发明名称 TURBOJET ENGINE REHEAT UNIT
摘要 FIELD: mechanical engineering; turbojet engines. ^ SUBSTANCE: reheat unit of turbojet engine contains prechamber and central body arranged one after another indirection of flow. Prechamber is furnished with V-shaped flame stabilizer which burners are arranged, and stabilizer proper is made up of two ring segments arranged at a distance not less than maximum thickness of cross section of central body. Said central body contains fixed housing with flat surfaces from both sides and flat deflecting panels in contact with flat surfaces, thickened inlet part rounded off in cross section and wedge-like outlet part. Wedge-like outlet part and contacting flat surfaces of housing and deflecting panels are coated with radio absorbing material. Flat panels and their hinge joints connecting them with central body housing are made hollow, and they are driven from both sides through hollow springs. Fixed hollow cylindrical rod is arranged inside hollow of each panel. Outer surface of said rod is slide-fitted with inner surfaces of hollow hinge joint. Ends of each hollow cylindrical rod pass inside hollow springs, pylons and are connected with cooling air supply pipelines through side holes in reheat unit wall. Hinge joints and cylindrical rods are provided with two rows of through holes arranged at angle relative to each other so that in nondeflected initial position of panels, holes in rods and hinge joints register in front rows in direction of flow and do not coincide in rear rows, and vise versa, in deflected positions of panels, holes coincide in rear rows and do not coincide in front rows. Inner space of each flat panel is connected at one side through holes with inner space of reheat unit, and at other side, with panels deflected, is connected through registered holes in rod and hinge joint, with inner space of cylindrical rod. Thin-walled streamlined screen is made lengthwise outer surface of hinge joint of each panel. Said screen forms inner space between screen and outer surface of hinge joint. Said space is connected inner space of cylindrical rod through registered holes of front rows of rod and hinge joint when panels are in not deflected initial position, and opposite edges of each flat panel in direction from hinge joint is made in form of ellipse, and at deflection of panels, projection of both panels onto plane of cross section reheat unit is screen in form of circle. ^ EFFECT: improved reliability of reheat unit, reduced level of infra-red radiation in rear semi-sphere of engine. ^ 8 dwg
申请公布号 RU2300655(C1) 申请公布日期 2007.06.10
申请号 RU20050138929 申请日期 2005.12.15
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO AVIAMOTORNYJ NAUCHNO-TEKHNICHESKIJ KOMPLEKS "SOJUZ" 发明人 BELOUSOV VIKTOR ALEKSEEVICH;VOLYNKIN SERGEJ KONSTANTINOVICH;DEMKIN NIKOLAJ BORISOVICH;SHUVALOV KIRILL SERGEEVICH;SHEPELEVA NINA GEORGIEVNA;JAKOVLEV NIKOLAJ NIKOLAEVICH
分类号 F02K3/105 主分类号 F02K3/105
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