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公开(公告)号:US20210003281A1
公开(公告)日:2021-01-07
申请号:US17029587
申请日:2020-09-23
Applicant: GENERAL ELECTRIC COMPANY
Abstract: A method for regulating jet wakes in a combustor including: directing compressed fluid into a passageway between a casing and a combustor liner; directing a combustion gas along a combustion zone; discharging a first portion of compressed fluid from the passageway into the combustion zone via a first through-hole which is disposed on a section of a combustor panel in a first circumferential row; and discharging a second portion of the compressed fluid from the passageway into the combustion zone via second through-holes, wherein the second through-holes are disposed on a section of the panel, spaced apart axially and circumferentially, and adjacent to the first through-hole, wherein the second through-holes include a first set of through-holes and a second set of through-holes, the first set of through-holes in a second row and the second set of through-holes in a third row, wherein the second and third rows extend circumferentially.
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公开(公告)号:US20200049349A1
公开(公告)日:2020-02-13
申请号:US16057249
申请日:2018-08-07
Applicant: General Electric Company
Inventor: Mayank Krisna Amble , Gurunath Gandikota , Perumallu Vukanti , Ravi Chandra , Karthikeyan Sampath
Abstract: The present disclosure is directed to a combustor assembly for a gas turbine engine. The combustor assembly includes a liner defining a combustion chamber therewithin and a pressure plenum surrounding the liner. The liner defines an opening and includes a walled chute disposed at least partially through the opening. A plurality of flow openings is defined through the walled chute.
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