Turbine engine shaft coupling
US-9022684-B2 · May 5, 2015 · US
US9745865B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9745865-B2 |
| Application number | US-201414163390-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 24, 2014 |
| Priority date | Jan 25, 2013 |
| Publication date | Aug 29, 2017 |
| Grant date | Aug 29, 2017 |
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Official abstract text for this publication.
A device for axial locking of a moving part in rotation with respect to a reference part, includes a downstream locking wedge provided with lugs laid out such that the downstream locking wedge can be placed in: a first angular position in which the downstream locking wedge may be translated axially with respect to the moving part, a second angular position in which the lugs axially immobilize the downstream locking wedge with respect to the moving part; an upstream locking wedge able to prevent the rotation of the downstream locking wedge with respect to the moving part; and a stop segment able to immobilize axially the upstream locking wedge against the downstream locking wedge.
Opening claim text (preview).
The invention claimed is: 1. An axial locking device for axial locking of a moving part with respect to a reference part, an annular cavity being defined between the reference part and the moving part, the reference part extending along a reference axis, the reference part comprising a groove and a support shoulder extending transversally to the reference axis, the moving part comprising a transversal slot delimited by a downstream edge and an upstream edge, the upstream edge comprising circumferential openings, the axial locking device comprising: a downstream locking wedge constructed to be inserted into the annular cavity, the downstream locking wedge being provided with lugs laid out such that the downstream locking wedge can be placed in: a first angular position in which the downstream locking wedge may be translated axially through the circumferential openings of the upstream edge, and a second angular position in which the lugs immobilize axially the downstream locking wedge in the transversal slot axially resting against the downstream edge and the support shoulder; an upstream locking wedge constructed to be inserted into the annular cavity until it comes into axial abutment against the downstream locking wedge, the upstream locking wedge being laid out to prevent the rotation of the downstream locking wedge in the transversal slot when the upstream locking wedge is in axial abutment against the downstream locking wedge, a stop segment constructed to be inserted into the annular cavity and to be inserted into the groove so as to immobilize axially the upstream locking wedge against the downstream locking wedge. 2. The axial locking device according to claim 1 , wherein the downstream locking wedge has an annular body from which the lugs project radially. 3. The axial locking device according to claim 1 , wherein the upstream locking wedge comprises complementary lugs, each complementary lug being constructed to be inserted: into one of the circumferential openings of the upstream edge, and between two consecutive lugs of the downstream locking wedge so as to prevent angular movements of the downstream locking wedge in the transversal slot. 4. The axial locking device according to claim 1 , wherein the upstream locking wedge has an annular body from which the complementary lugs project radially. 5. The axial locking device according to claim 1 , wherein the stop segment has a diameter at rest, the stop segment being able to be deformed elastically to have a transition diameter less than the diameter at rest. 6. An assembly immobilized axially comprising: a reference part extending along a reference axis, the reference part comprising a groove and a support shoulder extending transversally with respect to the reference axis; a moving part comprising a transversal slot delimited by a downstream edge and an upstream edge, the upstream edge comprising circumferential openings; an annular cavity being formed between the reference part and the moving part; a downstream locking wedge constructed to be inserted into the annular cavity, the downstream locking wedge being provided with lugs laid out such that the downstream locking wedge can be placed in: a first angular position in which the downstream locking wedge may be translated axially through the circumferential openings of the upstream edge, and a second angular position in which the lugs immobilize axially the downstream locking wedge in the transversal slot while axially resting against the downstream edge and the support shoulder; an upstream locking wedge constructed to be inserted into the annular cavity until it comes into axial abutment against the downstream locking wedge, the upstream locking wedge being laid out to prevent the rotation of the downstream locking wedge in the transversal slot when the upstream locking wedge is in axial abutment against the downstream locking wedge; a stop segment constructed to be inserted into the annular cavity and to be inserted into the groove so as to immobilize axially the upstream locking wedge against the downstream locking wedge; wherein the moving part is immobilized axially with respect to the reference part such that the downstream edge of the moving part is aligned axially with the support shoulder of the reference part by the downstream locking wedge being inserted into the transversal slot of the moving part in the second angular position, such that the downstream locking wedge axially rests against the support shoulder and against the downstream edge, by the upstream locking wedge axially resting against the downstream locking wedge so as to prevent the rotation of the downstream locking wedge in the transversal slot, and by the stop segment being inserted into the groove of the reference part so as to be immobilized axially. 7. The assembly according to claim 6 , wherein the upstream locking wedge axially resting against the downstream locking wedge has a width along the reference axis equal to the distance along the reference axis between the groove and the support shoulder. 8. The assembly according to claim 7 , wherein the reference part is integral with a turbine shaft into which is inserted the moving part, the reference part comprising: a nut screwed onto the turbine shaft, the nut comprising legs extending along the reference axis, the groove being formed in the legs of the nut, an anti-rotation device laid out to prevent the rotation of the nut with respect to the turbine shaft, the anti-rotation device comprising a transversal shoulder. 9. The assembly according to claim 8 , wherein the moving part is formed by a connector integral with a measuring stick inserted into the turbine shaft. 10. A turbomachine comprising the assembly according to claim 6 .
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Arrangement of sensing elements · CPC title
Arrangements for testing or measuring (for measuring vibrations G01H) · CPC title
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