Internal turbomachine casing having improved thermal insulation
AssigneeSafran Aircraft Engines
InventorChristophe SCHOLTES
Life of this patent
Estimating the term…
Loading patent…
AssigneeSafran Aircraft Engines
InventorChristophe SCHOLTES
Estimating the term…
An internal casing ferrule for a turbomachine, centered on a longitudinal central axis, which includes: a main body centered on this axis, with two ends, delimited by surfaces that are radially inner and outer relative to this axis; a thermal porous-structure insulation envelope having a volumetric porosity ≥50%, which includes: a lateral portion entirely covering the two ends; when viewed in section transversely to this axis, exterior and interior portions entirely covering, respectively, the radially outer and inner surfaces of the main body; and a protective envelope which at least partially covers the envelope and which includes, when viewed in section transversely to this axis, radially outer and inner protective portions, respectively covering, at least in part, the exterior and interior portions.
1-13. (canceled)
Internal casing ferrule for a turbomachine, the ferrule being centred on a longitudinal central axis, wherein the internal casing ferrule includes:
Dependencies are inferred from the claim text.