Invention Grant
US08943793B2 Rear section of aircraft nacelle and nacelle equipped with such rear section 有权
飞机机舱和机舱的后部配备有这样的后部

Rear section of aircraft nacelle and nacelle equipped with such rear section
Abstract:
The invention relates to a rear section (11) of an aircraft nacelle, that comprises two halves (13a, 13b) defining: a central portion (C) for receiving a turbojet engine (7), a cool-air annular passage (31) provided around said central portion (C), and at least one six-hour cavity (15) provided under said central portion (C). The rear section is characterized in that it comprises at least one duct (29a, 29b) for the fluidic communication between said annular passage (31) and said six-hour cavity (15) for maintaining the temperature inside the six-hour cavity (15) within a relatively low range.
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