Turbine engine wheel, in particular for a low pressure turbine
View Patent ↗A turbine engine wheel, in particular for a low pressure turbine, is provided. The wheel includes blades, each including an airfoil connected by a platform to a middle wall or tang extending radially and itself extended radially inwards by a root mounted in a slot of a disk, the platform and the tang defining two side cavities arranged on either side of the tang, which cavities are circumferentially open and are situated facing corresponding cavities in the directly adjacent blades, and sealing members being housed in the cavities adjacent to the blades. An annular sealing end plate is mounted on the upstream or downstream end of the disk, between the platforms and the disk, so as to face the slots and the roots of the blades, and includes a rotary coupling device for coupling with at least one of the sealing members.
1. A turbine engine wheel comprising:
blades, each comprising an airfoil connected by a platform to a middle wall or tang extending radially and the tang extended radially inwards by a root mounted in a slot of a disk, the platform and the tang defining two side cavities arranged on either side of the tang, wherein said cavities are circumferentially open and are situated facing corresponding cavities in directly adjacent blades;
a sealing member being housed in one of the side cavities adjacent to the blades; and
an annular sealing end plate mounted on an upstream or downstream end of the disk, said sealing end plate extending radially between the platforms and the disk, so as to face the slots and the roots of the blades, said sealing end plate including rotary coupling means for coupling with the sealing member,
wherein one of the sealing end plate and the sealing member includes a projecting portion and the other of the sealing end plate and the sealing member includes a housing of complementary shape to the projecting portion, the projecting portion being engaged in the housing.
2. A turbine engine wheel according to claim 1 , wherein the projecting portion is a peg.
3. A turbine engine wheel according to claim 1 , wherein a radially inner periphery of the sealing end plate is fastened to the upstream or downstream end of the disk by a twist-lock type coupling.
4. A turbine engine wheel according to claim 1 , wherein the sealing end plate includes an annular lip extending axially upstream.
5. A turbine engine wheel according to claim 1 , wherein the blade is made entirely out of a ceramic matrix composite material.
6. A turbine engine wheel according to claim 1 , wherein the sealing member is made of metal and is hollow or solid.
7. A turbine engine wheel according to claim 1 , wherein a radially outer portion of the sealing end plate bears axially against the sealing member and is spaced apart from the roots and the platforms of the blades.
8. A turbine engine wheel according to claim 1 , wherein the sealing end plate includes a seal arranged between the sealing end plate and the disk, radially outside bottoms of the slots for mounting the roots of the blades.
9. A turbine engine wheel according to claim 1 , further comprising two annular sealing end plates respectively mounted on the upstream end and the downstream end of the disk, each end plate extending radially between the platforms of the blades and the disk, so as to face the slots and the roots of the blades, at least one of the sealing end plates including the rotary coupling means for coupling with the sealing member.