Turbomachine rotary fan blade, fan, and turbomachine provided therewith
AssigneeSafran Aircraft Engines
InventorsGuillaume Pascal Jean-Charles Gondre, Thomas Alain De Gaillard, Pierre Jean Faivre D'Arcier
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AssigneeSafran Aircraft Engines
InventorsGuillaume Pascal Jean-Charles Gondre, Thomas Alain De Gaillard, Pierre Jean Faivre D'Arcier
Estimating the term…
The invention relates to a turbomachine rotary-fan blade having a predetermined breaking zone, which extends from the upstream edge along a given length and from the blade-tip edge over a given height. According to the invention, the body is made of a composite material comprising a fibre reinforcement obtained by three-dimensional weaving of warp and weft strands, and a resin matrix in which the fibre reinforcement is embedded, and has, in or in the vicinity of the zone, a discontinuity of at least some of the strands, configured such that the zone partially detaches when there is tangential friction in the thickness direction against the blade-tip edge, the height being less than 3% of the aerodynamic stream height of the blade.
A blade for a turbomachine rotary fan, the blade comprising a body having an upstream edge and a downstream edge, between which the body, extends along a first longitudinal direction, an extrados and an intrados, between which the body extends along a second thickness direction, which is transverse to the first direction, a blade root and an upper blade tip edge, between which the body extends along a third height direction, transverse to the first longitudinal direction and to the second thickness directions, a function of the blade root being to be fixed to a longitudinal rotary fan hub,
A blade for a turbomachine rotary fan, the blade comprising a body having an upstream edge and a downstream edge, between which the body extends along a first longitudinal direction, an extrados and an intrados, between which the body extends along a second thickness direction, which is transverse to the first direction, a blade root and an upper blade tip edge, between which the body extends along a third height direction, transverse to the first longitudinal direction and to the second thickness directions, a function of the blade root being to be fixed to a longitudinal rotary fan hub,
A blade for a turbomachine rotary fan, the blade comprising a body having an upstream edge and a downstream edge, between which the body extends along a first longitudinal direction, an extrados and an intrados, between which the body extends along a second thickness direction, which is transverse to the first direction, a blade root and an upper blade tip edge, between which the body extends along a third height direction, transverse to the first longitudinal direction and to the second thickness directions, a function of the blade root being to be fixed to a longitudinal rotary fan hub,
Dependencies are inferred from the claim text.