FIELD: aviation.
SUBSTANCE: aft portion of the wide-body aircraft comprises a frame with covering, empennage with two tail fins and common wing, jet engine, mounted between the tail fins with protrusion over the frame covering and casing. Motor is mounted coaxially with the ejector with possibility of air bleeding from the top and from sides of the aft portion of the fuselage.
EFFECT: increasing the lifting force of the aft portion due to air bleeding out from the zone under the fuselage.
2 cl, 2 dwg
Title | Year | Author | Number |
---|---|---|---|
AIRBORNE VEHICLE | 2013 |
|
RU2536154C1 |
AIRBORNE VEHICLE | 2013 |
|
RU2533933C1 |
AIRCRAFT | 2013 |
|
RU2530354C1 |
AIRBORNE VEHICLE | 2013 |
|
RU2544036C1 |
AIRCRAFT TAIL | 2013 |
|
RU2539439C1 |
WIDE-BODY AIRCRAFT WING (VERSIONS) | 2014 |
|
RU2568627C1 |
AIRCRAFT FUSELAGE | 2013 |
|
RU2544055C1 |
AIRCRAFT | 2012 |
|
RU2503590C1 |
AIRCRAFT (VERSIONS) | 2011 |
|
RU2462392C1 |
AIRCRAFT WING | 2014 |
|
RU2554026C1 |
Authors
Dates
2015-03-27—Published
2013-12-12—Filed