FIELD: electricity.
SUBSTANCE: multilayer electroconductive coating based on thermoresistant binding agent has at least two current-conducting layers of equal in strength carbon filler of harness-satin or broken twill, at least two dielectric layers alternated with the above current-conducting layers. The current-conducting layers have electric resistance of less than 10 Ohm. The dielectric layers comprise epoxy or cyanether binding agent with glass-transition temperature of 200-280°C and temperature of destruction commencement of 320-420°C and particles with size less than 100 nm containing carbon phase. The electroconductive coating has the following ratio of components, wt %: carbon filler 55-66, epoxy or cyanether binding agent 33.95-42, particles with carbon phase 0.05-3.
EFFECT: maintained high level of retained strength for the main material in polymer-composite structure in the epicentre of lightning stroke with current of 200 kA and transferred charge Q more than 30 Cb, increased resistance of the coating to dynamic and heat loads in result of lightning stroke impact, and namely: non-available delamination of the electroconductive coating from the main material in structure, decreased diameter of the binding agent destruction and pitch extraction from the top layer of the electroconductive coating, reduced diameter of harness opening into separate carbon fibres of electroconductive coating.
5 cl, 2 tbl, 3 ex
Title | Year | Author | Number |
---|---|---|---|
PANEL FROM POLYMER COMPOSITE MATERIAL WITH LIGHTNING-PROOF COATING | 2015 |
|
RU2588552C1 |
MULTILAYER LIGHTNING-PROTECTIVE COATING | 2002 |
|
RU2217320C1 |
MULTILAYER LIGHTNING-PROTECTION COATING | 2003 |
|
RU2263581C2 |
CURRENT-CONDUCTING POWDER BINDER BASED ON EPOXY COMPOSITION AND METHOD OF PRODUCING PREPREG AND REINFORCED CARBON COMPOSITE BASED ON IT (VERSIONS) | 2023 |
|
RU2820925C1 |
METHOD OF PROTECTION OF HELICOPTER FUEL TANKS AGAINST THERMAL EFFECT OF LIGHTNING CURRENT | 2000 |
|
RU2192991C2 |
LUBRICATING AGENT FOR GLASS AND BASALT FIBRE | 2014 |
|
RU2565301C1 |
METHOD FOR MANUFACTURING CARBON FIBER BASED ON WOVEN CARBON FILLER AND THERMOPLASTIC BINDER | 2020 |
|
RU2765042C1 |
PREPREG MATERIAL ABLE TO PROVIDE PROTECTION AGAINST LIGHTNING STRIKE AND RESISTANCE TO BURN-THROUGH | 2016 |
|
RU2724263C2 |
METHOD OF PRODUCING LAMINAR PLASTIC | 2015 |
|
RU2586149C1 |
POLYCYANURATE COMPOSITION, PREPREG BASED THEREON AND ARTICLE MADE THEREFROM | 2013 |
|
RU2535494C1 |
Authors
Dates
2015-10-20—Published
2014-07-22—Filed