Anisogrid composite lattice structures for spacecraft and aircraft applications

2006 ◽  
Vol 76 (1-2) ◽  
pp. 182-189 ◽  
Author(s):  
V.V. Vasiliev ◽  
A.F. Razin
2019 ◽  
Vol 225 ◽  
pp. 111192 ◽  
Author(s):  
Wenfeng Hao ◽  
Ye Liu ◽  
Tao Wang ◽  
Guangping Guo ◽  
Haosen Chen ◽  
...  

2009 ◽  
Vol 69 (11-12) ◽  
pp. 1896-1903 ◽  
Author(s):  
Hualin Fan ◽  
Fennian Jin ◽  
Daining Fang

2008 ◽  
Vol 39 (2) ◽  
pp. 176-187 ◽  
Author(s):  
Pimsiree Moongkhamklang ◽  
Dana M. Elzey ◽  
Haydn N.G. Wadley

2017 ◽  
Vol 24 (6) ◽  
pp. 919-927 ◽  
Author(s):  
ChangXian Wang ◽  
Mingji Chen ◽  
Kai Yao ◽  
Xiaolei Zhu ◽  
Daining Fang

AbstractComposite lattice structures are of considerable mechanical property and multifunctional design flexibility. However, the relatively low operating temperature of polymer composite prevents its application in high temperature or fire-proofing structures. Here, we propose a type of lightweight composite lattice sandwich structure that is capable of fire proofing as well as load bearing. In our design, the composite lattice sandwich structure is filled with heat insulation materials to interdict the thermal radiation and convection between its two facesheets. The top facesheet of the structure is covered with intumescent coating to isolate fire. Moreover, thermoresistant resin or flame retardant is adopted in manufacturing the top facesheet to improve its thermoresistance. A design procedure has been developed for such kind of fire-proofing structure, by which the material and geometry of the structure can be determined according to the fire-proofing effect. It was demonstrated by experiment that a 30-mm-thick structure, designed by the present procedure, was able to isolate 945°C fire load on the exposed surface for 3600 s, keeping the unexposed surface temperature rise below 139°C.


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