FIELD: transport.
SUBSTANCE: set of inventions relates to aircraft equipment. antiicing device(1) for aircraft nacelle contains electrical tapes (5) each one of which is made of main conductor (7) oriented along tape (5) which includes straightline elements (13) and curved elements (17. The tapes (5) include spirals (15) formed by combination of several curved elements (17). Adjacent tapes (5) are built in pairs and are powered from different sources. Air intake edge of aircraft includes antiicing device (1).
EFFECT: set of inventions is aimed to prevent formation of ice chunks.
12 cl, 9 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ELECTRIC ANTI-ICING DEVICE AND CORRESPONDING MONITORING SYSTEM | 2010 |
|
RU2516909C2 |
| METHOD OF CONTROL OVER ELECTRIC DEICING SYSTEM | 2009 |
|
RU2501717C2 |
| SECTION OF GONDOLA AIR INTAKE EDGE WITH ELECTRIC ICE PROTECTION AND ACOUSTIC ABSORPTION ZONE | 2007 |
|
RU2422331C2 |
| TURBOJET NACELLE AIR INTAKE EDGE | 2009 |
|
RU2492115C2 |
| AIR INTAKE PIEZOELECTRIC ANTI-ICING SYSTEM | 2008 |
|
RU2483000C2 |
| POWER SUPPLY CIRCUIT FOR TURBOJET ENGINE NACELLE | 2010 |
|
RU2561613C2 |
| AIR INTAKE FOR AIRCRAFT NACELLE | 2009 |
|
RU2480598C2 |
| AIRCRAFT LEADING EDGE | 2007 |
|
RU2467927C2 |
| ASSEMBLY OF ELEMENTS CONNECTED BY DEVICE PROTECTING SURFACE OF ONE OF SAID ELEMENTS | 2009 |
|
RU2521824C2 |
| NACELLE AIR INTAKE AND NACELLE CONTAINING SUCH AIR INTAKE | 2020 |
|
RU2801764C2 |
