FIELD: aviation.
SUBSTANCE: aircraft comprises fuselage with areas of structural interface for connection to one or multiple versions of vertical tail unit, horizontal tail unit and front empennage. Vertical tail empennage, horizontal tail unit and/or front horizontal empennage of different sizes, shapes, sweep angles, caisson chords and/or root chords can be attached to fuselage without changing structural design or configuration of areas of structural coupling with fuselage.
EFFECT: group of inventions is aimed at expansion of technical facilities array.
13 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SWEPT-FORWARD WING WITH SWIVEL PART OF OUTER WING PANELS | 2005 |
|
RU2296082C1 |
| ROTARY-WINGED AIRCRAFT WITH STABILIZER WING | 2020 |
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|
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| MULTI-PURPOSE SUPER-HEAVY TRANSPORT TECHNOLOGICAL AIRCRAFT PLATFORM OF SHORT TAKE-OFF AND LANDING | 2019 |
|
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| AIRCRAFT SIDE OF BODY JOINT | 2014 |
|
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| AERODYNAMIC SURFACE AND AIRFRAME OF AIRCRAFT | 2017 |
|
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| VERTICAL TAIL EMPENNAGE FOR FLOW CONTROL | 2018 |
|
RU2711821C1 |
| FRAMEWORK | 2016 |
|
RU2645522C1 |
| ROTARY-WINGED AIRCRAFT COMPRISING HORIZONTAL TAIL EMPENNAGE AND TWO KEELS ARRANGED ON HORIZONTAL TAIL EMPENNAGE | 2018 |
|
RU2706880C1 |
