Device for attaching hammer clamp blades, associated compressor hub, compressor and turbine engine
View Patent ↗A locking device for enabling the circular locking of a set of blades provided with a hammer base on the rim of a turbine engine compressor hub is disclosed. The rim includes a peripheral groove on the outer surface thereof for receiving the bases of the blades of the set and two shoulders framing the groove with surfaces which form bearings for holding the blades; and a cut-out provided in at least one of the shoulders to enable the bases of the blades to be inserted in the groove. The locking device translatably immobilizes the blades in the groove and is positioned in the groove between two consecutive blades and in turn translatably held in the groove by an attachment device. A carrier is shaped so as to fit into the cut-out and to rest circumferentially on at least one engagement surface of the shoulder.
1. A locking device designed to permit locking, in a circular fashion, of a set of blades provided with a hammer-type root, on a rim of a turbine engine compressor hub, said rim comprising a peripheral groove on an outer face thereof designed to receive the roots of the blades of said set and two shoulders surrounding said groove of which faces form bearing surfaces for holding said blades, said rim further comprising a cutout formed in at least one of said shoulders to enable the roots of the blades to be inserted in said groove, said device comprising:
a lock which immobilizes the blades in translation in said groove, said lock being positioned in said groove between first and second consecutive blades and being held in translation in said groove;
a support; and
a fixing device,
wherein said lock includes an upper block with a first planar face abutting said root of said first blade and a second planar face abutting said root of said second blade, and a base which supports the upper block, said base extended by segments with an upper surface which is planar and a lower surface with a shape corresponding to a shape of a base of said peripheral groove,
wherein said support includes first and second planar faces which are parallel to and abut first and second faces of said cutout and a shape of said support corresponds to a shape of said cutout, and
wherein a thickness of said segments is less than a radial clearance between said root of said blades and said base of said peripheral groove.
2. The locking device as claimed in claim 1 , wherein said lock is shaped so as not to interfere with the blades during installation in the groove, so that the set of blades may be made up of identical blades.
3. The locking device as claimed in claim 1 , wherein the support is shaped to be inserted into the cutout in a direction substantially parallel to an axis of the turbine engine.
4. The locking device as claimed in claim 1 , wherein the shape of the support is entirely the shape of the cutout formed in the open shoulder.
5. The locking device as claimed in claim 1 , wherein the upper block has substantially the shape of a parallelepiped, said first and second planar faces being oriented parallel with an axis of the turbine engine.
6. The locking device as claimed in claim 1 , wherein said segments extend tangentially to the groove on both sides of a lower part of the upper block.
7. The locking device as claimed in claim 1 , wherein the upper block comprises a first drilled hole and wherein the support comprises a second drilled hole, axes of the two drilled holes being oriented so as to be aligned when the locking device is in position on the hub.
8. The locking device as claimed in claim 7 , wherein the fixing device is a bolt passing through the two drilled holes and wherein the support has a bearing face perpendicular to the axis of said bolt.
9. A compressor hub for a turbine engine, designed to carry a set of blades provided with a hammer-type root, the rim of said hub comprising a peripheral groove on the outer face thereof designed to receive the roots of the blades of said set and two shoulders surrounding said groove of which the faces form bearing surfaces for holding said blades, said rim further comprising a cutout formed in at least one of said shoulders to enable the roots of the blades to be inserted in said groove,
wherein said cutout is shaped to receive the support for holding the lock of a locking device as claimed in claim 1 and said shoulder comprises a cooperating surface for the circumferential bearing of said support.
10. The compressor of a turbine engine comprising at least one hub as claimed in claim 9 .
11. A compressor of a turbine engine comprising a set of blades provided with a hammer-type root and a locking device for the blades as claimed in claim 1 .
12. A turbine engine comprising a compressor as claimed in claim 11 .
13. The locking device as claimed in claim 1 , wherein an overall length of said lock is less than an overall length of platforms of said first and second blades.