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- Article name
- Sandwich constructions with syntactic core for the aerospace parts
- Authors
- SOKOLOV I. I., , 7081291@gmail.com, All-Rusian Institute Aviation Materials, Moscow, Russia
KOGAN D. I., , kogan.viam@yandex.ru, All-Rusian Institute Aviation Materials, Moscow, Russia
RASKUTIN A. E., , araskutin@yandex.ru, All-Rusian Institute Aviation Materials, Moscow, Russia
BABIN A. N., , babin_viam@mail.ru, All-Rusian Institute Aviation Materials, Moscow, Russia
FILATOV A. A., , mbbbox@gmail.com, Experimental Desing Office "Sukhogo", Moscow, Russia
MOROZOV B. B., , mbbbox@gmail.com, Experimental Desing Office "Sukhogo", Moscow, Russia
- Keywords
- syntactic foam / cyanate ester resins / glass fiber reinforced plastics (GFRP) / carbon fiber reinforced plastics (CFRP) / sandwich panels
- Year
- 2014 Issue 1 Pages 37 - 42
- Code EDN
- Code DOI
- Abstract
- The main aspects of development and existing technical solutions in the field of manufacturing of sandwich constructions with syntactic core are described. The sandwich construction, based on cyanate ester matrix with glass microspheres and carbon fibres are shown. The high mechanical characteristic of sandwich costruction are marked (with temperature 160 oC). The results of practical mechanical data and mathematic data has a good correlation. The prospects of using syntactic cores for manufacturing of aerospace parts are shown.
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