A device for axial retention of mobile vanes mounted on a rotor disc includes two open rings, superimposed. At least one of the rings includes a rotating stop mechanism configured to cooperate with at least one hook of the disc. The two open rings are mounted in a discontinuous groove formed in the
A device for axial retention of mobile vanes mounted on a rotor disc includes two open rings, superimposed. At least one of the rings includes a rotating stop mechanism configured to cooperate with at least one hook of the disc. The two open rings are mounted in a discontinuous groove formed in the hooks, at the end of teeth situated on the periphery of the rotor disc, such that the rotating stop mechanism of the first ring is placed in the opening of the second ring. The significance of contact surfaces between the two rings allows a damping of vibrations during operation.
대표청구항▼
1. A device for axial retention of mobile vanes, configured to be inserted into a discontinuous groove of a turbomachine rotor disc, comprising: two rings, superimposed, each including an opening separating free ends of the ring,wherein at least the first ring includes a rotating stop means, provide
1. A device for axial retention of mobile vanes, configured to be inserted into a discontinuous groove of a turbomachine rotor disc, comprising: two rings, superimposed, each including an opening separating free ends of the ring,wherein at least the first ring includes a rotating stop means, provided to engage in the opening of the second ring such that the two rings form a double ring. 2. The device according to claim 1, wherein the two rings have a same width, same thickness, and identical outer diameter. 3. The device according to claim 1, wherein the rotating stop means protrudes outwardly, in a radial direction of the first ring. 4. The device according to claim 1, wherein the rotating stop means of the first ring includes a brace formed by a tab, bent, folded down and fixed on a face of the first ring. 5. The device according to claim 1, wherein the rotating stop means includes a brace machined in an oversize of the first ring. 6. The device according to claim 4, wherein the brace of the first ring includes an inter-tooth lug for stopping rotation, protruding radially toward the outside of the first ring. 7. The device according to claim 5, wherein the inter-tooth lug has a thickness equal to twice that of the rest of the ring. 8. The device according to claim 1, wherein the brace and the opening of the first ring are angularly spaced by an angle greater than 150°. 9. The device according to claim 1, wherein the second retaining ring also includes a rotating brace stop. 10. A turbomachine rotor comprising: at least one rotor disc whereof a body includes a plurality of slots and teeth including at least one hook, protruding in the axial direction of the disc, which defines, on that tooth, an elementary groove opening radially inwardly, a foot of a vane being inserted into the slot,wherein the foot is stopped in translation in the slot by at least one axial retaining device placed in a discontinuous groove, formed by a succession of elementary grooves, according to claim 1. 11. A turbomachine comprising a rotor as defined in claim 10.
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이 특허에 인용된 특허 (11)
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Agram Daniel A. (Melun FRX) Bodet Philippe (Villeneuve La Guyard FRX) Dhyser Franois G. (Le Mee Sur Seine FRX) Prigent Gerard D. (Paris FRX), System for balancing and damping a turbojet engine disk.
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