FLYING VEHICLE FOLDING AIRFOIL (EMBODIMENTS) Russian patent published in 1994 - IPC

Abstract RU 2007334 C1

FIELD: aircraft engineering. SUBSTANCE: members 1, 2 may be made with thicknesses in necessary points considering stiffness or may have aerodynamic vanes oriented down the flow which are used as ribs. The inner cavity between members 1 and 2 is air-filled when the airfoil is in the working position. EFFECT: improved structure. 2 cl, 7 dwg

Similar patents RU2007334C1

Title Year Author Number
METHOD OF CONTROL OF DISTRIBUTION OF AERODYNAMIC LOADS ON FLYING VEHICLE WING AND VERSIONS OF FLYING VEHICLE WING 1988
  • Shirinjants V.A.
  • Karakeshishev V.A.
  • Zakharov V.A.
RU2026240C1
AIRCRAFT MANUAL CONTROL SYSTEM 1994
RU2089447C1
MANUAL CONTROL SYSTEM OF TRAINER AEROPLANE 1993
RU2093419C1
LANDING GEAR UP LOCAL 1992
  • Sokolov V.I.
RU2076827C1
LANDING GEAR FRONT LEG WHEEL TURN CONTROL SYSTEM 1992
  • Sokolov V.I.
RU2042575C1
AVIATION SYSTEM 1987
  • Valuev A.A.
RU2049701C1
METHOD FOR CHANGING FLOATABILITY OF AIRSHIP WITH PROPULSION HYDROCARBON-FUELLED ENGINES AND PROPELLERS AS PROPULSIVE DEVICE 1990
  • Tokarev M.V.
RU2017650C1
DEVICE FOR CONTROL OF FLYING VEHICLE POWER PLANT 1989
  • Grigor'Ev S.M.
  • Zagrebin A.N.
  • Novikov S.N.
  • Fedoseev V.N.
RU2046065C1
METHOD FOR RESTORATION OF OZONE LAYER OF ATMOSPHERE 1991
  • Novikov V.K.
  • Favorskij O.N.
  • Khabarov O.S.
  • Baryshov N.D.
  • Bruk A.A.
  • Nikitin A.T.
  • Amelin B.N.
RU2005347C1
COMPLEX NAVIGATIONAL SYSTEM 1992
  • Eremin A.V.
  • Kukolevskij O.I.
  • Budnik V.K.
  • Borisov I.V.
RU2077028C1

RU 2 007 334 C1

Authors

Sokolovskij V.M.

Dates

1994-02-15Published

1992-08-18Filed