Gas turbine blade manufacturing by use of epoxy resin tooling and silicone rubber molding techniques
Gas turbine blade manufacturing by use of epoxy resin tooling and silicone rubber molding techniques
Purpose:
Conventional investment casting of turbine blades is a time consuming and expensive process due to the complications in wax injection steps and the complex shape of airfoil surfaces. By using rapid investment casting, a substantial improvement in the gas turbine blade manufacturing process can be expected. However, this process needs to be able to compete with conventional investment casting from a dimensional accuracy view of point. The purpose of this paper is to investigate the manufacture of gas turbine blades via two indirect rapid tooling (RT) technologies, namely epoxy (EP) resin tooling and silicon rubber molding.
Design/methodology/approach:
The second stage blade of a Ruston TA 1750 gas turbine (rated at 1.3 MW) was digitized by a coordinate measuring machine. The aluminum-filled EP resin and silicon rubber molds were fabricated using StereoLithography master models. Several wax patterns were made by injection in the EP resin and silicone rubber molds. These wax patterns were utilized for ceramic shell fabrication and blade casting.
Findings:
Dimensional inspection of cast blades showed that silicone rubber molding was not a suitable approach for production of blade wax patterns. The maximum deviation for the final cast blade made using the silicone rubber mold was þ0.402 mm. The maximum deviation for the final cast blade made using the EP resin mold was lower at 20.282 mm. This showed that EP resin tooling could enable new cost-effective solutions for small batch production of gas turbine blades.
Practical implications:
The research results presented will give efficient industrial approach and scientific insight of the gas turbine blade manufacturing by use of rapid technologies.
Originality/value:
There are some general research works related to utilization of rapid technologies for manufacturing of gas turbine blade. However, this paper presents a unique procedure of integrated reverse engineering and RT technologies for rapid investment casting of gas turbine blade through presenting comprehensive comparison between two techniques from dimensional accuracy view of point.
107-115
Vaezi, Mohammad
828e14c1-3236-4153-8f69-3837233f48ed
Safaeian, Davood
38e08e3e-3f9b-437d-8615-1e2a10b15012
Chua, Chee Kai
c18f7791-75be-42f8-99cb-6ec71d2184c4
May 2011
Vaezi, Mohammad
828e14c1-3236-4153-8f69-3837233f48ed
Safaeian, Davood
38e08e3e-3f9b-437d-8615-1e2a10b15012
Chua, Chee Kai
c18f7791-75be-42f8-99cb-6ec71d2184c4
Vaezi, Mohammad, Safaeian, Davood and Chua, Chee Kai
(2011)
Gas turbine blade manufacturing by use of epoxy resin tooling and silicone rubber molding techniques.
Rapid Prototyping Journal, 17 (2), .
(doi:10.1108/13552541111113853).
Abstract
Purpose:
Conventional investment casting of turbine blades is a time consuming and expensive process due to the complications in wax injection steps and the complex shape of airfoil surfaces. By using rapid investment casting, a substantial improvement in the gas turbine blade manufacturing process can be expected. However, this process needs to be able to compete with conventional investment casting from a dimensional accuracy view of point. The purpose of this paper is to investigate the manufacture of gas turbine blades via two indirect rapid tooling (RT) technologies, namely epoxy (EP) resin tooling and silicon rubber molding.
Design/methodology/approach:
The second stage blade of a Ruston TA 1750 gas turbine (rated at 1.3 MW) was digitized by a coordinate measuring machine. The aluminum-filled EP resin and silicon rubber molds were fabricated using StereoLithography master models. Several wax patterns were made by injection in the EP resin and silicone rubber molds. These wax patterns were utilized for ceramic shell fabrication and blade casting.
Findings:
Dimensional inspection of cast blades showed that silicone rubber molding was not a suitable approach for production of blade wax patterns. The maximum deviation for the final cast blade made using the silicone rubber mold was þ0.402 mm. The maximum deviation for the final cast blade made using the EP resin mold was lower at 20.282 mm. This showed that EP resin tooling could enable new cost-effective solutions for small batch production of gas turbine blades.
Practical implications:
The research results presented will give efficient industrial approach and scientific insight of the gas turbine blade manufacturing by use of rapid technologies.
Originality/value:
There are some general research works related to utilization of rapid technologies for manufacturing of gas turbine blade. However, this paper presents a unique procedure of integrated reverse engineering and RT technologies for rapid investment casting of gas turbine blade through presenting comprehensive comparison between two techniques from dimensional accuracy view of point.
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More information
Published date: May 2011
Organisations:
Engineering Science Unit
Identifiers
Local EPrints ID: 348235
URI: http://eprints.soton.ac.uk/id/eprint/348235
ISSN: 1355-2546
PURE UUID: 40213284-d818-4c33-a5f1-d2ca0f62ae51
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Date deposited: 11 Feb 2013 09:52
Last modified: 14 Mar 2024 12:56
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Contributors
Author:
Mohammad Vaezi
Author:
Davood Safaeian
Author:
Chee Kai Chua
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