| 摘要 |
A turbofan jet engine includes an external casing, connected by radial arms to an annular internal device, downstream of which is mounted, opposite to the external casing, a shell forming a fairing, ancillaries on the outside of the external casing, and ancillaries on the inside of the shell. The turbofan jet engine further includes at least one monoblock arm for the connection of ancillaries between the outside of the external casing and the inside of the shell, placed parallel to a radial arm.
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