Skip to Main Content
Article navigation
Volume 74, Issue 1
1 February 2002
Aircraft Engineering and Aerospace Technology Cover Image for Volume 74, Issue 1
Editors
Phil Webb
Phil Webb
Search for other works by this author on:
This Site
PubMed
Google Scholar
Research Article| February 01 2002

EDMing turbopump blisks Available to Purchase

H. Zhan;
H. Zhan
H. Zhan is Doctor of Engineering, Research Fellow at the Research Institute of Non‐traditional Machining & Mechatronics, Harbin Institute of Technology, Harbin 150001, P.R. China
Search for other works by this author on:
This Site
PubMed
Google Scholar
W. Zhao
W. Zhao
W. Zhao is Doctor of Engineering, Professor at the Research Institute of Non‐traditional Machining & Mechatronics, Harbin Institute of Technology, Harbin 150001, P.R. China
Search for other works by this author on:
This Site
PubMed
Google Scholar
Author & Article Information
Publisher: Emerald Publishing
Online ISSN: 1758-4213
Print ISSN: 1748-8842
© MCB UP Limited
2002
Aircraft Engineering and Aerospace Technology: An International Journal (2002) 74 (1): 19–22.
https://doi.org/10.1108/00022660210414994

Turbine blisks designed for advanced liquid rocket engine turbopumps are usually of a timed structure with twisted blades, and they can be machined effectively with the electrical discharge machining (EDM) process. After the machining specifications have been designated, the EDM process of a turbopump turbine blisk is discussed, in which the kernel problems are the design of the electrode and the searching of an interference free path to feed the electrode to machine the blisk.

Keywords:
Turbines, Engines
© MCB UP Limited
2002
You do not currently have access to this content.
Don't already have an account? Register

Purchased this content as a guest? Enter your email address to restore access.

Please enter valid email address.
Email address must be 94 characters or fewer.
Pay-Per-View Access
$39.00
Rental
This article is also available for rental through DeepDyve. Read this now at DeepDyve
184 Views
View Metrics
Robust longitudinal control for a hypersonic glider with moving-mass actuation via L1-augmented dynamic inversion
Nonlinear geometric multivariable control for unmanned aircraft flight system
Numerical simulation of strut angle optimization for enhanced performance in DLR scramjet combustor
Active disturbance rejection control optimized via chaotic comprehensive learning pigeon-inspired optimization for flapping-wing aerial vehicle

Suggested Reading

Optimal design and control of gas‐turbine engine components: a multicriteria approach
Aircraft Engineering and Aerospace Technology: An International Journal (December,1997)
CORRESPONDENCE. THE STEAM TURBINE.
Minutes of the Proceedings of the Institution of Civil Engineers (January,1906)
ENGINEERING CONFERENCE, 26TH MAY 1897, SHIPBUILDING. THE RELATIVE ADVANTAGES AND DISADVANTAGES OF ROTARY AND RECIPROCATING ENGINES AS APPLIED TO SHIP PROPULSION. (ABSTRACT).
Minutes of the Proceedings of the Institution of Civil Engineers (January,1897)
Wear debris analysis group (1982‐84)
Industrial Lubrication and Tribology (April,1994)
DISCUSSION. THE STEAM TURBINE.
Minutes of the Proceedings of the Institution of Civil Engineers (January,1906)

Recommended for you

These recommendations are informed by your reading behaviors and indicated interests.

Cited By

Google Scholar
This Feature Is Available To Subscribers Only

or Create an Account

Close Modal
Close Modal