发明名称 A gas turbine engine
摘要 Within an intake for a gas turbine engine provision is provided through stator vanes 25, 45 in the stator whereby back pressure from a necessary obstruction 34, 46 can be utilised to balance forward pressure variations caused by intake droop or crosswinds in order to reduce those forward pressure detriments for more efficient engine operation according to a desired objective regime. Typically the flow through the intake 20 is analysed and then an appropriate positioning of the stator vanes 25, 45 determined in order to provide approximate balance between the forward pressures and back pressures. Normally, a combination of camber variation of stator vanes 45 a and stagger variation of stator vanes 45 b are utilised in order to achieve a desired momentum balance around the circumference of the intake 20. It will be understood that both the forward pressures and the back pressures are differentially variable about the circumference such that one opposes the other.
申请公布号 GB0314123(D0) 申请公布日期 2003.07.23
申请号 GB20030014123 申请日期 2003.06.18
申请人 ROLLS-ROYCE PLC 发明人
分类号 F01D5/10;F01D5/14;F01D9/04;F02C7/00;F02C7/04;F04D29/54 主分类号 F01D5/10
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