FIELD: aircraft engineering.
SUBSTANCE: proposed aircraft comprises fuselage with T-shape tail unit, hybrid power plant, smaller all-moving wing with hour engine nacelles, larger high wing with two hybrid nacelles arranged behind all-moving wing and three-leg wheeled retractable undercarriage. Hybrid power plant comprises lithium-ionic storage batteries, turboprops with push propellers and reversible motor-generators of hybrid engine nacelles and motors with pull propellers of the latter. Pull propellers are fitted on all-moving wing outer panels on both sides from high wing outer panel push propeller rotary axis.
EFFECT: higher operating efficiency.
4 cl, 1 tbl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| HYBRID SHORT TAKEOFF AND LANDING ELECTRIC AIRCRAFT | 2014 |
|
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| MULTIROTOR HYBRID ELECTRICAL CONVERTIPLANE | 2014 |
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|
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| CRYOGENIC TURBO-ELECTRIC STOL AIRCRAFT | 2013 |
|
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| HEAVY CONVERTIBLE ELECTRIC DRONE | 2013 |
|
RU2532672C1 |
