发明名称 |
METHODS AND APPARATUS FOR OPERATING GAS TURBINE ENGINES |
摘要 |
A method enables a gas turbine engine multi-domed combustor including an outer liner and an inner liner that define a combustion chamber therebetween to be assembled. The method comprises coupling a first dome including a heat shield that includes an annular endbody that extends a first distance axially from the heat shield to the combustor outer liner, and coupling a second dome including a heat shield that includes an annular endbody that extends a second distance axially from the heat shield to the first dome, such that the second dome is radially aligned with respect to the first dome, and wherein the second dome second distance is less than the first dome first distance
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申请公布号 |
US2004040307(A1) |
申请公布日期 |
2004.03.04 |
申请号 |
US20020233356 |
申请日期 |
2002.08.30 |
申请人 |
DIMOV MINA;ANGEL PAUL R.;MARAKOVITS STEVEN;BROWN DANIEL DALE |
发明人 |
DIMOV MINA;ANGEL PAUL R.;MARAKOVITS STEVEN;BROWN DANIEL DALE |
分类号 |
F23R3/12;F23R3/00;F23R3/28;F23R3/34;F23R3/50;F23R3/52;(IPC1-7):F23R3/14 |
主分类号 |
F23R3/12 |
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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