Method and apparatus for air flow control in an aircraft sidewall volume

An aircraft fuselage sidewall may include an aircraft sidewall volume (70) and a flow controller. The aircraft sidewall volume (70) may be delineated by an aircraft skin (50) forming an outboard boundary of the aircraft sidewall volume (70), a passenger cabin sidewall (60) forming an inboard boundar...

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Bibliographic Details
Main Authors Kusuda, Charles E, Gray, John C, Blake, John D, Sedgwick Leigh M, Satterfield, Scott M
Format Patent
LanguageEnglish
French
German
Published 14.08.2019
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Summary:An aircraft fuselage sidewall may include an aircraft sidewall volume (70) and a flow controller. The aircraft sidewall volume (70) may be delineated by an aircraft skin (50) forming an outboard boundary of the aircraft sidewall volume (70), a passenger cabin sidewall (60) forming an inboard boundary of the aircraft sidewall volume (70) and fuselage frame structures forming axial boundaries of the aircraft sidewall volume (70). The flow controller may be positioned at a portion of the aircraft sidewall volume (70) to selectably control air flow through the aircraft sidewall volume (70).
Bibliography:Application Number: EP20110193898