FIELD: aeronautics; aviation; cosmonautics.
SUBSTANCE: group of inventions relates to anti-icing systems for aircraft and method of removing or preventing formation of ice on aircraft blades with rotor. In the first version, the system comprises combined blades divided into sections in a certain way, plurality of first and second heating systems distributed on different rotor sections, control unit. In the second version, the system differs from the first by arrangement of heating elements. Method includes determination of conditions of icing, provision of conditions for power supply to heating elements.
EFFECT: providing all-weather use of aircraft.
20 cl, 8 dwg, 1 tbl
| Title | Year | Author | Number |
|---|---|---|---|
| ANTI-ICING SYSTEM | 2014 |
|
RU2583111C1 |
| METHOD OF PREVENTION OF FORMATION AND REMOVAL OF ICE FROM COMPOSITE STRUCTURAL ELEMENTS AND DEVICE FOR ITS IMPLEMENTATION | 2015 |
|
RU2578079C1 |
| METHOD AND DEVICE TO PREVENT AIRCRAFT SKIN ICING | 2007 |
|
RU2466064C2 |
| IMPROVED DESIGN OF THE INPUT DEVICE | 2018 |
|
RU2727820C2 |
| METHOD OF COUNTERACTION TO THE ICING OF THE WIND GENERATOR BLADES AND THE BLADE OF THE WIND GENERATOR | 2015 |
|
RU2683354C2 |
| ELECTRO-THERMAL DE-ICING SYSTEM FOR HELICOPTER BLADES | 2002 |
|
RU2226481C2 |
| METHOD OF HELICOPTER ROTOR ICING DETECTION | 2007 |
|
RU2341414C1 |
| DEVICE AND METHOD FOR ELIMINATION OF ICING AND/OR PREVENTING ICE FORMATION AND PROFILE BODY AND AIRCRAFT WITH SAID DEVICE | 2014 |
|
RU2602266C2 |
| METHOD AND DEVICE FOR PREVENTION OF WIND GENERATOR BLADES ICING | 2015 |
|
RU2685160C2 |
| ROTOR BLADE FOR HIGH-SPEED GYRODYNE AIRCRAFT | 2006 |
|
RU2408499C2 |
