Invention Grant
- Patent Title: Gas turbine combustion chamber tile having effusion cooling holes including straight and offset sections
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Application No.: US14304367Application Date: 2014-06-13
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Publication No.: US09696036B2Publication Date: 2017-07-04
- Inventor: Carsten Clemen
- Applicant: Rolls-Royce Deutschland Ltd & Co KG
- Applicant Address: DE Blankenfel, De-Mahlow
- Assignee: ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Current Assignee: ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Current Assignee Address: DE Blankenfel, De-Mahlow
- Agency: Shuttleworth & Ingersoll, PLC
- Agent Timothy J. Klima
- Priority: DE102013214487 20130724
- Main IPC: F23R3/06
- IPC: F23R3/06 ; F23R3/00 ; F23R3/10
Abstract:
The present invention relates to a combustion chamber tile of a gas turbine with a plate-like basic element which is provided with at least one effusion cooling hole extending through the basic element from a surface of one side to the other side, with the effusion cooling hole being designed, from the one side of the basic element and beginning from an inlet opening, substantially at right angles to the surface over part of its length, wherein the effusion cooling hole inside the basic element has a straight section and is then provided with an offset section.
Public/Granted literature
- US20150027127A1 COMBUSTION CHAMBER TILE OF A GAS TURBINE Public/Granted day:2015-01-29
Information query
