Consolidation of reactive Ultem® powder-coated carbon fiber tow for space structure composites by resistive heating

被引:26
作者
Naskar, Amit K.
Edie, Dan D. [1 ]
机构
[1] Clemson Univ, Dept Chem Engn, Clemson, SC 29634 USA
[2] Clemson Univ, Ctr Adv Engn Fibers & Films, Clemson, SC 29634 USA
关键词
phenylethynyl terminated poly(etherimide); reactive Ultem (R); carbon fiber; resistive heating; inflatable space structure;
D O I
10.1177/0021998306061300
中图分类号
TB33 [复合材料];
学科分类号
摘要
In this exploratory study, polyacrylonitrile (PAN)-based carbon fiber tows are coated with a commercial, heat-crosslinkable polyetherimide (Ultem(R)) powder. Then an electrical current is applied across the powder-coated fiber tows (towpreg) to melt the thermoplastic powder and form rigidized composites. These consolidated composite samples are characterized by scanning electron microscopy (SEM) and conventional tensile testing. Measuring the applied current and the degree of consolidation yielded the power requirement for successful wetting of the carbon fiber tows by Ultem melt, both on earth and in outer space. The results show that resistive heating is a feasible route for the rigidization of inflatable composite structures in space.
引用
收藏
页码:1871 / 1883
页数:13
相关论文
共 19 条
[1]  
Allen L.E., 1988, J THERMOPLAST COMPOS, V1, P371, DOI [10.1177/089270578800100405, DOI 10.1177/089270578800100405]
[2]   IMPREGNATION DYNAMICS OF CARBON-FIBER TOWS [J].
BAYRAMLI, E ;
POWELL, RL .
JOURNAL OF COMPOSITE MATERIALS, 1992, 26 (10) :1427-1442
[3]  
*BP AM CHEM, TYP PROP THORN CARB
[4]  
BULLIONS TA, 2000, INT SAMPE S EXHIBITI, V45, P1048
[5]  
CHMIELEWSKI C, 1991, P AM SOC COMP TECHN, P993
[6]  
Cioeta M, 2000, SCI ENG COMPOS MATER, V9, P91
[7]   Elastic behaviour and low-temperature specific heat of linear and reticulated amorphous polymers [J].
D'Angelo, G ;
Tripodo, G ;
Carini, G ;
Bartolotta, A ;
Salvato, G ;
Privalko, VP .
PHILOSOPHICAL MAGAZINE B-PHYSICS OF CONDENSED MATTER STATISTICAL MECHANICS ELECTRONIC OPTICAL AND MAGNETIC PROPERTIES, 1999, 79 (11-12) :1889-1895
[8]   Consolidation process of PEEK/carbon composite for aerospace applications [J].
Denault, J ;
Dumouchel, M .
ADVANCED PERFORMANCE MATERIALS, 1998, 5 (1-2) :83-96
[9]   The effect of processing on the structure and properties of carbon fibers [J].
Edie, DD .
CARBON, 1998, 36 (04) :345-362
[10]   Modeling of the consolidation of polycarbonate carbon fiber towpregs [J].
Nunes, JP ;
Bernardo, CA ;
Pouzada, AS ;
Edie, DD .
POLYMER COMPOSITES, 1999, 20 (02) :260-268