Design and Qualification of a Advanced Hybrid Filament-Wound Composite Pressure Vessel for Aircraft Application

Zhi Dong Liu; Bin Yu; Qing Chen Jin; Wei Chen

doi:10.4028/www.scientific.net/AMR.631-632.67

Paper Titles

Study of Transient Liquid-Phase Bonding of SiC Particle Reinforced Aluminum Matrix Composite
p.44

Design, Development and Qualification of High Performance Load Sharing Composite Pressure Vessel for Aircraft Application
p.50

Study on Properties Comparison of AH36 Opened Plate and Original Plate
p.56

Solidification Behavior of Rapidly Quenched LaFe_13-xSi_x Alloys
p.62

Design and Qualification of a Advanced Hybrid Filament-Wound Composite Pressure Vessel for Aircraft Application
p.67

Study on Measuring Particle Size Distribution of a Nanodiamond Powder
p.73

The Rietveld Refinement of Thermal Synthesized Rhombohedra Boron Nitride Micro-Rod
p.78

Preparation of TPU-Polyester Coated Fabrics with High Adhesive Performance
p.82

Sonochemical Preparation of Polymer Microcapsules
p.86

HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 631-632Design and Qualification of a Advanced Hybrid...

Design and Qualification of a Advanced Hybrid Filament-Wound Composite Pressure Vessel for Aircraft Application

Abstract:

This paper describes a composite pressure vessel(COPV) development program which have been finished by Lanzhou Institute of Physics (LIP). In order to dramatically improve reliability and safety of COPV applied in military aircraft, this COPV(L376-COPV) design relies partly on the heritage of mature technologies and was developed in combination with existing and new technologies, Unlike traditional COPV, the impact resistant capability from high energy bullet of L376-COPV is improved greatly by liner material heart treatment and T800/K49 fiber hybrids over-wrap. L376-COPV design, analysis, manufacturing, testing and results was introduced.

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Periodical:

Advanced Materials Research (Volumes 631-632)

Pages:

67-72

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.631-632.67

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Online since:

January 2013

Authors:

Zhi Dong Liu, Bin Yu, Qing Chen Jin, Wei Chen

Keywords:

Aircraft, Composite Pressure Vessel, Design, Qualification Test

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