Journal article
The effect of external casing impingement cooling manifold standoff distance on casing contraction for thermal control of blade tip clearance
- Abstract:
-
Thermal closure of the engine casing is widely used to minimize undesirable blade tip leakage flows thus improving jet engine performance. This may be achieved using an impingement cooling scheme on the external casing wall, provided by manifolds attached to the outside of the engine. The assembly tolerance of these components leads to variation in the standoffdistance between the manifold and the casing, and its effects on casing contraction must be understood to allow build tolerance to be ...
Expand abstract
- Publication status:
- Published
- Peer review status:
- Peer reviewed
Actions
Authors
Funding
Rolls-Royce plc
More from this funder
Technology
Strategy Board
More from this funder
Bibliographic Details
- Publisher:
- American Society of Mechanical Engineers Publisher's website
- Journal:
- Journal of Turbomachinery Journal website
- Volume:
- 140
- Issue:
- 2
- Pages:
- 021005
- Publication date:
- 2017-11-29
- DOI:
- EISSN:
-
1528-8900
- ISSN:
-
0889-504X
- Source identifiers:
-
811498
Item Description
- Pubs id:
-
pubs:811498
- UUID:
-
uuid:7e267451-54fd-4fa4-be1b-9c770c0faec1
- Local pid:
- pubs:811498
- Deposit date:
- 2018-11-27
Terms of use
- Copyright holder:
- Rolls-Royce plc
- Copyright date:
- 2017
- Notes:
- © 2018 by Rolls-Royce plc.
If you are the owner of this record, you can report an update to it here: Report update to this record