发明名称 AIRCRAFT ENGINE AND METHOD OF ITS OPERATION
摘要 FIELD: engines and pumps.SUBSTANCE: engine has front and rear air screws with variable-rake. In cruising flight, engine runs at constant air screw tip peripheral speed. In, at least, liftoff, climb or approach, blade tip peripheral speed exceeds that in cruising speed. Blades are closed from their rake in cruising flight to that in approach. Front air screw 23 has, at least, nine blades (Nf=9) and diameter Df. Rear air screw 24 has maximum number of blades Nr=Nf minus, at least, three. Front and rear air screws 23, 24 are separated by axial clearance x. Ratio x/Df varies from 0.15 to 0.4. Engine may be gas turbine, diesel or gasoline engine, or that running on fuel cells.EFFECT: reduced noise.11 cl, 5 dwg
申请公布号 RU2472942(C2) 申请公布日期 2013.01.20
申请号 RU20090133692 申请日期 2008.02.06
申请人 ROLLS-ROJS PI-EHL-SI, VELIKOBRITANIJA 发明人 PARRI EHNTONI BRAJN;KHOVART NIKOLAS;TEHJLOR MARK DAVID
分类号 F01D1/24;B64C11/48;B64C11/50;F02C9/58;F02K3/072 主分类号 F01D1/24
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