FIELD: aircraft engineering.
SUBSTANCE: proposed assembly comprises metal frame connected with ceramic cowling by the ply of resilient thermosetting resin. Frame circumference has circular groove filled with said resin at centre of which crossed through slots are made at 45 degrees to the frame lengthwise axis. Through bores are made at edges and at centre of crossing of grooves. Frame part facing said cowling has temperature compensators composed by extra axial through groves with bores to make collet lugs to contact by their outer surface with cowling inner surface. Crossed slots and temperature compensators are arranged to alternate regularly.
EFFECT: higher reliability of attachment.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ATTACHMENT POINT BETWEEN CERAMIC FAIRING AND FLYING-VEHICLE BODY | 2004 |
|
RU2258283C1 |
| ANTENNA FAIRING | 2018 |
|
RU2690040C1 |
| ATTACHMENT ASSEMBLY OF CERAMIC FAIRING WITH METAL CASING OF AIRCRAFT | 2015 |
|
RU2581886C1 |
| ANTENNA FAIRING | 2020 |
|
RU2735381C1 |
| METHOD OF CONNECTION OF CERAMIC FAIRING WITH METAL CASING OF AIRCRAFT | 2014 |
|
RU2566643C1 |
| METHOD FOR CONNECTING THE CERAMIC FAIRING WITH THE METAL BODY OF THE AIRCRAFT | 2021 |
|
RU2764158C1 |
| ANTENNA DOME | 2012 |
|
RU2500055C1 |
| ATTACHMENT FITTING OF CERAMIC COVER OF ANTENNA DOME TO METAL FRAME | 2014 |
|
RU2559732C1 |
| FAIRING | 2017 |
|
RU2654953C1 |
| FLYING VEHICLE ANTENNA FAIRING | 2006 |
|
RU2316088C1 |
