
民航发动机简CFM.ppt
23页COMAC PROPRIETARY INFORMATIONThe information contained in this document is COMAC proprietary information and is disclosed in confidence. It is the property of COMAC and shall not be used, disclosed to others or reproduced without the express written consent of COMAC.民民 航航 发发 动动 机机 第九部分第九部分黄国平 李传鹏NUAANUAAJET ENGINE22024/7/29CFM56@ CFMI1913 1913 法国法国 Rene lorinRene lorin设计发展制造组装联合公司共享GE、SNECMA所有资源各占50%份额一个项目管理一个客户界面产品支持市场NUAANUAAJET ENGINE32024/7/29CFM56@ CFMI •Snecma:- 低压系统 LP system- 安装 Installations- 齿轮箱 Gearbox- 控制与附件- Controls and accessories•GE:- 核心机 Core engine- 系统集成 System integration- 全权限数字电子控制系统FADEC/MEC systems整合资源整合资源研制高性能系列发动机研制高性能系列发动机NUAANUAAJET ENGINE42024/7/29CFM56@ CFMI(FADEC)3-D AeroProject TECH56• New fan• Six-stage compressor• New combustor• Advance turbineCFM56-2CFM56-7BCFM56-5B/PCFM56-5ACFM56-3CFM56-5C/PCFM56-5C-3TOWUpgradeNext-Generation UpgradesTechnologyFlow全权限数字电子控制全权限数字电子控制NUAANUAAJET ENGINE52024/7/29CFM56@ CFMI☆CFM56-2NUAANUAAJET ENGINE62024/7/29CFM56@ CFMI1913 1913 法国法国 Rene lorinRene lorin☆CFM56-3NUAANUAAJET ENGINE72024/7/29CFM56@ CFMI1913 1913 法国法国 Rene lorinRene lorin☆CFM56-3NUAANUAAJET ENGINE82024/7/29CFM56@ CFMI1913 1913 法国法国 Rene lorinRene lorin☆CFM56-5ANUAANUAAJET ENGINE92024/7/29CFM56@ CFMI1913 1913 法国法国 Rene lorinRene lorin☆CFM56-5B☆CFM56-5ANUAANUAAJET ENGINE102024/7/29CFM56@ CFMI1913 1913 法国法国 Rene lorinRene lorin☆CFM56-5BNUAANUAAJET ENGINE112024/7/29CFM56@ CFMI1913 1913 法国法国 Rene lorinRene lorin☆CFM56-5CNUAANUAAJET ENGINE122024/7/29CFM56@ CFMI1913 1913 法国法国 Rene lorinRene lorin☆CFM56-5C☆CFM56-7BNUAANUAAJET ENGINE132024/7/29CFM56@ CFMI1913 1913 法国法国 Rene lorinRene lorin☆CFM56-5C☆CFM56-7BNUAANUAAJET ENGINE142024/7/29CFM56@ CFMI1913 1913 法国法国 Rene lorinRene lorin☆CFM56-5C☆CFM56-7BNUAANUAAJET ENGINE152024/7/29CFM56@ CFMICFM56-7CFM56-7B18 (19,500 Ibs)CFM56-7B20 (20,600 Ibs)CFM56-7B22 (22,700 Ibs)B737-600CFM56-7B20 (20,600 lbs)CFM56-7B22 (22,700 lbs)CFM56-7B24 (24,200 lbs)B737-700 & 700 IGWCFM56-7B24 (24,200 lbs)CFM56-7B26 (26,300 lbs)CFM56-7B27 (27,300 lbs)B737-800CFM56-7B24 (24,200 lbs)CFM56-7B26 (26,300 lbs)CFM56-7B27 (27,300 lbs)B737-900CFM56-7B24 (24,200 lbs)C40ACFM56-7B26 (26,300; 27,300 lbs)737-BBJ, BBJ2, or COMBICFM56-7B27 (27,300 lbs)AWACCFM56-3CFM56-3B1 (18,500Ibs) (20,100Ibs)CFM56-3B2 (20,100 Ibs) (22,000Ibs) (22,100 Ibs)CFM56-3C (18,500Ibs) (20,100Ibs) (22,100 Ibs) (23,500 Ibs)B737-300 B737-500B737-300 B737-400B737-300 B737-400 B737-500B737 ClassicB737 NGNUAANUAAJET ENGINE162024/7/29CFM56@ CFMI-3 主要性能类型结构布局结构布局旋转方向旋转方向压气机压气机- 风扇- 增压级- 高压压气机燃烧室燃烧室涡轮涡轮- 高压涡轮- 低压涡轮重量重量尺寸尺寸- 长度- 高度涡扇双转子轴流顺时针 (从后往前看)单级3级9级环形燃烧室单级4级1949 kg (4297 Ibs)2.72m (98.16 ins)1.61m (66.38 ins)-7 Main FeaturesType of engineArrangementRotationCompressors- Fan- LP Compressor- HP CompressorCombustion chamberTurbines- HP Turbine- LP TurbineWeightOverall dimensions- Length- Height- WidthTurbo fanTwo spool axial flowClockwise (ALF)Single stageThree stagesNine stagesAnnual SAC(option DAC)Single stageFour stages5205 lbs2.51m (98.72 ins)1.83m (72 ins)2.12m (83.4 ins)NUAANUAAJET ENGINE172024/7/29CFM56@ CFMI☆CFM56-7B☆CFM56-3NUAANUAAJET ENGINE182024/7/29CFM56@ CFMI☆CFM56-7BNUAANUAAJET ENGINE192024/7/29CFM56@ CFMI☆CFM56-5B发动机主要装备与空客A319、A320、A321系列飞机上 包括了7个系列的发动机,编号从CFM56-5B1一直到CFM56-5B7-5B1-5B2-5B3-5B4-5B5-5B6-5B7A321 A321 A321 A320 A319 A319 A319 30,000lbs 31,000 lbs 33,000 lbs 27,000 lbs 22,000 lbs 23,500 lbs 27,000 lbs NUAANUAAJET ENGINE202024/7/29CFM56@ CFMI类型类型结构布局结构布局旋转方向旋转方向压气机压气机- 风扇风扇- 增压级增压级- 高压压气机高压压气机燃烧室燃烧室涡轮涡轮- 高压涡轮高压涡轮- 低压涡轮低压涡轮重量重量尺寸尺寸- 长度长度- 高度高度- 宽度宽度涡扇涡扇双转子轴流双转子轴流顺时针顺时针 (从后往前看从后往前看)1级级4级级9级级环形燃烧室环形燃烧室单级单级4级级2381 kg (5249 Ibs)2.94m2.14m 1.97mNUAANUAAJET ENGINE212024/7/29CFM56@ CFMI☆CFM56-5B☆CFM56-5BNUAANUAAJET ENGINE222024/7/29CFM56@ CFMI☆CFM56-5B☆CFM56-5BNUAANUAAJET ENGINE232024/7/29CFM56@ CFMI☆CFM56-5B☆CFM56-5B风扇模块核心机模块低压涡轮模块附件动力模块。
