Gas turbine combustor and gas turbine
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United States of America Patent
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-
May 20, 1997
Grant Date -
N/A
app pub date -
Dec 13, 1994
filing date -
Dec 15, 1993
priority date (Note) -
In Force
status (Latency Note)
Importance
Abstract
A gas turbine combustor is provides with a stabilizer at a downstream side of a premixing device for premixing and supplying fuel and air into a combustion chamber. The stabilizer has a cylindrical part extending axially from an upstream end thereof to a downstream end and a stabilizing part at the downstream end of the cylindrical part for stabilizing a flame, and the stabilizer is mounted on an inside of the combustor by a plurality of members arranged annularly and secured to the inside of the combustor at their ends, each of the members having a part slidably inserted in an opening of the cylindrical part so as to restrict the stabilizer to move axially while allowing deformation of the stabilizer and another part supporting the upstream end of the cylindrical part so as to restrict radial movement of the stabilizer.
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