AIRCRAFT WING WITH ENGINE ATTACHMENT STRUT WITH LATERAL CHANNEL FOR FLOW ARRANGED IN ITS FRONT AREA Russian patent published in 2011 - IPC B64C7/02 

Abstract RU 2423289 C2

FIELD: transport.

SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft wing with engine attachment section, and to aircraft with such wing. Aircraft wing comprises tail section (2b) and root section (2a) with engine attachment strut (4) arranged under wing. Note here that attachment strut front area (8) extends ahead relative to wing front edge 10. There is lateral ledge (12) arranged in front area (8) of attachment strut (4) to extend toward root section (2a) and confine airflow lateral channel (14). Ledge rear end (12a) stays in contact with wing front edge while magnitude (Ls) of said lateral ledge (12) in direction toward with root section (2a) increases as it moves from front end (12b) to rear end (12a).

EFFECT: improved aircraft aerodynamics.

7 cl, 8 dwg

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Authors

Danten Stefani

Fol' T'Erri

Zherar Ljudovik

Zhimene Filipp

Dates

2011-07-10Published

2007-03-28Filed