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TURBINE ENGINE COMPRISING A CONTRAROTATING PROPELLER RECEIVER SUPPORTED BY A STRUCTURAL CASING ATTACHED TO THE INTERMEDIATE HOUSING

  • US 20130098066A1
  • Filed: 10/18/2012
  • Published: 04/25/2013
  • Est. Priority Date: 10/21/2011
  • Status: Active Grant
First Claim
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1. An aircraft turbine engine comprising:

  • a contrarotating propeller receiver and a dual-body gas generator comprising a low-pressure compressor and a high-pressure compressor separated by an intermediate housing, said gas generator being arranged upstream from said receiver,a structural casing for supporting the receiver, said casing surrounding the gas generator and having a downstream end attached to said receiver and an upstream end attached to said intermediate housing,connection means between said structural supporting casing and the gas generator, arranged between the upstream and downstream ends of the casing, wherein said connection means are designed to enable relative movement between said structural support casing and the gas generator.

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