A hybrid knowledge based system for cost modelling applied to aircraft gas turbine design
A hybrid knowledge based system for cost modelling applied to aircraft gas turbine design
This paper presents a novel technique for representing cost information for a candidate design. The underlying principle involves the use of a knowledge based system for cost modelling that makes the cost implications of design decisions more visible and available to the designer at the concept design stage.
The development of a hybrid between hierarchical trees and an object-oriented knowledge representation of cost and manufacturing knowledge is given.
The representation of cost and manufacturing information as an abstract product structure and reusable object libraries is shown. The extraction of key geometric information needed from a CAD system is discussed and demonstrated.
The tool is intended to provide a clear and easily audited response to incremental changes in component geometry and the product definition. The tool is also capable of modelling stochastic quantities present in cost models and can therefore analyse cost risk.
A case study demonstrating the research applied to a Rolls-Royce aircraft gas turbine engine component is presented. This case study also demonstrates how the tool is deployed using web technologies through a client running standard browser software.
life cycle cost design gas turbine knowledge concept
Scanlan, J.P.
7ad738f2-d732-423f-a322-31fa4695529d
Tammineni, S.
be40c497-1869-4512-917e-6d3728bbca90
Keane, A. J.
26d7fa33-5415-4910-89d8-fb3620413def
Scanlan, J.P.
7ad738f2-d732-423f-a322-31fa4695529d
Tammineni, S.
be40c497-1869-4512-917e-6d3728bbca90
Keane, A. J.
26d7fa33-5415-4910-89d8-fb3620413def
Scanlan, J.P., Tammineni, S. and Keane, A. J.
(2007)
A hybrid knowledge based system for cost modelling applied to aircraft gas turbine design.
Journal of Engineering Design.
(Submitted)
Abstract
This paper presents a novel technique for representing cost information for a candidate design. The underlying principle involves the use of a knowledge based system for cost modelling that makes the cost implications of design decisions more visible and available to the designer at the concept design stage.
The development of a hybrid between hierarchical trees and an object-oriented knowledge representation of cost and manufacturing knowledge is given.
The representation of cost and manufacturing information as an abstract product structure and reusable object libraries is shown. The extraction of key geometric information needed from a CAD system is discussed and demonstrated.
The tool is intended to provide a clear and easily audited response to incremental changes in component geometry and the product definition. The tool is also capable of modelling stochastic quantities present in cost models and can therefore analyse cost risk.
A case study demonstrating the research applied to a Rolls-Royce aircraft gas turbine engine component is presented. This case study also demonstrates how the tool is deployed using web technologies through a client running standard browser software.
Text
Sree_datum_Journal_of_Engineering_design_paper.doc
- Other
More information
Submitted date: 19 January 2007
Keywords:
life cycle cost design gas turbine knowledge concept
Identifiers
Local EPrints ID: 43226
URI: http://eprints.soton.ac.uk/id/eprint/43226
ISSN: 0954-4828
PURE UUID: f8f9857e-050a-450e-983c-083d624036b5
Catalogue record
Date deposited: 17 Jan 2007
Last modified: 16 Mar 2024 02:53
Export record
Contributors
Author:
S. Tammineni
Download statistics
Downloads from ePrints over the past year. Other digital versions may also be available to download e.g. from the publisher's website.
View more statistics