MODULARITY OF AN AIRCRAFT TURBOMACHINE
An aircraft turbomachine, including a first shaft having external splines oriented parallel to an axis of rotation of the shaft, a second shaft having internal splines complementary to the external splines, this second shaft being fitted axially on the first shaft and these shafts rotating as one by...
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Main Authors | , |
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Format | Patent |
Language | English French German |
Published |
13.09.2023
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Subjects | |
Online Access | Get full text |
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Summary: | An aircraft turbomachine, including a first shaft having external splines oriented parallel to an axis of rotation of the shaft, a second shaft having internal splines complementary to the external splines, this second shaft being fitted axially on the first shaft and these shafts rotating as one by engagement of their splines, and a system for axially locking the shafts with respect to one another, wherein the system includes screws that are oriented radially with respect to the axis, each of these screws being screwed into a first orifice in one of the shafts and having a free end for engaging a second orifice in the other of the shafts. |
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Bibliography: | Application Number: EP20210811414 |