Invention Grant
- Patent Title: Diffuser part for a gas turbine
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Application No.: US15212791Application Date: 2016-07-18
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Publication No.: US10465708B2Publication Date: 2019-11-05
- Inventor: Carsten Clemen , Ivo Szarvasy
- Applicant: Rolls-Royce Deutschland Ltd & Co KG
- Applicant Address: DE Blankenfelde-Mahlow
- Assignee: ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Current Assignee: ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Current Assignee Address: DE Blankenfelde-Mahlow
- Agency: Shuttleworth & Ingersoll, PLC
- Agent Timothy J. Klima
- Priority: DE102015213625 20150720
- Main IPC: F04D29/54
- IPC: F04D29/54 ; F01D9/02 ; F01D25/26 ; F23R3/04 ; F04D29/32

Abstract:
A diffuser component for a gas turbine is provided, where a fluid flow in the direction of a combustion chamber of the gas turbine can be slowed down by the diffuser component, and a flow cross-section of the diffuser component, which is defined by a diffuser wall is widened to do so. The diffuser wall is at least locally braced, in that at least one stiffening element with a lattice-type structure is provided on the diffuser wall.
Public/Granted literature
- US20170023014A1 DIFFUSER PART FOR A GAS TURBINE Public/Granted day:2017-01-26
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