AIRPLANE Russian patent published in 1994 - IPC

Abstract RU 2010744 C1

FIELD: aviation technology. SUBSTANCE: in any of its longitudinal sections airframe of airplane is in the form of cubic parabola with blunted tail part and with leading edge sweep angle of not less than 60 deg. Elevator is in the form of hinged forward portion of the airframe. EFFECT: improved flight performance parameters.

Similar patents RU2010744C1

Title Year Author Number
AIRCRAFT PROPULSOR 1996
  • Duchenko Aleksandr Lazarevich
RU2094326C1
AIRCRAFT 1998
  • Duchenko A.L.
RU2134649C1
SUPERSONIC MANEUVERABLE AIRCRAFT 2000
  • Kuznetsov A.I.
RU2180309C2
HELICOPTER 1993
  • Duchenko Aleksandr Lazarevich
RU2089455C1
SUPERSONIC LOW-NOISE AIRCRAFT WITH TANDEM WINGS 2015
  • Durov Dmitrij Sergeevich
RU2605585C1
SUPERSONIC AIRCRAFT WITH CLOSED STRUCTURE WINGS 2015
  • Durov Dmitrij Sergeevich
RU2591102C1
SUPERSONIC CONVERTIBLE AIRCRAFT 2009
  • Durov Dmitrij Sergeevich
RU2432299C2
PROPULSOR 1997
  • Duchenko Nikolaj Aleksandrovich
RU2120396C1
SUPERSONIC CONVERTIBLE AIRCRAFT 2015
  • Durov Dmitrij Sergeevich
RU2605587C1
SUPERSONIC CONVERTIBLE AIRPLANE WITH X-SHAPED WING 2016
  • Durov Dmitrij Sergeevich
RU2632782C1

RU 2 010 744 C1

Authors

Duchenko Aleksandr Lazarevich

Dates

1994-04-15Published

1990-04-04Filed