发明名称 КОЛЬЦЕВАЯ КАМЕРА СГОРАНИЯ ГАЗОТУРБИННОГО ДВИГАТЕЛЯ
摘要 FIELD: gas-turbine engine engineering. ^ SUBSTANCE: ring combustion chamber comprises fire tube and vortex burners arranged over periphery of its face and made of fuel-air scroll and air swirlers with outlet conical branch pipe having cylindrical section. The shell is secured to the face coaxially to each branch pipe defining a ring space. The outer side of the end cylindrical section or inner side of the shell located above it is provided with longitudinal ribs distributed uniformly over periphery and defining insulated passages. The through openings connected with the ring space are made in the face of the fire tube under the shell. ^ EFFECT: enhanced reliability and expanded functional capabilities. ^ 2 cl, 2 dwg
申请公布号 RU2004137975(A) 申请公布日期 2006.06.10
申请号 RU20040137975 申请日期 2004.12.27
申请人 Акционерное общество открытого типа Авиамоторный научно-технический комплекс "СОЮЗ" (RU) 发明人 Иванов Петр Глебович (RU)
分类号 F23R3/28 主分类号 F23R3/28
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