Method for manufacturing an air intake structure for a turbojet engine nacelle
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United States of America Patent
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Nov 1, 2016
Grant Date -
Nov 28, 2013
app pub date -
Aug 2, 2013
filing date -
Feb 4, 2011
priority date (Note) -
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Abstract
A method for manufacturing an air-intake structure for a turbojet-engine nacelle includes two component parts, i.e. one air-intake lip structure and one outer cowl for the air-intake structure. In particular, the method includes the following steps: separately manufacturing the component parts such that each integrates one overlapping portion with a part to which is to be attached. The overlapping portion is configured such that an outer surface of the outer overlapping portion provides continuity with an outer surface of the outer cowl associated with the inner overlapping portion. To secure the overlapping portions, glue or a fastener may be used.
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