STAROVEROV' WING (VERSIONS) Russian patent published in 2013 - IPC B64C9/32 B64C3/38 B64C3/56 

Abstract RU 2480375 C1

FIELD: transport.

SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft hardware intended for improving landing capabilities. Aircraft wing consists of outer wings. Note here that outer wings or their part turn about axis located in plan between perpendicular to aircraft axis and outer wing axis. Outer wing may turn relative to line making in plan with aircraft lengthwise axis the angle exceeding its sweep angle.

EFFECT: short landing run, efficient braking by wheels.

4 cl, 2 dwg

Similar patents RU2480375C1

Title Year Author Number
STAROVEROV'S SPACECRAFT (VERSIONS) AND/OR ALGORITHMS OF ITS OPERATION 2012
  • Staroverov Nikolaj Evgen'Evich
RU2503592C1
AIRCRAFT FOR LANDING AT CROSS WIND (VERSIONS) 2008
  • Staroverov Nikolaj Evgen'Evich
RU2400398C2
BICYCLE LANDING GEAR 2012
  • Staroverov Nikolaj Evgen'Evich
RU2494011C1
HYDROPLANE (VERSIONS) 2013
  • Staroverov Nikolaj Evgen'Evich
RU2513345C1
CANARD CONTROL (VERSIONS) 2007
  • Staroverov Nikolaj Evgen'Evich
RU2410286C2
COUNTERAIR MISSILE 2009
  • Staroverov Nikolaj Evgen'Evich
RU2439476C2
RESCUE SYSTEM OF AIRPLANE (VERSIONS) 2006
  • Staroverov Nikolaj Evgen'Evich
RU2336203C2
METHOD FOR IMPROVING BRAKING EFFICIENCY OF AIRCRAFT DURING GROUND ROLLING AND INCREASING SAFETY AT TAKEOFF AND LANDING, AND DEVICE FOR ITS IMPLEMENTATION 2011
  • Staroverov Nikolaj Evgen'Evich
RU2484279C1
PILOTLESS COMBAT AIRCRAFT /VERSIONS/ 2016
  • Staroverov Nikolaj Evgenevich
RU2622327C1
SPACE ROCKET AND METHOD OF ITS LANDING (VERSIONS) 2014
  • Staroverov Nikolaj Evgen'Evich
RU2568630C1

RU 2 480 375 C1

Authors

Staroverov Nikolaj Evgen'Evich

Dates

2013-04-27Published

2011-12-19Filed