DocumentCode
3439236
Title
Notice of Retraction
Shaping of continuous carbon fibre reinforced 5A06 composites by vacuum anti-pressure infiltration technology
Author
Xinkun Wang ; Shenghai Xi ; Yi Chen
Author_Institution
Beijing Aeronaut. Technol. Res. Center, Beihang Univ., Beijing, China
fYear
2013
fDate
15-18 July 2013
Firstpage
1065
Lastpage
1068
Abstract
Notice of Retraction
After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.
We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.
The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.
This paper studies key parameters of continuous carbon fibre reinforced 5A06 composites technique by the vacuum anti-pressure infiltration. Production steps of composites are generally described as follows: preform manufacturing, liquid metal infiltration by gas pressure and finishing. Results illustrate that besides the remained ratio of fibre tensile strength, the compression strength of fiber preform is remarkably influenced by temperature and mechanical properties of composites. When preform temperature decreased from 680°C to 620°C and the fibres are coated C-Al2O3 layer, the tensile strength of the composites increased from 69MPa to 651MPa.
After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.
We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.
The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.
This paper studies key parameters of continuous carbon fibre reinforced 5A06 composites technique by the vacuum anti-pressure infiltration. Production steps of composites are generally described as follows: preform manufacturing, liquid metal infiltration by gas pressure and finishing. Results illustrate that besides the remained ratio of fibre tensile strength, the compression strength of fiber preform is remarkably influenced by temperature and mechanical properties of composites. When preform temperature decreased from 680°C to 620°C and the fibres are coated C-Al2O3 layer, the tensile strength of the composites increased from 69MPa to 651MPa.
Keywords
carbon fibre reinforced composites; compressive strength; liquid metals; preforms; squeeze casting; tensile strength; vacuum techniques; compression strength; continuous carbon fibre reinforced 5A06 composites; fibre tensile strength; finishing; gas pressure; liquid metal infiltration; preform manufacturing; shaping; squeeze casting; temperature 680 degC to 620 degC; vacuum antipressure infiltration technology; Acoustics; Carbon; Heating; Metals; Preforms; Silicon carbide; Temperature; 5A06 matrix; continuous carbon fibre reinforcements; vacuum anti-pressure infiltration;
fLanguage
English
Publisher
ieee
Conference_Titel
Quality, Reliability, Risk, Maintenance, and Safety Engineering (QR2MSE), 2013 International Conference on
Conference_Location
Chengdu
Print_ISBN
978-1-4799-1014-4
Type
conf
DOI
10.1109/QR2MSE.2013.6625749
Filename
6625749
Link To Document