发明申请
US20050247042A1 Turbofan jet engine with ancillaries distribution support 有权
Turbofan喷气发动机配有辅助分配支持

Turbofan jet engine with ancillaries distribution support
摘要:
This invention concerns a turbofan jet engine comprising an outer casing supported by arms, an inner casing facing the casing and ancillaries. An ancillaries distribution support is formed along the axis of an arm, on the inner casing, comprising a first sole plate for reception of ancillaries on the outer side of the inner casing. The invention reduces the longitudinal dimension necessary for the ancillaries to pass through.
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