VARIABLE-GEOMETRY WING Russian patent published in 2008 - IPC B64C3/46 

Abstract RU 2330790 C2

FIELD: transportation.

SUBSTANCE: wing incorporates a thrust surface, a controlled fairing with the front and rear edges hinged, by its front edge, to the wing thrust surface to form with the said surface a pneumatic chamber designed to up rise the fairing by compressed gas and to move it back into initial position. The wing incorporates a patch. The fairing rear edge is arranged in the gap between the wing thrust surface and the said patch. The fairing is made from an elastic material.

EFFECT: simpler design.

2 dwg

Similar patents RU2330790C2

Title Year Author Number
VARIABLE-CHORD WING 2010
  • Zhitnikov Ehduard Dmitrievich
RU2429988C1
CONTROLLED-LIFT WING 2007
  • Zhitnikov Ehduard Dmitrievich
RU2380278C2
TRIPLE-WING AIRCRAFT 2006
  • Zhitnikov Ehduard Dmitrievich
RU2319642C2
ELASTIC PNEUMATIC CYLINDER 2006
  • Zhitnikov Ehduard Dmitrievich
RU2319043C2
BEARING UNIT OF AIRCRAFT 2007
  • Zhitnikov Ehduard Dmitrievich
RU2354581C1
MINIATURE AIRPLANE 2006
  • Zhitnikov Ehduard Dmitrievich
RU2327605C1
PNEUMATIC BEAM 2007
  • Zhitnikov Ehduard Dmitrievich
RU2352736C1
SLOT-HOLE WING 2007
  • Zhitnikov Ehduard Dmitrievich
RU2356797C1
AIRCRAFT WITH TWO-POSITION FLAPS 2010
  • Zhitnikov Ehduard Dmitrievich
RU2429989C1
SMALL TWO-DECK AIRCRAFT CARRIER 2009
  • Zhitnikov Ehduard Dmitrievich
RU2390462C1

RU 2 330 790 C2

Authors

Zhitnikov Ehduard Dmitrievich

Dates

2008-08-10Published

2006-05-19Filed