FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering. Outlet system (1) can be arranged in an aircraft comprising airframe (2) and at least one wing (3) extending outwardly from airframe (2) which comes into contact with the air to provide a lift to airframe (2). Outlet system (1) comprises fluid discharge opening, first cover (4) shaped to skirt surrounding wing (3). One end of first cover (4) is connected to airframe (2), and its other end extends outward from airframe (2) so that there is distance with wing (3). Between first cover (4) and wing (3) there is hole (A) for directing fluid medium (F) on wing (3) between wing (3) and airframe (2). On airframe (2) there is outlet line (5) facing hole (A) and allowing to remove fluid medium (F) directed through hole (A) from wing (3).
EFFECT: protection against precipitation – rain or ice.
12 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ICING CONDITION DETECTING SYSTEM | 2013 |
|
RU2638064C2 |
| FRONT PART OF DIVIDER CONTAINING PLATE, MAKING SURFACE TO GUIDE CIRCUIT AND ACTING AS ANTI-ICING CHANNEL | 2014 |
|
RU2575676C2 |
| DEVICE FOR COMBATING CRYSTAL ICING OF TURBOFAN ENGINES (TDCE) | 2023 |
|
RU2814576C1 |
| BLEED AIR PRESSURE CONTROL SYSTEM FOR AIRCRAFT ANTI-ICING SYSTEM, AIRCRAFT ENGINE NACELLE ANTI-ICING SYSTEM AND AIR BLEED CONTROL METHOD IN ANTI-ICING SYSTEM | 2015 |
|
RU2714330C2 |
| IMPROVED DESIGN OF THE INPUT DEVICE | 2018 |
|
RU2727820C2 |
| AIRCRAFT DE-ICING SYSTEM AND AIRCRAFT WITH SUCH SYSTEM | 2011 |
|
RU2529927C1 |
| SPECIAL AIR INTAKE DEVICE WITH ANTI-ICING SYSTEM | 2023 |
|
RU2825936C1 |
| INTERNAL COMBUSTION ENGINE OIL TANK | 2008 |
|
RU2461725C1 |
| STREAMLINED BODY, PRIMARILY FOR AIRCRAFT | 2010 |
|
RU2496680C1 |
| METHOD OF DETECTING LEAKAGE OF FLUID MEDIUM IN TURBOMACHINE AND FLUID MEDIUM DISTRIBUTION SYSTEM | 2015 |
|
RU2693147C2 |
