Integrated computational materials engineering from a gas turbine engine perspective
Source abstract
Abstract
Abstract In 2008, the National Research Council published a landmark report on Integrated Computational Materials Engineering (ICME) and defined it as ‘an emerging discipline that aims to integrate computational materials science tools into a holistic system that can accelerate materials development, transform the engineering design optimization process, & unify design and manufacturing’. ICME is becoming a critical enabler for reducing the design/make cycle time and getting complex systems into production more quickly. There are several reasons why this is the case. Firstly, ICME allows materials experts to develop new material systems and methods of manufacture much more quickly. Advanced new materials and their associated manufacturing processes can be tailored to deliver products that meet design requirements quickly and more effectively in terms of cost and performance. Secondly, ICME enables design processes to quantify cause and affect relationships between manufacturing methods and variability, material properties, product geometry, and design requirement margins. In the design phase, material selection itself can impose consideration of material-specific failure modes that are naturally correlated to important attributes such as strength, weight, and geometry. ICME enables designers to quickly understand the complex and probabilistic interactions between the material, manufacturing processes, manufacturing variability, and design. Thirdly, it has been shown that successful account of variability of the manufacturing processes in life calculations leads to improved accuracy in declared low cycle fatigue crack initiation and damage tolerance lives on life limited gas turbine engine components. Furthermore, ICME enables engineers to rapidly explore more effective design and manufacturing solutions for delivering superior products at lower cost, faster but not without challenges. To highlight challenges and progress toward realization of this transformational technology, a survey of recent examples of materials and manufacturing process simulations along with the overarching approach and requirements within ICME to link these simulation capabilities to design and manufacturing methods will be reviewed from a gas turbine engine perspective.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Manufacturing Process and Optimization · Material Selection and Properties · High Temperature Alloys and Creep
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (14)
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1. Matlik JF, Bolcavage A: Integrated computational materials engineering from a gas turbine engine perspective. In Symposium of integrated computational engineering - the customer’s point of view. Pittsburgh, PA: Presentation at the Materials Science & Technology 2012 Conference & Exhibition,; 2012. 8 October 2012 8 October 2012
2. Glavicic MG, Goetz RL, Shen G, Rasche JA, Ress RA III, Stillinger J: Application of ICME to turbine engine component design optimization. In 52nd AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics and materials conference. Denver; 2011. 4–7 April 2011, AIAA-2011–1738 4–7 April 2011, AIAA-2011-1738
3. National Research Council: Accelerating technology transition: bridging the valley of death for materials and processes in defense systems. The National Academies Press, Washington, DC; 2004.
4. Olson GB: Integrated Computational Materials Design: From Genome to Flight. In 54th AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics and materials conference. Boston; 2013. 8–11 April 2013, AIAA-2013–1847 8–11 April 2013, AIAA-2013-1847
5. Martin R, Evans D: Reducing costs in aircraft: the metals affordability initiative consortium. JOM 2000, 52(3):24–28. 10.1007/s11837-000-0096-y10.1007/s11837-000-0096-y ↗
6. Cowles B, Backman B, Dutton R: Verification and validation of ICME methods and models for aerospace applications. Integr Mater Manuf Innov 2012, 1: 2. 10.1186/2193-9772-1-210.1186/2193-9772-1-2 ↗
7. National Research Council: Integrated computational materials engineering: a transformational discipline for improved competitiveness and national security. The National Academies Press, Washington, DC; 2008.
8. Huron ES, Reed RC, Hardy MC, Mills MJ, Montero RE, Portella PD, Jack T: Polycrystalline γ (Ni)/γ′ (Ni3A1)-δ (Ni3Nb) eutectic Ni-base superalloys: chemistry, solidification and microstructure. In Superalloys. Edited by: Xie M, Helmink RC, Tin S. Hoboken, NJ: Wiley; 2012:633–642.
9. Villars P, Okamoto H, Cenzual K (Eds): ASM alloy. ASM International, Phase Diagrams Center, Materials Park, OH; 2007.
10. Shen G, Cooper N, Ottow N, Goetz R, Matlik J: Integration and automation of residual stress and service stress modeling for superalloy component design. In Superalloys 2012. Edited by: Huron ES, Reed RC, Hardy MC, Mills MJ, Montero RE, Portella PD, Telesman J. Hoboken: Wiley; 2012:129–134.10.1002/9781118516430.ch14 ↗
11. Keskin A, Saiz A: An integrated design system for optimization of gas turbine components. In 53rd AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics and materials conference. Honolulu; 2012. 23–26 April 2012, AIAA-2013–1408 23–26 April 2012, AIAA-2013-1408
12. EuroPAM: 16th European conference and exhibition on digital simulation for virtual engineering. Toulouse; 2006. 10–12 October 2006 10–12 October 2006
13. Azaidan M, Mills A, Harrison R: Bayesian framework for aerospace gas turbine engine prognostics. In IEEE aerospace conference. Big Sky; 2013. 2–9 March 2013 2–9 March 2013
14. Mahoney S, Stillinger J: Towards a probabilistic framework for integrated computational materials engineering. In 53rd AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics and materials conference. Honolulu; 2012. 23–26 April 2012. AIAA-2013–1529 23–26 April 2012. AIAA-2013-1529