Integrated Front Panel for a Burner
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United States of America Patent
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Issued Date -
May 13, 2021
app pub date -
Nov 12, 2019
filing date -
Nov 12, 2019
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Abstract
A turbomachine includes a compressor and a turbine with a burner and a combustor between the compressor and the turbine. The burner is downstream of the compressor and upstream of the turbine. The burner is connected to the combustor at a front panel of the burner. The front panel includes a frame, a rim extending around a central aperture within the frame, and a seal segment. The frame, the rim, and the seal segment are all integrally formed as a single unitary body.
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