Invention Grant
- Patent Title: Device for cooling a turbomachine housing
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Application No.: US17059738Application Date: 2019-05-28
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Publication No.: US11428111B2Publication Date: 2022-08-30
- Inventor: Benoit Guillaume Silet , Laurent Claude Descamps , Bertrand Guillaume Robin Pellaton
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Lathrop GPM LLP
- Priority: FR1854643 20180530
- International Application: PCT/FR2019/051258 WO 20190528
- International Announcement: WO2019/229377 WO 20191205
- Main IPC: F01D11/24
- IPC: F01D11/24 ; F01D25/12 ; F01D25/14 ; F02C7/18

Abstract:
A cooling device for an annular casing of a turbomachine includes a collector housing having ejection openings in a radially inner part of the collector housing facing the annular casing and at least two cooling tubes extending circumferentially from the collector housing and having election openings in a radially inner part of the tubes facing the annular casing. The collector housing having an air passage formed by a radial groove extending radially from a radially inner end of the collector housing to a radially outer end of the collector housing and an axial groove extending from a first axial end to a second axial end of the collector housing.
Public/Granted literature
- US20210222581A1 DEVICE FOR COOLING A TURBOMACHINE HOUSING Public/Granted day:2021-07-22
Information query
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