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公开(公告)号：US20250067434A1
公开(公告)日：2025-02-27
申请号：US18804670
申请日：2024-08-14
Applicant: ROLLS-ROYCE PLC
Inventor： Marcin Damian DUTKA
Abstract: A tile for a gas turbine engine combustor. The tile has a base that has a hot-side surface, a cold-side surface, a first circumferential extremity, a second circumferential extremity and a local radial axis. The tile also has a plurality of cooling channels that have inlets on the cold-side surface and outlets on the hot-side surface, and one or more rail structure attached to the cold-side surface of the base.
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