FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to flying-wing aircraft. Aircraft comprises at least one channel for draft flow extending through airframe from air intake at airframe surface via jet engine to jet nozzle at airframe surface. Said jet engine is located at least partially ahead of said air intake. Said air intake has curved sections to feed draft flows to engine.
EFFECT: better aircraft concealment.
11 cl, 10 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| CONVERTIBLE SUBSONIC AIRCRAFT | 2024 |
|
RU2839782C1 |
| AIRCRAFT WITH SHORT OR VERTICAL TAKE-OFF AND LANDING | 2019 |
|
RU2708120C1 |
| HIGHLY MANEUVERABLE AIRCRAFT | 2017 |
|
RU2682700C2 |
| VTOL AIRCRAFT | 2022 |
|
RU2788231C1 |
| SUPERSONIC AIRCRAFT JET ENGINE | 2007 |
|
RU2454354C2 |
| SUPERSONIC AIRCRAFT JET ENGINE | 2007 |
|
RU2499739C2 |
| AIRCRAFT WITH PERFECTED AERODYNAMIC CHARACTERISTICS | 2011 |
|
RU2575738C2 |
| AEROSPACE CRAFT WITH NUCLEAR PROPULSOR AND AEROSPACE FLIGHTS PERFORMED THEREBY | 2013 |
|
RU2574295C2 |
| MULTI-FUNCTIONAL TWO-SEAT STEALTH AIRCRAFT | 2023 |
|
RU2807624C1 |
| AIRCRAFT WITH SHORT OR VERTICAL TAKE-OFF AND LANDING WITH HYBRID POWER PLANT | 2019 |
|
RU2729750C1 |
