FIELD: aviation.
SUBSTANCE: supersonic aircraft comprises a fuselage, a wing, an air intaker, a vertical tail and ailerons. Wingtip are formed fissile consisting of two halves: a fixed bottom part forming a single profile with the wing, and the movable bottom part with the possibility to deviate downwards for 90 degrees.
EFFECT: increased flight range.
6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SUPERSONIC AIRCRAFT WITH VARIABLE DURING THE FLIGHT WING CURVATURE | 2016 |
|
RU2623489C1 |
| SUPERSONIC AIRCRAFT | 2015 |
|
RU2613747C2 |
| HYPERSONIC AIRCRAFT | 2012 |
|
RU2509035C1 |
| EXECUTIVE SUPERSONIC AIRCRAFT | 2015 |
|
RU2602130C1 |
| TRANSPORT AIRCRAFT | 2011 |
|
RU2467924C1 |
| SUPERSONIC CONVERTIPLANE WITH X-SHAPED WING | 2015 |
|
RU2621762C1 |
| AIRCRAFT | 2012 |
|
RU2495796C1 |
| HIGH-CAPACITY AIRCRAFT | 2007 |
|
RU2335430C1 |
| SUPERSONIC LOW-VISIBILITY AIRCRAFT-HELICOPTER | 2018 |
|
RU2692742C1 |
| UNMANNED CONVERTIPLANE ROCKET CARRIER AND METHOD FOR USE THEREOF | 2018 |
|
RU2699514C1 |
