发明名称 |
Gas turbine engine fan bleed heat exchanger system |
摘要 |
<p>A heat exchanger system for a gas turbine engine includes: a fan (112) having at least two stages of rotating fan blades surrounded by a fan casing (114), the fan operable to produce a flow of pressurized air at a fan exit; at least one heat exchanger (116) having a first flowpath in fluid communication with the fan (112) at a location upstream of the fan exit; and a fluid system coupled to a second flowpath of the at least one heat exchanger (116). The first and second flowpaths are thermally coupled to each other.</p> |
申请公布号 |
EP2159383(A2) |
申请公布日期 |
2010.03.03 |
申请号 |
EP20090167468 |
申请日期 |
2009.08.07 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
COFFINBERRY, GEORGE ALBERT |
分类号 |
F01D25/12;F01D25/18;F02C7/14;F02C7/224;F02K3/06 |
主分类号 |
F01D25/12 |
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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