发明名称 ADJUSTABLE FLAT NOZZLE FOR GAS TURBINE ENGINE
摘要 FIELD: mechanical engineering; gas turbine engines. SUBSTANCE: proposed adjustable flat nozzle has body, turnable flap and movable scoop member. Axis of rotation of turnable flap is displaced relative to axis of rotation of scoop member towards body outlet part. Outline of inner surface of scoop member inlet part is made arc-shaped, with constant radius of circumference. Outline of inner surface of scoop member outlet part is made diverging. Conjugate point of outlines of inner surfaces of inlet and outlet parts is arranged at angle alpha = 64-65°. Conjugate point of inner outline and cut of scoop member is arranged at angle beta = 73-74° to inlet edge of scoop member relative to axis of rotation of scoop member. Outline of inner surface of turnable flap is made converging-diverging, with point of inflection of outlines displaced towards flap outlet part. EFFECT: improved reliability of nozzle owing to simplification of design, reduced infrared visibility, improved efficiency of engine. 3 dwg
申请公布号 RU2193680(C2) 申请公布日期 2002.11.27
申请号 RU20010100146 申请日期 2001.01.03
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "AVIADVIGATEL'" 发明人 SHKLJAEV I.V.;POZHARINSKIJ A.A.
分类号 F02K1/12 主分类号 F02K1/12
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