PRODUCTION OF WING FOR AIRCRAFT WITH FUSELAGE BY CONFIGURING WING FOR EXTENSIVE LAMINAR AIRFLOW AND AIRCRAFT (VERSIONS) Russian patent published in 2014 - IPC B64C3/14

Abstract RU 2531536 C2

FIELD: transport.

SUBSTANCE: aircraft has fuselage and swept wing configured for laminar airflow at cruising flight, convex-concave airfoils that feature definite magnitudes of depth, chord and shape along wing span. Wong leading edges are configured to influence the laminar air flow. Maximum depth-to-chord ratio along wing span is related to Mach number of cruising flight. Every version of aircraft is characterised by a definite wing profile selection.

EFFECT: optimised airflow.

24 cl, 10 dwg

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RU 2 531 536 C2

Authors

Trejsi Richard R.

Sturdza Peter

Chehjz Dzhejms D.

Dates

2014-10-20—Published

2010-10-15—Filed