FIELD: engines and pumps.
SUBSTANCE: proposed assembly comprises first and second elements and connector arranged there between to protect the surface of second element. Said connector comprises structure-forming skin secured to first element and porous material applied on said structure-forming skin and coupled with said second element. This assembly can be arranged in nacelle air intake of turbojet equipped with pneumatic deicer.
EFFECT: decreased weight, possibility of application in high-temperature zone.
22 cl, 7 dwg, 1 tbl
| Title | Year | Author | Number |
|---|---|---|---|
| SOUNDPROOF PANEL, AIR INTAKE DESIGN AND INNER FIXED STRUCTURE WITH SUCH PANEL FOR AIRCRAFT ENGINE NACELLE | 2009 |
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| CELLULAR STRUCTURE FOR NOISE ABSORBING PANELS | 2008 |
|
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| METHOD OF ARRANGING ANTI-ICING SYSTEM AT NACELLE PANEL | 2009 |
|
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| METHOD OF NACELLE DEICING ELEMENT FABRICATION | 2009 |
|
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| SOUND-ABSORBING PANEL FOR EJECTOR NOZZLE | 2009 |
|
RU2526215C2 |
| SECTION OF GONDOLA AIR INTAKE EDGE WITH ELECTRIC ICE PROTECTION AND ACOUSTIC ABSORPTION ZONE | 2007 |
|
RU2422331C2 |
| FABRICATION OF BAFFLE BOARDS, PARTICULARLY, FOR AIRCRAFT | 2009 |
|
RU2519382C2 |
| AIRCRAFT POWER PLANT AND ITS AIR INTAKE | 2009 |
|
RU2537998C2 |
