发明名称 Gas turbine engines
摘要 In a by-pass gas turbine engine having a lobed type by-pass air and turbine exhaust mixer unit, the reheat gutters are arranged in the mixer in the turbine exhaust duct. The gutters extend radially and are substantially Y-shaped, each of the two legs of the Y extending radially along the sides of a mixer lobe.
申请公布号 US8061144(B1) 申请公布日期 2011.11.22
申请号 US19780886537 申请日期 1978.03.02
申请人 MAGUIRE ADDISON CHARLES;ROLLS-ROYCE LIMITED 发明人 MAGUIRE ADDISON CHARLES
分类号 F02K3/10;F02K1/38;F02K1/46 主分类号 F02K3/10
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