FIELD: aeronautical engineering and rocketry.
SUBSTANCE: novelty is that metal frame coning toward end is installed on outer surface of ceramic hood and joined thereto by means of silicone rubber base adhesive. Installed between them on mutually coordinated conical surfaces is enclosed corrugated insert whose temperature coefficient of linear expansion is higher than that of metal frame material; it is joined to ceramic hood by means of silicone rubber base adhesive. Butt-end of ceramic hood rests on composite support assembled of two rings made of material whose temperature coefficient of linear expansion is higher than that of metal frame and joined together by means of stop screws. Mechanical coupling of one of composite support rings is ensured due to ring split and its locking within internal drilling of metal frame.
EFFECT: enhanced performance characteristics.
3 cl, 3 dwg
Title | Year | Author | Number |
---|---|---|---|
ANTENNA DOME | 2012 |
|
RU2500055C1 |
NOSE FAIRING OF FLIGHT VEHICLE | 2004 |
|
RU2269844C1 |
ANTENNA FAIRING | 2001 |
|
RU2189674C1 |
ANTENNA DOME | 2011 |
|
RU2447549C1 |
ANTENNA FAIRING | 2001 |
|
RU2189673C1 |
ANTENNA DOME | 2012 |
|
RU2494504C1 |
PERMANENT CONNECTIVE JOINT | 2002 |
|
RU2231875C2 |
MISSILE ANTENNA NOSE FAIRING | 2001 |
|
RU2189672C1 |
CONE | 2002 |
|
RU2225664C2 |
ANTENNA NOSE FAIRING | 2004 |
|
RU2273077C1 |
Authors
Dates
2006-07-20—Published
2005-01-11—Filed