×

GAS TURBINE ENGINE ARCHITECTURE WITH SPLIT COMPRESSOR SYSTEM

  • US 20180216525A1
  • Filed: 01/30/2017
  • Published: 08/02/2018
  • Est. Priority Date: 01/30/2017
  • Status: Abandoned Application
First Claim
Patent Images

1. A gas turbine engine comprising:

  • an engine core including a low pressure compressor, a high pressure compressor, a high pressure turbine and a low pressure turbine fluidly connected in series by an annular core gaspath concentric to an engine axis; and

    an external shaft disposed radially outwardly of an outer circumference of the core gaspath and drivingly connecting the low pressure turbine to the low pressure compressor.

View all claims
  • 1 Assignment
Timeline View
Assignment View
    ×
    ×