Unit for an aircraft thruster
A unit for an aircraft thruster is provided that includes a first ferrule configured to be attached to a second ferrule and a first connection flange configured to be secured to a second corresponding connection flange secured to the second ferrule. The connection flange includes a portion forming a plane extending along a radial direction with respect to the first ferrule. A link between the first ferrule and the corresponding connection flange is offset to a distance from said plane corresponding to a length for damping a shear-generating flexural moment, generated by fluxes of forces passing through the first ferrule.
1. A unit for an aircraft thruster comprising:
a first ferrule configured to be attached to a second ferrule at a junction plane wherein the first ferrule does not overlap the second ferrule; and
a first connection flange configured to be secured, at the junction plane, to a second corresponding connection flange secured to the second ferrule, said first connection flange comprising a first connection portion extending along a radial direction with respect to the first ferrule and a second tubular connection portion attached on the first ferrule,
wherein a vertical gap between the first ferrule and the second tubular connection portion of said first connection flange increases as the second tubular connection portion approaches the junction plane in order to dampen a shear-generating flexural moment, generated by fluxes of forces passing through the first ferrule.
2. The unit according to claim 1 , wherein the first ferrule is an internal ferrule of at least one of an air intake structure of a nacelle and/or of a structure of a reverser of the nacelle and/or of a fan case of a turbine engine.
3. The unit according to claim 1 , wherein the length l for damping said moment is defined in the following formula (1):
ℓ
=
R
×
e
3
×
(
1
-
v
2
)
1
4
(
1
)
wherein R and e respectively define a radius and thickness of the first ferrule, and v is the Poisson coefficient of a material forming the first ferrule at right angles to the junction plane.
4. The unit according to claim 1 , wherein the first ferrule and the first connection flange are made in one piece in a composite material.
5. The unit according to claim 1 , wherein the first connection flange is a metal material.
6. The unit according to claim 1 , wherein the first ferrule further comprises a transition corner configured to be set into place at right angles to the junction plane between the latter and the first ferrule.
7. The unit according to claim 1 , wherein the first ferrule further comprises a reinforcement plate added onto the first connection flange.
8. A method for manufacturing the unit according to claim 1 , comprising a step in which the vertical qap between the first ferrule and the second tubular connection portion of said first connection flange increases as the second tubular connection portion approaches the junction plane in order to dampen the shear-generating flexural moment, generated by fluxes of forces passing through the first ferrule.