FIELD: anti-icing systems.
SUBSTANCE: invention relates to aircraft anti-icing systems, as well as to solar batteries. Anti-icing system comprises wires for connection with aircraft power supply system brought to inner surface of aircraft skin. Set of exposed conductors (1, 2) is arranged on the outer surface subject to icing and flush with it. At that, in the active zone next to each anode (1) there is cathode (2) and vice versa. Distance between anode (1) and cathode (2) should be such that short circuit does not occur in humid air.
EFFECT: reduced weight and power consumption.
1 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD FOR CHANGING CHARACTERISTICS OF AERODYNAMIC CONTROL ELEMENT OF UNMANNED AERIAL VEHICLE | 2022 |
|
RU2819376C1 |
| ANTI-ICING SYSTEM | 2014 |
|
RU2583111C1 |
| METHOD OF REDUCING EFFECT OF ICING ON AERODYNAMIC SURFACE | 2019 |
|
RU2724026C1 |
| ANTI-ICING DEVICE | 1997 |
|
RU2112708C1 |
| AUTOMATED ELECTROPULSE DE-ICING DEVICE | 2016 |
|
RU2648656C2 |
| METHOD FOR PREVENTING THE FORMATION AND REMOVAL OF ICE | 2020 |
|
RU2756065C1 |
| METHOD OF ANTI-ICING PROTECTION OF STRUCTURAL MEMBERS OF FLYING VEHICLES | 2002 |
|
RU2233232C2 |
| COMBINED ANTI-ICE SYSTEM | 2013 |
|
RU2536419C1 |
| ELECTRIC PULSE SYSTEM FOR REMOVAL OF ICE FORMATION FROM SKINNING OF AIRCRAFT UNITS | 2019 |
|
RU2704699C1 |
| SYSTEM OF PROTECTION OF OBJECT SURFACE FROM ICE FORMATION | 2006 |
|
RU2329182C1 |
