Invention Grant
- Patent Title: Holding device of a cooling tube for a turbojet casing
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Application No.: US14721555Application Date: 2015-05-26
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Publication No.: US10077677B2Publication Date: 2018-09-18
- Inventor: Sébastien Jean Laurent Prestel , Baptiste Marie Aubin Pierre Jouy
- Applicant: SNECMA
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Pillsbury Winthrop Shaw Pittman LLP
- Priority: FR1454790 20140527
- Main IPC: F01D25/12
- IPC: F01D25/12 ; F28F9/013 ; F01D25/14 ; F01D11/24 ; F02C7/18 ; F01D25/28 ; F28D1/047

Abstract:
A holding device of a cooling tube for a turbojet casing, the holding device including a first plate configured to be arranged in integral contact with a turbojet casing; a second plate, the first and second plates having a gap therebetween; a first spacer and the second spacer which are arranged between the first plate and the second plate and defining the gap between the first and second plates, the first and second spacers having a spacing therebetween suitable for passing the cooling tube.
Public/Granted literature
- US20150345328A1 HOLDING DEVICE OF A COOLING TUBE FOR A TURBOJET CASING Public/Granted day:2015-12-03
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