FIELD: aviation.
SUBSTANCE: group of inventions relates to aircraft, device for elimination of icing and prevention of ice formation, profiled body and method for elimination of icing of aircraft surface area. Device for eliminating icing comprises heat-release device or hybrid device, deforming device, ice detecting device. Profiled body comprises a device for elimination of icing, device for preventing ice formation, reducing adhesion of ice coating deforming device. To eliminate icing of aircraft surface area made with a property reducing ice adhesion, heat energy is introduced at a given line in a certain manner for subsequent fracture of ice by deformation of a portion of surface and its removal from surface.
EFFECT: eliminating ice from surface of aircraft and prevention of its formation.
21 cl, 7 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ANTI-ICING SYSTEM | 2014 |
|
RU2583111C1 |
| METHOD FOR PREVENTING THE FORMATION AND REMOVAL OF ICE | 2020 |
|
RU2756065C1 |
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|
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|
RU2489320C2 |
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|
RU2768992C1 |
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|
RU2218291C1 |
| METHOD OF DETERMINATION OF AVAILABILITY AND INTENSITY OF ICING OF FLYING VEHICLE | 1992 |
|
RU2005666C1 |
| GROUND DEICING DEVICE | 2007 |
|
RU2384477C2 |
| DEVICE TO DETECT AND REMOVE ICE OR FLUID LAYER | 2007 |
|
RU2453475C2 |
| METHOD OF DETECTION OF PRESENCE AND INTENSITY OF AIRCRAFT ICING | 2007 |
|
RU2341413C1 |
