Invention Grant
- Patent Title: Gas engine component with cooling passages in wall
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Application No.: US15487406Application Date: 2017-04-13
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Publication No.: US10683762B2Publication Date: 2020-06-16
- Inventor: Mark O'Leary
- Applicant: Rolls-Royce North American Technologies, Inc.
- Applicant Address: US IN Indianapolis
- Assignee: Rolls-Royce North American Technologies Inc.
- Current Assignee: Rolls-Royce North American Technologies Inc.
- Current Assignee Address: US IN Indianapolis
- Agency: Brinks Gilson & Lione
- Main IPC: B22C9/10
- IPC: B22C9/10 ; F01D5/18

Abstract:
A ceramic structure may include a sacrificial ceramic core. The sacrificial ceramic core may include a ceramic body corresponding to a cooling cavity of a heat exchanger segment. The ceramic body may have an exterior surface that includes an outer surface and an inner surface interconnected to one another by at least a leading edge, a trailing edge, a tip facing edge and a base facing edge. The ceramic body may define a plurality of apertures extending between the outer surface and the inner surface. The ceramic body may include a trailing first pin and a leading first pin. The trailing first pin and the leading first pin may extend away from the inner surface. The leading first pin may be spaced away from the trailing first pin and in closer proximity to the leading edge than the trailing first pin.
Public/Granted literature
- US20180016914A1 GAS ENGINE COMPONENT WITH COOLING PASSAGES IN WALL AND METHOD OF MAKING THE SAME Public/Granted day:2018-01-18
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