Turbine wheel with an axial retention system for vanes
View Patent ↗A turbine wheel includes: a plurality of blades, a rotor including a disk having the blades mounted at a periphery thereof, each blade including an airfoil with a foot secured to a platform carrying an attachment member engaged in a housing that opens into the periphery of the disk and that extends axially between two opposite side faces of the disk, the housings being spaced apart from one another by portions of the disk that form teeth, and an axial retention plate retaining the blades on the disk and including a retention plate situated on one side of the disk. On the other side of the disk, the teeth of the disk present portions in relief that project radially and that form abutments pressing axially against the portions in relief that are formed under the platforms of the blades and that are set back relative to side faces of the attachment members situated beside a second side face of the disk, and side faces of the attachment members of the blade and of the disk at its periphery are situated in substantially a same plane on each side of the disk.
1. A turbine wheel comprising:
a plurality of blades;
a rotor including a disk having opposite upstream and downstream side end faces at a periphery of the disk and including the blades mounted at the periphery of the disk, each blade including an airfoil with a foot secured to a platform carrying an attachment member having opposite upstream and downstream side end faces and engaged in a housing opening out into the periphery of the disk, the housings extending axially over an entire distance between the opposite upstream and downstream side end faces of the periphery of the disk and being separated from one another by portions of the disk that form teeth; and
axial retaining devices for retaining the blades on the disk, the blades being retained axially at a first one of the upstream and downstream side end faces of the disk by a retaining plate and being retained axially at a second other of the upstream and downstream side end faces of the disk by portions in relief formed under the platforms of the blades pressing axially against portions in relief formed on the teeth of the disk,
wherein an axial pressure is set back relative to the side faces of the attachment members situated on the second side end face of the disk,
wherein the upstream and downstream side end faces of the attachment members of the blades and of the disk at the periphery thereof are situated substantially in a same plane on each of the upstream and downstream side of the periphery of the disk, respectively, and
wherein the retaining plate comprises teeth exerting the axial pressure against the side end face of the attachment member without contacting the first side end face of the disk.
2. A turbine wheel according to claim 1 , wherein the axial pressure between the blades and the disk is provided and maintained without encroaching on the axial clearance between the rotor and an adjacent stator.
3. A turbine wheel according to claim 1 , wherein the retaining plate presents extra thickness at its periphery, thereby forming a cantilevered-out mass.
4. A turbine wheel according to claim 1 , wherein the retaining plate is mounted on the rotor by being prevented from moving axially by a retaining split ring.
5. A turbine wheel according to claim 4 , wherein at least one opening forming an inspection window is formed in the rotor to enable positioning of the retaining split ring to be inspected visually.
6. A turbine wheel according to claim 1 , wherein the retaining plate presses against the attachment members of the blades with prestress.
7. A turbine wheel according to claim 1 , wherein the retaining plate has a radial dimension that is limited so as to press only against the lower portions of the attachment members of the blades.
8. A turbomachine including a turbine wheel according to claim 1 .