Inter-turbine casing with cooling circuit, and turbofan comprising it
View Patent ↗An inter-turbine casing for a turbofan is disclosed. The casing includes an outer ring, an inner ring, and an intermediate ring between the inner ring and the outer ring. The inner and intermediate rings have respective openings for the passage of cooling air. The casing includes at least one sealing device, arranged between the outer ring and the intermediate ring, with a base, provided with at least one orifice for the passage of cooling air, and a peripheral skirt which is able to be compressed and expanded elastically. The base bears against the outer ring and the peripheral skirt bears against the intermediate ring.
1. An inter-turbine casing for a turbofan, comprising:
an outer ring;
an inner ring; and
an intermediate ring between the inner ring and the outer ring, the inner and intermediate rings having respective openings for the passage of cooling air,
wherein the casing comprises at least one sealing device, arranged between the outer ring and the intermediate ring, with a base, provided with at least one orifice for the passage of cooling air, and a peripheral skirt which is able to be compressed and expanded elastically, the base bearing against the outer ring and the peripheral skirt bearing against the intermediate ring.
2. The inter-turbine casing as claimed in claim 1 , wherein the peripheral skirt extends from said base in a substantially perpendicular direction to a plane of said base.
3. The inter-turbine casing as claimed in claim 1 , wherein the peripheral skirt has a free edge which is curved inwardly so as to form a bearing face.
4. The inter-turbine casing as claimed in claim 1 , wherein the sealing device comprises a fastening device, arranged on the base, with holes passing through said base and accommodating fastening bolts.
5. The inter-turbine casing as claimed in claim 1 , further comprising structural radial arms which pass through said respective openings in the inner ring and intermediate ring, wherein said sealing device is installed between one end of one of the structural radial arms and said outer ring.
6. The inter-turbine casing as claimed in claim 5 , wherein said sealing device is installed such that at least one orifice in the base is situated opposite an opening in the outer ring.
7. The inter-turbine casing as claimed in claim 1 , wherein the sealing device is installed such that the peripheral skirt surrounds an opening in said intermediate ring.
8. The inter-turbine casing as claimed in claim 1 , wherein the sealing device is installed such that the peripheral skirt is prestressed in compression.
9. The inter-turbine casing as claimed in claim 5 , wherein the sealing device is fastened to an end plate of one of the structural arms by bolts passing through fastening holes formed in the base.
10. The inter-turbine casing as claimed in claim 1 , further comprising sleeves arranged between the intermediate ring and the inner ring, each of said sleeves bringing one of the respective openings in the intermediate ring into communication with one of the respective openings in the inner ring.
11. The inter-turbine casing as claimed in claim 10 , wherein said sleeves are provided with lateral perforations for the passage of cooling air.
12. A turbofan comprising at least one inter turbine casing comprising:
an outer ring;
an inner ring; and
an intermediate ring between the inner ring and the outer ring, the inner and intermediate rings having respective openings for the passage of cooling air,
wherein the casing comprises at least one sealing device, arranged between the outer ring and the intermediate ring, with a base, provided with at least one orifice for the passage of cooling air, and a peripheral skirt which is able to be compressed and expanded elastically, the base bearing against the outer ring and the peripheral skirt bearing against the intermediate ring.