FIELD: aeronautical engineering; arrangement of main units of aircraft. SUBSTANCE: aircraft has wing 1 and tail unit 4 connected with fuselage 2. Mounted on wing 1 are two engines 5 with pusher propellers. Distance between longitudinal axes of propellers is equal to 1/7 to 1/6 of wing span. EFFECT: enhanced reliability. 2 dwg
Title | Year | Author | Number |
---|---|---|---|
AIRCRAFT | 1994 |
|
RU2107011C1 |
CARRIER PLANE | 2009 |
|
RU2402459C1 |
LIGHTWEIGHT AMPHIBIAN AIRCRAFT | 2006 |
|
RU2328413C1 |
MULTI-PURPOSE SUPER-HEAVY TRANSPORT TECHNOLOGICAL AIRCRAFT PLATFORM OF SHORT TAKE-OFF AND LANDING | 2019 |
|
RU2714176C1 |
VTOL AIRCRAFT | 2006 |
|
RU2350510C2 |
AIRCRAFT | 1995 |
|
RU2102279C1 |
FLYING VEHICLE (VARIANTS) | 2002 |
|
RU2212360C1 |
EXECUTIVE SUPERSONIC AIRCRAFT | 2015 |
|
RU2602130C1 |
AIRCRAFT | 2005 |
|
RU2308399C1 |
AMPHIBIOUS AEROPLANE | 1999 |
|
RU2151084C1 |
Authors
Dates
1996-09-20—Published
1992-12-30—Filed