发明名称 |
Double dome combustor with counter rotating toroidal vortices and dual radial fuel injection |
摘要 |
An annular combustion chamber for a gas turbine engine establishes two toroidal primary combustion zones. This provides high combustion capacity in a short combustor. Airflow is introduced in a manner to establish the flow pattern of the vortices, and the fuel is introduced in a manner avoiding destruction of the vortices.
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申请公布号 |
US5195315(A) |
申请公布日期 |
1993.03.23 |
申请号 |
US19910640757 |
申请日期 |
1991.01.14 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
HOLLADAY, THOMAS E. |
分类号 |
F23R3/02;F23R3/34;F23R3/42 |
主分类号 |
F23R3/02 |
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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