发明名称 Gas turbine engine bleed air power assist system and method
摘要 <p>A bleed air power assist system is coupled to a gas turbine engine (100) that includes a high pressure turbine (126), a low pressure turbine (128), and an electrical generator (138) driven by the high pressure turbine (126). The bleed air power assist system selectively bleeds air discharged from the high pressure turbine (126) and supplies it to an air turbine (156) that is also coupled to the generator (138). Thus, the system selectively reduces the power extracted from the high pressure turbine (126). This, coupled with the bleed air that is diverted from the low pressure turbine (128), allows the low pressure spool (136) to run at lower speeds when high engine thrust is not needed or desired, but when the generator (138) is still needed to supply high electrical loads.</p>
申请公布号 EP1617053(A2) 申请公布日期 2006.01.18
申请号 EP20050254467 申请日期 2005.07.18
申请人 HONEYWELL INTERNATIONAL INC. 发明人 LAIDLAW, MITCHELL J.;LIBERA, ANTHONY C.;MAHONEY, TIMOTHY D.
分类号 F02C7/32;F01D15/10;F02C3/10;F02C9/18 主分类号 F02C7/32
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