Invention Application
- Patent Title: DEVICE FOR COOLING AN ANNULAR OUTER TURBINE CASING
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Application No.: US16623086Application Date: 2018-06-04
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Publication No.: US20200182089A1Publication Date: 2020-06-11
- Inventor: Arnaud Lasantha GENILIER , François Pierre Michel COMTE , Fabien Stéphane GARNIER , Vincent François Georges MILLIER
- Applicant: SAFRAN AIRCRAFT ENGINES
- Priority: com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@40e64f9e
- International Application: PCT/FR2018/051284 WO 20180604
- Main IPC: F01D25/14
- IPC: F01D25/14 ; F01D25/12
![DEVICE FOR COOLING AN ANNULAR OUTER TURBINE CASING](/abs-image/US/2020/06/11/US20200182089A1/abs.jpg.150x150.jpg)
Abstract:
The invention relates to a device (26) for cooling an annular outer turbine casing (17), the device (26) comprising at least one circumferentially extending tube (27) having an air inlet intended for conveying cooling air, said tube (27) having a radially inner wall provided with cooling air discharge openings and a radially outer wall arranged axially opposite each other, an air inlet manifold (28), the inlet of the tube (27) opening into said manifold (28), characterized in that the tube (27) comprises at least one intermediate wall extending over a circumferential portion of the tube (27) from the air inlet, the intermediate wall being located radially between the radially inner wall and the radially outer wall, the radially inner wall and the intermediate wall forming a first air conveying duct, the radially outer wall and the intermediate wall forming a second air conveying duct extending circumferentially beyond the first air conveying duct, relative to the air inlet.
Public/Granted literature
- US11542833B2 Device for cooling an annular outer turbine casing Public/Granted day:2023-01-03
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