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Thrust mounting arrangement

  • US 20090309005A1
  • Filed: 06/05/2009
  • Published: 12/17/2009
  • Est. Priority Date: 06/13/2008
  • Status: Active Grant
First Claim
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1. A mounting arrangement for mounting a gas turbine engine to a pylon of an aircraft, the gas turbine has a rotational axis the mounting arrangement comprisesa mounting block,two thrust struts andtwo cranks each pivotably attached to one of the thrust struts and pivotably attached the mounting block, wherein a gap is provided between the two cranks and the mounting block.

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