange of said front center body support. 8. The gas turbine engine as recited in claim 7, wherein said multiple of fasteners are accessible from a forward side of the gas turbine engine. 9. The gas turbine engine as recited in claim 1, wherein said front wall supports a bearing structure to support an output shaft driven by said gearbox, and wherein said output shaft is operable to drive a fan. 10. The gas turbine engine as recited in claim 1, wherein said gearbox drives a fan section at a speed different than a speed of the low speed spool. 11. The gas turbine engine as recited in claim 1, wherein said front center body support provides a unitary component with a front center body section having a vane arranged in an annular core path and that at least partially defines a core flow path. 12. The gas turbine engine as recited in claim 11, wherein the front center body support and the front center body section are integral with one another. 13. The gas turbine engine as recited in claim 11, wherein the front center body support and the front center body section are welded to one another. 14. The gas turbine engine as recited in claim 1, wherein the bearing package includes a centering spring mounted to the front center body support and a coupling shaft section coupled to the low spool. 15. The gas turbine engine as recited in claim 14, comprising a coupling shaft interconnecting and splined to each of the gearbox and the coupling shaft section. 16. A method for servicing a gas turbine engine comprising: providing access from a forward side of a front center body assembly to a gearbox driven by a low spool;servicing a component located within a bearing compartment aft of the front center body assembly;disassembling a fan mounted to the gearbox, wherein the disassembling step includes removing a fan hub from an output shaft coupled to the gearbox;removing first a multiple of fasteners located within the forward side of the front center body assembly to disassemble a front wall from a front center body support of the front center body assembly, the fastener removing step performed subsequent to the fan hub removing step, wherein a flex support is secured to the gearbox and the front center body support, wherein the output shaft, the flex support and the gearbox comprise a gearbox module; andremoving a second multiple of fasteners interconnecting the flex support and the front center body support, and displacing the gearbox module away from the front center body support to remove the gearbox module as an assembly. 17. The method as recited in claim 16, comprising the step of removing a bearing package mounted to the front center body support and the low spool subsequent to removing the gearbox. 18. The method as recited in claim 17, wherein the gearbox includes the bearing package, and the displacing step includes displacing the bearing package out of engagement with a coupling shaft.