Circumferential blocking device of clamp vanes for turbine engine, with improved radial deployment
View Patent ↗The invention relates to a device ( 30 ) for blockage of vanes in a circumferential groove ( 10 ) of a turbine engine disc, the device being intended to deploy in a radial direction to be locked in the circumferential groove open radially. According to the invention, the blocking device comprises a first and a second piece ( 32, 34 ) designed to deploy in the radial direction by relative displacement of these pieces in the circumferential direction ( 23 ).
1. A blocking device for vanes in a circumferential groove of a turbine engine disc, said device being designed to deploy in a radial direction to be locked in said circumferential groove open radially,
wherein said blocking device comprises a first and second piece designed to deploy in the radial direction by relative displacement of said pieces in the circumferential direction.
2. The device as claimed in claim 1 , wherein at least one of said first and second pieces is equipped with a gripping member for being taken along relative to the other piece, according to the circumferential direction.
3. The device as claimed in claim 2 , wherein the gripping member is a tab or a cable.
4. The device as claimed in claim 2 or 3 , wherein the piece equipped with the gripping member has a stop in the circumferential direction.
5. The device as claimed in claim 1 , wherein at least one of said first and second pieces has a ramp for deployment of the device in the radial direction, during relative displacement of said pieces in the circumferential direction.
6. The device as claimed in claim 1 , further comprising locking means of for locking the two pieces in a position deployed radially.
7. A system comprising two pieces designed to enter respectively in two blocking devices as claimed in claim 2 , wherein said two pieces are joined together by said gripping member on either side of which they are located.
8. The device as claimed in claim 1 , wherein said blocking device is configured to pass from a retracted state to a deployed state as said first and second pieces follow said relative displacement in the circumferential direction, wherein a radial dimension of said blocking device increases as said blocking device passes from said retracted state to said deployed state.
9. A turbine engine wheel comprising a disc with a circumferential groove, vanes with bases retained radially by said groove, at least one blocking device designed to deploy in a radial direction to be locked in said circumferential groove open radially, wherein said blocking device comprises a first piece and a second piece designed to deploy in the radial direction by relative displacement of said pieces in the circumferential direction.
10. A turboengine comprising at least one wheel as claimed in claim 9 .
11. A process for installing a blocking device in a circumferential groove of a disc of a turbine engine, said blocking device comprising a first piece and a second piece, said method comprising:
placing said blocking device in the circumferential groove; and
deploying said blocking device in the radial direction to lock said blocking device in said circumferential groove, by relative displacement of said first and second pieces in the circumferential direction.