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Title:
METHOD AND APPARATUS FOR AIR FLOW CONTROL IN AIRCRAFT SIDEWALL VOLUME
Document Type and Number:
Japanese Patent JP2012126392
Kind Code:
A
Abstract:

To provide an aircraft configuration that improves air flow control in the aircraft sidewall volume.

An aircraft fuselage sidewall may include the aircraft sidewall volume and a flow controller. The aircraft sidewall volume may be delineated by an aircraft skin forming an outboard boundary of the aircraft sidewall volume, a passenger cabin sidewall forming an inboard boundary of the aircraft sidewall volume and fuselage frame structures forming axial boundaries of the aircraft sidewall volume. The flow controller may be positioned at a portion of the aircraft sidewall volume to selectably control air flow through the aircraft sidewall volume.


Inventors:
GRAY JOHN C
SEDGWICK LEIGH M
SATTERFIELD SCOTT M
BLAKE JOHN D
KUSUDA CHARLES E
Application Number:
JP2011273186A
Publication Date:
July 05, 2012
Filing Date:
December 14, 2011
Export Citation:
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Assignee:
BOEING CO
International Classes:
B64C1/40; B64D13/00
Domestic Patent References:
JP2010519119A2010-06-03
JP2010521362A2010-06-24
JPS5946435A1984-03-15
JPH08338541A1996-12-24
JPS6463666A1989-03-09
JPH10274161A1998-10-13
Foreign References:
US5897079A1999-04-27
US20090189018A12009-07-30
Attorney, Agent or Firm:
Sonoda Yoshitaka
Kobayashi Yoshinori