FIELD: devices for protection of flying vehicle movable surfaces against icing.
SUBSTANCE: proposed device is made in form of pipe line with inlet branch pipe (6) mounted on movable slat, outlet branch pipe (1) mounted on wing and elbow. Branch pipes and elbows are interconnected by means of bearing units. Bearing units include rotating bearings located in bodies; elbows are interconnected by means of bearing unit (5) provided with spherical bearing at slide fit over inner diameter; sealing rings of spherical bearing and packing washers of rotating bearing flanges are made from metal.
EFFECT: enhanced efficiency and reliability; reduction of labor input.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ANTI-ICE SYSTEM FOR AIRCRAFT WING SLATS | 2019 |
|
RU2742203C1 |
| SYSTEM FOR DISTRIBUTION AND DISCHARGE OF ANTI-ICING FLUID IN AIRCRAFT SKIN | 2023 |
|
RU2824828C1 |
| BEARING ASSEMBLY | 2010 |
|
RU2520706C2 |
| PIPE LINE ARTICULATED JOINT | 2003 |
|
RU2282094C2 |
| MAIN OIL ELECTRIC PUMP UNIT, AND METHOD FOR IMPROVEMENT OF UNIT CHARACTERISTICS | 2011 |
|
RU2484305C1 |
| AERODYNAMICALLY CONTROLLED APPARATUS FOR HIGH-SPEED DESCENDING FROM MOUNTAINS | 1999 |
|
RU2152885C1 |
| BELL-TYPE FURNACE CIRCULATION FAN | 0 |
|
SU1341229A1 |
| VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH ROTOR WITH FOLDING RETRACTABLE BLADES | 2019 |
|
RU2727787C1 |
| SLAT | 2009 |
|
RU2497717C2 |
| CENTRIFUGAL FILM-TYPE EVAPORATION APPARATUS | 0 |
|
SU816475A1 |
