Invention Grant
- Patent Title: Turbine casing cooling device for a turbomachine
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Application No.: US17299702Application Date: 2019-12-03
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Publication No.: US11549394B2Publication Date: 2023-01-10
- Inventor: Julian Nicolas Girardeau , Maxime Aurélien Rotenberg
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Christensen O'Connor Johnson Kindness PLLC
- Priority: FR1872479 20181207
- International Application: PCT/FR2019/000198 WO 20191203
- International Announcement: WO2020/115374 WO 20200611
- Main IPC: F01D25/14
- IPC: F01D25/14 ; F01D9/06 ; F01D11/24

Abstract:
The disclosure provides devices for cooling a turbine casing for a turbomachine and methods of using the same. The devices extend around an axis (X) and include air-distribution means configured to take in air and convey it to the casing. The air-distribution means include a first ramp and a second ramp extending circumferentially about the axis (X), each ramp having air ejection orifices intended to be directed towards the casing in order to cool it The devices further include adjustment means capable of adjusting the flow rate of air ejected at the level of the first ramp with respect to the flow rate of air ejected at the level of the second ramp.
Public/Granted literature
- US20220018264A1 TURBINE CASING COOLING DEVICE FOR A TURBOMACHINE Public/Granted day:2022-01-20
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