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公开(公告)号：US11112117B2
公开(公告)日：2021-09-07
申请号：US16037389
申请日：2018-07-17
Applicant: General Electric Company
Inventor： Nayan Vinodbhai Patel , Ying Huang , Duane Douglas Thomsen
Abstract: A fuel nozzle for a combustor assembly of a heat engine is generally provided. The fuel nozzle defines a fuel nozzle centerline therethrough and a radial direction extended from the nozzle centerline. The fuel nozzle includes a first wall extended along the radial direction. The first wall defines a first cooling passage and a second cooling passage each extended therethrough. The first cooling passage is defined at a first acute angle relative to the nozzle centerline. The second cooling passage is defined at a second acute angle 90 degrees or less relative to the first acute angle.
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公开(公告)号：US20200025384A1
公开(公告)日：2020-01-23
申请号：US16037389
申请日：2018-07-17
Applicant: General Electric Company
Inventor： Nayan Vinodbhai Patel , Ying Huang , Duane Douglas Thomsen
Abstract: A fuel nozzle for a combustor assembly of a heat engine is generally provided. The fuel nozzle defines a fuel nozzle centerline therethrough and a radial direction extended from the nozzle centerline. The fuel nozzle includes a first wall extended along the radial direction. The first wall defines a first cooling passage and a second cooling passage each extended therethrough. The first cooling passage is defined at a first acute angle relative to the nozzle centerline. The second cooling passage is defined at a second acute angle 90 degrees or less relative to the first acute angle.
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