2016
DOI: 10.1115/1.4034883
|View full text |Cite
|
Sign up to set email alerts
|

Quantitative Assessment of the Impact of Alternative Manufacturing Methods on Aeroengine Component Lifing Decisions

Abstract: Static structural aeroengine components are typically designed for full lifetime operation. Under this assumption, efforts to reduce weight in order to improve the performance result in structural designs that necessitate proven yet expensive manufacturing solutions to ensure high reliability. However, rapid developments in fabrication technologies such as additive manufacturing may offer viable alternatives for manufacturing and/or repair, in which case different component lifing decisions may be preferable. … Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1
1
1

Citation Types

0
15
0

Year Published

2017
2017
2022
2022

Publication Types

Select...
5
1

Relationship

2
4

Authors

Journals

citations
Cited by 12 publications
(15 citation statements)
references
References 27 publications
0
15
0
Order By: Relevance
“…They further conduct design of experiment to study cost fluctuations caused by variation of PSS design decisions, visualizing the result through spider diagrams and response surfaces. Furthermore, Thomsen et al [49] propose a valuemaximizing framework for making component lifting decision in the context of aerospace PSS design.…”
Section: Pss Cost Engineering: Insights From the Systematic Literaturmentioning
confidence: 99%
“…They further conduct design of experiment to study cost fluctuations caused by variation of PSS design decisions, visualizing the result through spider diagrams and response surfaces. Furthermore, Thomsen et al [49] propose a valuemaximizing framework for making component lifting decision in the context of aerospace PSS design.…”
Section: Pss Cost Engineering: Insights From the Systematic Literaturmentioning
confidence: 99%
“…They further conduct design of experiment to study cost fluctuations caused by variation of PSS design decisions, visualizing the result through spider diagrams and response surfaces. Furthermore, Thomsen et al, (2017) propose a valuemaximizing framework for making component lifting decision in the context of aerospace PSS design.…”
Section: Estimation By Analogymentioning
confidence: 99%
“…Unless the condition of the engine components are known, there needs to be a sufficient margin to failure at any state of operation. Typically, many components are designed to be serviced at scheduled major overhauls only, and individual components may be replaced or repaired pre-maturely with their real capability (Thomsen et al 2017). This is seen as an overdesign issue and a candidate for optimization.…”
Section: Different Terms For Margins Across the Design Processmentioning
confidence: 99%