发明名称 LANCE INJECTOR FOR INJECTING FUEL OIL INTO A GAS TURBINE COMBUSTION CHAMBER
摘要 A lance injector includes: an outer tubular body (15) and an inner tubular body (16), which extend along a common axis (A) and define a first fluid line (22) in a gap between the outer tubular body (15) and the inner tubular body (16), and a second fluid line (23) in the inner tubular body (16); a nozzle (18) connected fluidically to the first fluid line (22) and the second fluid line (23), at respective first ends (15a, 16a) of the outer (15) and inner (16) tubular bodies; and constraint members (17, 27, 30) configured so as to prevent the relative axial slide between the outer tubular body (15) and the inner tubular body (16) in a locking region at the respective first ends (15a, 16a), and such to permit the relative axial slide between the outer tubular body (15) and the inner tubular body (16) as effect of expansion elsewhere.
申请公布号 EP3049722(A1) 申请公布日期 2016.08.03
申请号 EP20140796263 申请日期 2014.09.26
申请人 ANSALDO ENERGIA S.P.A. 发明人 PASTORINO, PIERPAOLO;GALELLA, ROCCO
分类号 F23D11/28;F23D11/10 主分类号 F23D11/28
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