发明名称 |
Hot spike mixer |
摘要 |
A mixer at the exit opening of a high performance jet engine to prevent premature migration of the core flow into the duct stream thereby operating to eliminate hot streaks in the augmentor and nozzle areas during augmentation. The mixer consists of a concave fillet positioned on the pressure side of the turbine exit guide vane and exhaust case at the trailing edge.
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申请公布号 |
US4305248(A) |
申请公布日期 |
1981.12.15 |
申请号 |
US19790082354 |
申请日期 |
1979.10.05 |
申请人 |
THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE AIR FORCE |
发明人 |
WRIGHT, DAVID L. |
分类号 |
F02K1/38;(IPC1-7):F02K3/08 |
主分类号 |
F02K1/38 |
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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