FIELD: aviation technique. SUBSTANCE: flat adjustable under-fuselage air intake of an aircraft has a subsonic part with a main braking wedge, having a changeable geometry, consisting of separate flat movable portions, movably connected one with another. A front end of the first portion of the braking wedge is connected with the fuselage with possibility of rotation by a joint assembly, it is not connected with the second portion of the wedge and it is mounted with possibility of touching a wall of the fuselage. The second and the third portions of the braking wedge are mounted with possibility of common (as monolithic assembly) rotation relative to a joint between the third and the fourth portions. EFFECT: simplified structure. 1 cl, 2 dwg
Title | Year | Author | Number |
---|---|---|---|
RAM-JET ENGINE | 1992 |
|
RU2040702C1 |
ASYMMETRICAL AIR-SCOOP FOR THREE FLOW ENGINE OF FASTER-THAN-SOUND AIRCRAFT | 2018 |
|
RU2670664C9 |
STEALTH AIR INTAKE OF SUPERSONIC AIRCRAFT | 2022 |
|
RU2801718C1 |
JET ENGINE AIR INTAKE | 2024 |
|
RU2823410C1 |
AIR INTAKE POWER UNIT DEVICE OF HYPERSONIC AIRCRAFT | 2012 |
|
RU2522661C1 |
CRUISING MISSILE IN TRANSPORTATION-LAUNCHING CONTAINER | 2001 |
|
RU2215981C2 |
AIRCRAFT (VERSIONS) | 2012 |
|
RU2486105C1 |
VARIABLE GEOMETRY AIR INTAKE FOR SUPERSONIC PASSENGER AIRCRAFT | 2021 |
|
RU2766238C1 |
SUPERSONIC MISSILE | 2017 |
|
RU2686567C2 |
AIR INTAKE WITH VARIABLE GEOMETRY FOR SUPERSONIC AIRCRAFT (VERSIONS) | 2007 |
|
RU2353550C1 |
Authors
Dates
1994-08-30—Published
1992-07-14—Filed