Turbofan engine comprising a fairing being located in the secondary flow channel and having a separate end element
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United States of America Patent
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Jun 2, 2020
Grant Date -
Feb 15, 2018
app pub date -
Aug 9, 2017
filing date -
Aug 11, 2016
priority date (Note) -
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Abstract
A turbofan engine including a core engine and at least one fan by means of which fluid is guided to a primary flow channel for the core engine as well as to a secondary flow channel of the turbofan engine, wherein the secondary flow channel is provided for an outer fluid flow that is guided past the core engine, and at least one splitter fairing arranged inside the secondary flow channel around which the fluid flow is flowing during operation of the turbofan engine, which cases at least one component of the turbofan engine that is guided radially through the secondary flow channel, and which has an end element with a leading edge section that is facing towards the fluid flow and/or a trailing edge section that is positioned in the flow direction of the fluid flow.
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