Built-in chaining: introducing complex components into architectural synthesis

Author(s):  
P. Marwedel ◽  
B. Landwehr ◽  
R. Domer
2020 ◽  
Vol 40 (10) ◽  
pp. 870-872
Author(s):  
T. R. Ablyaz ◽  
E. S. Shlykov ◽  
K. R. Muratov

Author(s):  
Gabriel Caffarena ◽  
Juan A. López ◽  
Gerardo Leyva ◽  
Carlos Carreras ◽  
Octavio Nieto-Taladriz

2021 ◽  
Vol 1748 ◽  
pp. 022027
Author(s):  
Jin Shuo ◽  
Ren Yuan ◽  
Ma Qingzeng ◽  
Ge Hailong ◽  
Li Wenlong ◽  
...  

2012 ◽  
Vol 531-532 ◽  
pp. 135-140 ◽  
Author(s):  
Yu Di Zhang ◽  
Hai Feng Hu ◽  
Chang Rui Zhang ◽  
Guang De Li

C/SiC composites have widely application prospects in the field of aeronautic and aerospace for their excellent properties. The joining of C/SiC composites is a key to fabricate large and complex components. In this paper, 1D C/SiC pins were prepared by precursor infiltration and pyrolysis (PIP) process and used to join C/SiC composites by Slurry react (SR) and PIP process. The shear strength of the C/SiC pins with different carbon fiber volumes was investigated with the maximum shear strength as high as 339.46MPa. Influences of C/SiC pins on the joining properties of C/SiC composites were studied. The shear strength and flexural strength of C/SiC-C/SiC joining are improved from 9.17MPa and 30.41MPa without pins to 20.06MPa and 75.03MPa with one C/SiC pin (diameter 2mm), respectively. The reliability of C/SiC-C/SiC joining is also improved with C/SiC pins in that the fracture mode changes from catastrophic without pins to non-catastrophic. The SEM photos show a strong bond between joining layer and C/SiC composites without obvious interface.


2019 ◽  
Vol 48 ◽  
pp. 81-85 ◽  
Author(s):  
David G Rattray ◽  
Leonard J Foster

2018 ◽  
Vol 29 (11) ◽  
pp. 665-689
Author(s):  
C. Hartmann ◽  
R. Chenouard ◽  
E. Mermoz ◽  
A. Bernard

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