Device for improved air and fuel distribution to a combustor [electronic resource].

Published: Washington, D.C. : United States. Dept. of Energy, 2016.
Oak Ridge, Tenn. : Distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy
Additional Creators: United States. Department of Energy and United States. Department of Energy. Office of Scientific and Technical Information

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www.osti.gov

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Summary

A flow conditioning device (30, 50, 70, 100, 150) for a can annular gas turbine engine, including a plurality of flow elements (32, 34, 52, 54, 72, 74, 102) disposed in a compressed air flow path (42, 60, 80, 114, 122) leading to a combustor (12), configured such that relative adjustment of at least one flow directing element (32, 52, 72, 110) with respect to an adjacent flow directing element (34, 54, 74, 112, 120) during operation of the gas turbine engine is effective to adjust a level of choking of the compressed air flow path (42, 60, 80, 114, 122).

Report Numbers

E 1.99:9,353,949
9,353,949

Subject(s)

Note

Published through SciTech Connect.
05/31/2016.
"9,353,949"
"13/448,458"
Walter R. Laster; Reinhard Schilp.
SIEMENS ENERGY, INC., Orlando, FL (United States)

Funding Information

FC26-05NT42644

View MARC record | catkey: 23491867