首页> 外国专利> TURBOFAN ENGINE WITH COMPACT SYSTEM OF AIR TAKEOFF FROM BOOSTER COMPRESSOR

TURBOFAN ENGINE WITH COMPACT SYSTEM OF AIR TAKEOFF FROM BOOSTER COMPRESSOR

机译:涡轮增压发动机,采用增压压缩机的紧凑型进气系统

摘要

FIELD: engines and pumps.;SUBSTANCE: turbofan engine (10) comprises a fan (14), attached to a frame (32) of fan fixation inside a fan body (30). The booster compressor (16) is attached to the fan (14) inside a flow separator (34). The body (30) surrounds the fan (14) and the separator (34) and is located at a distance from the separator (34) to form an outer contour (36) between them. The frame of fan fixation (32) is located behind the booster compressor (16) and includes a row of struts (38), passing along the radius outside via an outer circuit (36) from a circular bushing (40), arranged between the booster compressor (16) and the high pressure compressor (18). The system (54) of air takeoff from booster compressor is located inside the separator (34) and includes an inlet channel (58) of the takeoff system, arranged between the booster compressor (16) and the bushing (40), and an outlet channel (60) of the takeoff system, arranged at the rear end of the separator (34) in front of struts (38).;EFFECT: increased efficiency ratio.;7 cl, 2 dwg
机译:领域:涡轮风扇发动机(10)包括风扇(14),该风扇(14)附接到风扇主体(30)内部的风扇固定框架(32)。增压压缩机(16)安装在分流器(34)内部的风扇(14)上。主体(30)围绕风扇(14)和分离器(34),并且位于与分离器(34)相距一定距离处,以在它们之间形成外轮廓(36)。风扇固定框架(32)位于增压压缩机(16)的后方,并包括一排支柱(38),该支柱(38)从外部穿过环形衬套(40),通过外部回路(36)沿半径范围从外部穿过,布置在两个之间。增压压缩机(16)和高压压缩机(18)。从增压压缩机排出的空气的系统(54)位于分离器(34)的内部,并且包括布置在增压压缩机(16)和衬套(40)之间的排出系统的入口通道(58)和出口。起飞系统的通道(60),布置在撑杆(38)前面的分离器(34)的后端。

著录项

  • 公开/公告号RU2433312C2

    专利类型

  • 公开/公告日2011-11-10

    原文格式PDF

  • 申请/专利权人 DZHENERAL EHLEKTRIK KOMPANI;

    申请/专利号RU20060145808

  • 发明设计人 MONIZ TOMAS ORI (US);

    申请日2006-12-21

  • 分类号F04D27/02;F02K3/075;F02C9/18;F01D17/10;

  • 国家 RU

  • 入库时间 2022-08-21 17:48:09

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