Fan disk for a jet engine and jet engine

The invention concerns a fan disk (10) for a jet engine (1) in which there flows a gas stream in a flow direction, characterised in that it has a pin-shaped radial section comprising: a first branch (12), designed to be fixed to a drive shaft (20) of the jet engine (1), a second branch (16), extendi...

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Bibliographic Details
Main Authors ACCARY ARNAUD, KIENER-CALVET BENJAMIN, BOIS STEPHANE, DEJAUNE CLAUDE, TAN-KIM ALEXANDRE, PETARD BENJAMIN, FOLL JULIEN
Format Patent
LanguageEnglish
Published 03.02.2016
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Summary:The invention concerns a fan disk (10) for a jet engine (1) in which there flows a gas stream in a flow direction, characterised in that it has a pin-shaped radial section comprising: a first branch (12), designed to be fixed to a drive shaft (20) of the jet engine (1), a second branch (16), extending opposite the first branch (12) and designed to support a plurality of fan blades (3a), and a curved junction wall (14) that extends between the first branch (12) and the second branch (16).
Bibliography:Application Number: CN201480032808