| 摘要 |
An assembly on an engine such as a turbofan engine comprises a first 64 and a second 46 piece mounted so as to rotate relative to one another. A connecting device between the pieces comprises a first annular part 78 defining a radial flange fixed to the first piece 64, a second annular part 80 extending axially, and bent studs 72 connecting the first and second annular parts together. The second annular part 80 is sectorized so that it is comprised of multiple sections 80. This minimises the transfer of loads when contact occurs during a fan blade break-off test. Electrical coils 70, 74 may inductively transfer electrical energy from the stationary beating support 64 to a shaft 46 to power a detonator in a blade-off test. |
