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REVERSE FLOW GAS TURBINE ENGINE WITH OFFSET RGB

  • US 20180073429A1
  • Filed: 01/17/2017
  • Published: 03/15/2018
  • Est. Priority Date: 09/15/2016
  • Status: Active Grant
First Claim
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1. A gas turbine engine comprising:

  • an engine case housing a low pressure compressor drivingly connected to a low pressure turbine by a low pressure compressor shaft extending along an engine axis, the low pressure turbine disposed forward of the low pressure compressor, a low pressure turbine shaft drivingly connected to the low pressure turbine and extending forward of the low pressure turbine, a reduction gear box (RGB) drivingly connected to the low pressure turbine shaft forward of the low pressure turbine, the RGB radially offset from the engine axis, and an access port defined in an axially forwardly facing surface of the engine case, the port disposed to provide access to the low pressure compressor shaft.

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