FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft bearing elements. Aircraft comprises two fuselages with cryogenic fuel tanks. Wherein in one fuselage tank is located in fuselage nose section and in another fuselage — in fuselage tail section. Wing with takeoff and landing mechanization. Three engines located under the wing, one on the right and left wing panels, and the third one between two fuselages and made with possibility of using alternative fuel sources. T-shaped tail unit of closed type. Group of inventions also relates to wing with takeoff and landing mechanization for such aircraft.
EFFECT: development of aircraft, which provides improved basing conditions, transport logistic and fuel efficiency, as well as reduced emission of combustion products into atmosphere.
2 cl, 5 dwg
Title | Year | Author | Number |
---|---|---|---|
WING IN GROUND | 2019 |
|
RU2729114C1 |
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|
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AIRCRAFT | 2008 |
|
RU2466907C1 |
TRANSPORT PLANE | 2020 |
|
RU2758396C1 |
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|
RU2812162C1 |
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|
RU2728017C2 |
DRONE | 2023 |
|
RU2818209C1 |
AIRCRAFT WING | 2019 |
|
RU2717416C1 |
WING OF AIRCRAFT WITH RETRACTING AIR SCREW | 2016 |
|
RU2637277C1 |
LONG-HAUL AIRCRAFT | 2023 |
|
RU2813390C1 |
Authors
Dates
2024-03-11—Published
2023-09-11—Filed