AIRCRAFT WITH IMPROVED CENTRAL FAIRING Russian patent published in 2011 - IPC B64C23/06 B64C7/00 

Abstract RU 2424157 C2

FIELD: transport.

SUBSTANCE: invention relates to aircraft engineering. Aircraft 10 comprises fuselage 12, two wings 14, 16 whereto engine nacelles are attached, each being secured by central fairing 18, 20 to fuselage on its both sides. Said central fairing comprises two opposed surfaces jointed to wing upper and lower surfaces arranged along fuselage. One of said surfaces has local deformation of shape geometry to create aero dynamical lateral disturbances of airflow from central fairing to wing to control airflow over wing surface.

EFFECT: perfected aircraft design.

14 cl, 21 dwg

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RU 2 424 157 C2

Authors

Fol' T'Erri

Zhimene Filipp

Name Arno

Dates

2011-07-20Published

2006-11-06Filed