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公开(公告)号：US20210088214A1
公开(公告)日：2021-03-25
申请号：US17110099
申请日：2020-12-02
申请人： GTL Company
发明人： Paul Gloyer , Eric Jacob , Jonathan French , Joshua Batterson , Tina Rice , Gary Flandro
摘要： A method comprising performing simulations to determine energy transfer between the bulk fluid motion of gases through a combustion chamber and resonant acoustic modes of the combustion chamber using a simulation model. The method also comprises configuring one or more combustion chamber parameters for the simulation model to shape the resonant acoustic modes to diminish coupling between the resonant acoustic modes and driving mechanisms at a head portion of the combustion chamber and to enhance coupling between the resonant acoustic modes and damping mechanisms at an aft portion of the combustion chamber. The method further comprises determining whether the combustion chamber meets a predetermined performance level in response to determining that the combustion chamber meets a predetermined combustion stability level.
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公开(公告)号：US20180106480A1
公开(公告)日：2018-04-19
申请号：US15729591
申请日：2017-10-10
申请人： GTL Company
发明人： Paul Gloyer , Eric Jacob , Jonathan French , Joshua Batterson , Tina Rice , Gary Flandro
CPC分类号： F23R3/18 , F02K9/52 , F02K9/62 , F02K9/97 , F05D2260/81 , F05D2260/964 , F23R3/002 , F23R2900/00018 , G06F17/5009 , G06F17/5095 , G06F2217/16
摘要： A method comprising performing simulations to determine energy transfer between bulk fluid motion of gases through a combustion chamber and resonant acoustic modes of the combustion chamber using a simulation model. The method also comprises configuring one or more combustion chamber parameters for the simulation model to shape the resonant acoustic modes to diminish coupling between the resonant acoustic modes and driving mechanisms at a head portion of the combustion chamber and to enhance coupling between the resonant acoustic modes and damping mechanisms at an aft portion of the combustion chamber. The method further comprises determining whether the combustion chamber meets a predetermined performance level in response to determining that the combustion chamber meets a predetermined combustion stability level.
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公开(公告)号：US12086517B2
公开(公告)日：2024-09-10
申请号：US17110099
申请日：2020-12-02
申请人： GTL Company
发明人： Paul Gloyer , Eric Jacob , Jonathan French , Joshua Batterson , Tina Rice , Gary Flandro
IPC分类号： G06F30/28 , F02K9/52 , F02K9/62 , F02K9/64 , F02K9/97 , F23R3/00 , F23R3/18 , G06F30/15 , G06F30/20 , G06F111/10
CPC分类号： G06F30/28 , F02K9/52 , F02K9/62 , F02K9/97 , F23R3/002 , F23R3/18 , G06F30/15 , G06F30/20 , F02K9/64 , F05D2260/81 , F05D2260/964 , F23R2900/00018 , G06F2111/10
摘要： A method comprising performing simulations to determine energy transfer between the bulk fluid motion of gases through a combustion chamber and resonant acoustic modes of the combustion chamber using a simulation model. The method also comprises configuring one or more combustion chamber parameters for the simulation model to shape the resonant acoustic modes to diminish coupling between the resonant acoustic modes and driving mechanisms at a head portion of the combustion chamber and to enhance coupling between the resonant acoustic modes and damping mechanisms at an aft portion of the combustion chamber. The method further comprises determining whether the combustion chamber meets a predetermined performance level in response to determining that the combustion chamber meets a predetermined combustion stability level.
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