Abstract
Commercially pure (CP-70) titanium is used as the metallic liner for composite overwrapped pressure vessels used in satellite launch vehicles. The metallic liner is fabricated from domes machined out of CP-70 titanium forgings. During the hot closed-die forging of CP-70 domes from billets, the amount of deformation varies location to location, due to the non-uniform flow of material in the die cavity. This non-uniform strain distribution in the hemispherical dome results in microstructural variations along the forging axis which will remain even after annealing. The aim of the present work is to study the tensile properties, impact strength and fracture toughness of CP-70 hemispherical forging in annealed condition from top end to bottom end of domes in radial and circumferential directions with a view to understand the variation in mechanical properties to asses the design margin. Study revealed significant amount of the work-hardening difference within a forged dome even after annealing.
Similar content being viewed by others
References
Tam W H, Griffin P S, and Jackson A C, Design and Manufacture of a Composite Overwrapped Pressurant Tank Assembly, American Institute of Aeronautics & Astronautics, AIAA 2002, p 1.
Karpagaraj A, Sivashanmugam N, and Sankaranarayanasamy K, Mater Sci Eng A 640 (2015) 180.
ASTM E8, Standard Test Methods for Tension Testing of Metallic Materials, ASTM International, West Conshohocken, PA (2011).
ASTM E23, Standard Test Methods for Notched Bar Impact Testing of Metallic Materials, ASTM International, West Conshohocken, PA (2007).
ASTM E1820, Standard Test Method for Measurement of Fracture Toughness, ASTM International, West Conshohocken, PA (2011).
ASTM E3, Standard Guide for Preparation of Metallographic Specimens, ASTM International, West Conshohocken, PA (2011).
AMS 4921L, Titanium Bars, Wire, Forgings and Rings Commercially Pure 70 ksi (483 MPa) Yield strength, Aerospace Material specification, SAE Aerospace (2007).
Chun X, and Zhu W, Trans Non Ferrous Met Soc China 22 (2012) 1939.
ASTM E646, Standard Test Method for Tensile Strain-Hardening Exponents (n-Values) of Metallic Sheet Materials, ASTM International, West Conshohocken, PA (2007).
Sharma V M J, Sree Kumar K, Nageswara Rao B, and Pathak S D, MetallMater Trans A 40A (2009) 3186.
Roach M D, Williamson R S, Thomas J A, Griggs J A, and Zardiackas L D, J Biomed Mater Res B Appl Biomater 102B (2014) 73.
Acknowledgements
The authors wish to thank Director, VSSC for his permission to publish this work.
Author information
Authors and Affiliations
Corresponding author
Additional information
Publisher's Note
Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.
Rights and permissions
About this article
Cite this article
Manikandan, P., Rao, G.S., Muneshwar, P. et al. Tensile and Fracture Properties of Commercially Pure Titanium (CP-70) Hemispherical Forgings. Trans Indian Inst Met 72, 1469–1473 (2019). https://doi.org/10.1007/s12666-019-01593-4
Received:
Accepted:
Published:
Issue Date:
DOI: https://doi.org/10.1007/s12666-019-01593-4