Invention Grant
- Patent Title: Method of forming dust-removal holes for a turbine blade, and an associated ceramic core
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Application No.: US16077171Application Date: 2017-02-10
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Publication No.: US10537935B2Publication Date: 2020-01-21
- Inventor: Adrien Bernard Vincent Rollinger , Mirna Bechelany
- Applicant: SAFRAN
- Applicant Address: FR Paris
- Assignee: SAFRAN
- Current Assignee: SAFRAN
- Current Assignee Address: FR Paris
- Agency: Pillsbury Winthrop Shaw Pittman LLP
- Priority: FR1651134 20160212
- International Application: PCT/FR2017/050310 WO 20170210
- International Announcement: WO2017/137709 WO 20170817
- Main IPC: B22C9/10
- IPC: B22C9/10 ; F01D5/18

Abstract:
A ceramic core used for fabricating a hollow turbine blade for a turbine engine using the lost wax casting technique, the blade including calibrated dust-removal holes emanating from a top of at least one cavity and opening out into a bathtub of the blade, wherein each of the calibrated dust-removal holes is formed in a core portion of height that is determined to be sufficient to guarantee mechanical strength, the core portion including a through orifice of axis perpendicular to a longitudinal axis of the calibrated dust-removal hole and defining on either side of the through orifice firstly a core cylinder having a determined diameter corresponding to the dust-removal hole that is to be formed, and secondly a remaining core volume that is to be plugged after casting, such that the calibrated dust-removal hole is obtained without drilling and without using connection rods.
Public/Granted literature
- US20190022743A1 A METHOD OF FORMING DUST-REMOVAL HOLES FOR A TURBINE BLADE, AND AN ASSOCIATED CERAMIC CORE Public/Granted day:2019-01-24
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