Accelerated whole engine structural design process based on data reuse
Accelerated whole engine structural design process based on data reuse
The design of complex engineering systems, such as a gas turbine engine, is often decomposed into system design and subsystem/component design. Both the system and subsystem designs normally go through several design iterations. For each iteration, a series of analyses, simulations, optimisations and, at times, experiments are carried out to find the optimum. Traditionally, the data generated in one design iteration is not fed explicitly into the next iteration. This is because a new design iteration can often start with structural changes and the new design is considered to be topologically different from the previous design. Most existing design optimisation techniques cannot leverage the data across multiple design iterations and each design iteration has, therefore, to start almost from scratch. This paper presents a novel structural design process that is capable of accelerating both the component level and system level design by reusing data from previous design iterations. A case study of multiple design variables and topology changes in three components of a whole engine model (WEM) is carried out and it demonstrates that the proposed method employing surrogate modelling and data reuse technologies can significantly reduce analysis costs from one design iteration to the next.
Wang, Leran
91d2f4ca-ed47-4e47-adff-70fef3874564
Cimpoesu, Petru-Cristian
7c428386-b15e-4aa3-a5a5-14dd1317b06d
Toal, David
dc67543d-69d2-4f27-a469-42195fa31a68
Anobile, Alessandro
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3 October 2023
Wang, Leran
91d2f4ca-ed47-4e47-adff-70fef3874564
Cimpoesu, Petru-Cristian
7c428386-b15e-4aa3-a5a5-14dd1317b06d
Toal, David
dc67543d-69d2-4f27-a469-42195fa31a68
Anobile, Alessandro
3e1fabd6-1592-47c3-9080-417707be326b
Wang, Leran, Cimpoesu, Petru-Cristian, Toal, David and Anobile, Alessandro
(2023)
Accelerated whole engine structural design process based on data reuse.
Royal Aeronautical Society 8th Aircraft Structural Design Conference, Royal Aeronautical Society, London, United Kingdom.
03 - 04 Oct 2023.
9 pp
.
Record type:
Conference or Workshop Item
(Paper)
Abstract
The design of complex engineering systems, such as a gas turbine engine, is often decomposed into system design and subsystem/component design. Both the system and subsystem designs normally go through several design iterations. For each iteration, a series of analyses, simulations, optimisations and, at times, experiments are carried out to find the optimum. Traditionally, the data generated in one design iteration is not fed explicitly into the next iteration. This is because a new design iteration can often start with structural changes and the new design is considered to be topologically different from the previous design. Most existing design optimisation techniques cannot leverage the data across multiple design iterations and each design iteration has, therefore, to start almost from scratch. This paper presents a novel structural design process that is capable of accelerating both the component level and system level design by reusing data from previous design iterations. A case study of multiple design variables and topology changes in three components of a whole engine model (WEM) is carried out and it demonstrates that the proposed method employing surrogate modelling and data reuse technologies can significantly reduce analysis costs from one design iteration to the next.
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RAeS_2023_v4
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Published date: 3 October 2023
Venue - Dates:
Royal Aeronautical Society 8th Aircraft Structural Design Conference, Royal Aeronautical Society, London, United Kingdom, 2023-10-03 - 2023-10-04
Identifiers
Local EPrints ID: 482527
URI: http://eprints.soton.ac.uk/id/eprint/482527
PURE UUID: 65548c0b-d124-49ad-94bb-fa34091f3c50
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Date deposited: 10 Oct 2023 16:45
Last modified: 18 Mar 2024 03:07
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Contributors
Author:
Petru-Cristian Cimpoesu
Author:
Alessandro Anobile
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