Device for securing a cooling tube to a turbomachine housing
FR3171682A1Pending Publication Date: 2026-07-31SAFRAN AIRCRAFT ENGINES SAS
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Patent Information
- Authority / Receiving Office
- FR · FR
- Patent Type
- Applications
- Current Assignee / Owner
- SAFRAN AIRCRAFT ENGINES SAS
- Filing Date
- 2025-01-28
- Publication Date
- 2026-07-31
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Abstract
This presentation concerns a device for retaining an air-jet cooling tube on a turbomachine housing. The device comprises: - an external support adapted to be positioned around a turbomachine housing, - a collar adapted to encircle a tube and attach it to the support, and - a graphite ring intended to be positioned around the tube, between the collar and the tube. The ring comprises two half-rings, each intended to encircle a portion of the tube. Figure for the abstract: Fig. 4
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