发明名称 |
Method and apparatus for enhancing heat transfer in a combustor liner for a gas turbine |
摘要 |
A combustor liner is provided on its backside cooling surface with a braze alloy coating and cooling enhancement material, preferably metallic particles to enhance the heat transfer between the liner and the cooling medium. The surface area of the backside coated area is increased substantially by the coating and particles in relation to the uncoated surface areas. Consequently, the life of the liner is extended.
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申请公布号 |
US2002152755(A1) |
申请公布日期 |
2002.10.24 |
申请号 |
US20020166748 |
申请日期 |
2002.06.12 |
申请人 |
JOHNSON ROBERT ALAN;LOPRINZO ANTHONY JOSEPH;LEE CHING-PANG;ABUAF NESIM;HASZ WAYNE CHARLES;MORTON HARMON LINDSAY |
发明人 |
JOHNSON ROBERT ALAN;LOPRINZO ANTHONY JOSEPH;LEE CHING-PANG;ABUAF NESIM;HASZ WAYNE CHARLES;MORTON HARMON LINDSAY |
分类号 |
F23R3/00;(IPC1-7):F23R3/42 |
主分类号 |
F23R3/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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