FIELD: transport.
SUBSTANCE: invention relates to administrative supersonic airplanes. Aircraft contains wing coupled with fuselage nose and central parts of which are performed with rounded shape of cross-section, and rear part is provided with power plant with two air intakes and engine nacelle located behind recess which is limited by the first and the second pair of flats located in tandem. Flats of each of the pairs are turned relative to each other by obtuse angles the edges of which are passed near aircraft plane of symmetry.
EFFECT: lowering irregularity of supersonic flow supplied to air intakes.
5 cl, 10 dwg
Title | Year | Author | Number |
---|---|---|---|
AIRCRAFT | 2012 |
|
RU2517629C1 |
AIRCRAFT | 2012 |
|
RU2517627C1 |
SUPERSONIC AIRCRAFT | 2013 |
|
RU2548200C2 |
SUPERSONIC AIRCRAFT | 2020 |
|
RU2753443C1 |
TACTICAL AIRCRAFT WITH INCREASED AERODYNAMIC CHARACTERISTICS | 2022 |
|
RU2807556C1 |
FLIGHT VEHICLE (VERSIONS), FLIGHT VEHICLES PARTS, METHOD OF EXPLOITING FLIGHT VEHICLE AND ITS PARTS | 2010 |
|
RU2466061C2 |
SUPERSONIC AIRCRAFT | 2021 |
|
RU2776193C1 |
SUPERSONIC AIRCRAFT (VERSIONS) | 2007 |
|
RU2391254C2 |
MULTI-FUNCTIONAL TWO-SEAT STEALTH AIRCRAFT | 2023 |
|
RU2807624C1 |
AIRCRAFT (VERSIONS) | 2012 |
|
RU2486105C1 |
Authors
Dates
2014-06-27—Published
2012-11-20—Filed