FIELD: aviation.
SUBSTANCE: invention relates to the aviation equipment. Aircraft wing comprises lining, power kit, engine and propeller, latter are made as single monoblock with possibility of displacement and/or turn, wing contains compartment with length of 10–25 % of local chord for monoblock retraction at its displacement and/or turn. Compartment for harbor monoblock is located in lower part of wing. Compartment comprises a closing flap of curvilinear shape, similar to wing profiling.
EFFECT: invention is aimed at reduction of noise level and length of take-off distance, landing, reduction and climbing.
3 cl, 4 dwg
Title | Year | Author | Number |
---|---|---|---|
WING OF AIRCRAFT WITH RETRACTING AIR SCREW | 2016 |
|
RU2637277C1 |
AIRCRAFT WING | 2019 |
|
RU2717416C1 |
AIRCRAFT WITH A HYBRID POWER PLANT | 2022 |
|
RU2789425C1 |
SUBSONIC AIRLINER | 2012 |
|
RU2529309C2 |
MULTI-PURPOSE SUPER-HEAVY TRANSPORT TECHNOLOGICAL AIRCRAFT PLATFORM OF SHORT TAKE-OFF AND LANDING | 2019 |
|
RU2714176C1 |
ROTOR-CRAFT | 2016 |
|
RU2662339C2 |
DEVICE FOR IMPROVEMENT OF AIRCRAFT LIFTING PROPERTIES | 2014 |
|
RU2556745C1 |
MULTI-PURPOSE TWIN-ENGINED SEA-BASED AND LAND- BASED AIRCRAFT OF SHORT TAKEOFF AND LANDING | 2001 |
|
RU2196707C2 |
UNMANNED AERIAL VEHICLE OF VERTICAL TAKE-OFF AND LANDING | 2017 |
|
RU2716391C2 |
AIRCRAFT | 1992 |
|
RU2023628C1 |
Authors
Dates
2019-08-05—Published
2018-10-17—Filed