FIELD: aircraft engineering.
SUBSTANCE: jet engine comprises air intake cowling including two separate, in fact, tubular sections. Sections include first air intake section displacing forward and section secured to engine structure. Clearance is arranged between said first and second sections. Note here that said clearance allows bypassing when sections are located in immediate proximity and low-speed additional air function when sections are separated by a wider clearance.
EFFECT: improved air pressure conditions.
15 cl, 18 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SUPERSONIC AIRCRAFT JET ENGINE | 2007 |
|
RU2454354C2 |
| ASYMMETRICAL AIR-SCOOP FOR THREE FLOW ENGINE OF FASTER-THAN-SOUND AIRCRAFT | 2018 |
|
RU2670664C9 |
| METHOD OF CHANGE OF AERODYNAMIC CHARACTERISTICS OF SUBSONIC FLYING VEHICLE AND DEVICE FOR REALIZATION OF THIS METHOD | 2004 |
|
RU2282563C2 |
| SUPERSONIC AIRCRAFT WITH CLOSED STRUCTURE WINGS | 2015 |
|
RU2591102C1 |
| SUPERSONIC CONVERTIBLE AIRPLANE WITH X-SHAPED WING | 2016 |
|
RU2632782C1 |
| METHOD TO VARY HYPERSONIC AIRCRAFT AERODYNAMIC CHARACTERISTICS AND DEVICE TO THIS END | 2008 |
|
RU2383469C1 |
| SUPERSONIC CONVERTIBLE AIRCRAFT | 2015 |
|
RU2605587C1 |
| AIR INTAKE OF INTERNAL COMPRESSION SUPERSONIC ENGINE | 1997 |
|
RU2182670C2 |
| SUPERSONIC CONVERTIPLANE WITH X-SHAPED WING | 2015 |
|
RU2621762C1 |
| VARIABLE GEOMETRY AIR INTAKE FOR SUPERSONIC PASSENGER AIRCRAFT | 2021 |
|
RU2766238C1 |
