细看F-16 的发动机F110

来源:百度文库 编辑:超级军网 时间:2024/04/30 04:44:06
GE Aircraft Engines report that their development F110-GE-132 jet engine for the F-16C/D is undergoing an exhaustive series of ground tests in readiness of flight testing next year. The F110 engine is derived from the F110-GE-100 and F110-GE-129 engines, which power the majority of F-16C/Ds world-wide.

Capable of producing a maximum of 32,500 pounds (144 kN) of thrust, the F110-GE-132 is said to have 50% more life than the GE-129 variant. Engine life can be further improved by limiting thrust levels to 29,000 (129 kN) - the thrust rating of GE-129 engines.

The F110-GE-132 engine has already completed performance baseline testing and altitude tests; endurance testing starts this summer. The new engine is based on proven technologies derived from GE Aircraft Engines' experience and development of the F118 engine (B-2 bomber), F414 engine (F/A-18E/F), F120 engine (JSF) and the F404.

The UAE Air Force has selected the F110-GE-132 for its eighty F-16 Block 60 aircraft. Following flight testing in 2002 and 2003, first production engines are due to be delivered in 2003 to support the UAE's aircraft delivery schedule from 2004.

Further orders for F110 engines include that of the Air Force of Chile, which has selected the F110-GE-129 to power its new fleet of F-16C/D aircraft. Elsewhere, the F110 engine family is used to power F-16s for the USAF, Bahrain, Egypt, Greece, Israel, Turkey, UAE, and Japan's F-2 fighter.GE Aircraft Engines report that their development F110-GE-132 jet engine for the F-16C/D is undergoing an exhaustive series of ground tests in readiness of flight testing next year. The F110 engine is derived from the F110-GE-100 and F110-GE-129 engines, which power the majority of F-16C/Ds world-wide.

Capable of producing a maximum of 32,500 pounds (144 kN) of thrust, the F110-GE-132 is said to have 50% more life than the GE-129 variant. Engine life can be further improved by limiting thrust levels to 29,000 (129 kN) - the thrust rating of GE-129 engines.

The F110-GE-132 engine has already completed performance baseline testing and altitude tests; endurance testing starts this summer. The new engine is based on proven technologies derived from GE Aircraft Engines' experience and development of the F118 engine (B-2 bomber), F414 engine (F/A-18E/F), F120 engine (JSF) and the F404.

The UAE Air Force has selected the F110-GE-132 for its eighty F-16 Block 60 aircraft. Following flight testing in 2002 and 2003, first production engines are due to be delivered in 2003 to support the UAE's aircraft delivery schedule from 2004.

Further orders for F110 engines include that of the Air Force of Chile, which has selected the F110-GE-129 to power its new fleet of F-16C/D aircraft. Elsewhere, the F110 engine family is used to power F-16s for the USAF, Bahrain, Egypt, Greece, Israel, Turkey, UAE, and Japan's F-2 fighter.
Engine F110 CUTAWAY
Engine F110 Cutaway
车间好破啊, 这个
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通过这幅图我们可以了解到发动机采用的是3级轴流式风扇,风扇转子叶片材料为钛合金,位于后面的是安装在机匣内的风扇定子整流叶片
发动机风扇定子采用水平对开式机匣,转子和整流叶片可单独更换。风扇直径970mm,压比3.2(所谓压比就是空气被压缩后的压力,与压缩前的压力之比值,愈大者性能愈好。压气机的压比通常在10左右)。风扇和压气机是航空发动机的重要部件,其性能的好坏直接影响整个发动机的工作效率。
压气机采用9级轴流式高压压气机,头3级材料为钛合金(依图可以观察到颜色偏黄),后6级为A286钢。零级和头3级整流叶片可调,转子为盘鼓式。
压气机定子为水平对开式机匣,前段为钛合金,后段为钢(上图显示的是后段部分)。设有孔探仪窥孔,用以观察转子和其他部件。

在这里要说明的是压气机是由定子页片与转子页片交错组成,一对定子页片与转子页片称为一级,定子叶片固定在机匣内,转子叶片由转子轴与涡轮相连。目前的涡喷或涡扇发动机一般为8-12级压气机,级数越多越往后压力越大。
高压涡轮为单级轴流式。高负荷气冷叶片,用冲击和气膜冷却。
低压涡轮是2级轴流式,2级转子叶片均可单独更换,第2级导向器叶片可分段更换。
加力燃烧室是V形加径向混合型火焰稳定器,尾喷管是收敛-扩张可调喷管控制系统
尾喷管收敛-扩张型。喷口面积由液压作动筒和作动环控制,主、副喷管的调节板分三段铰接,在凸轮和滚柱上移动,以调节喷口面积。喷管外壳材料为焊接的钛合金
涡轮风扇发动机由风扇、压气机、燃烧室、驱动压气机的高压涡轮、驱动风扇的低压涡轮和排气系统组成。其中压气机、燃烧室和高压涡轮三部分统称为核心机,由核心机排出的燃气中的可用能量,一部分传给低压涡轮用以驱动风扇,余下的部分在喷管中用于加速排出的燃气。

风扇转子实际上是 1级或几级叶片较长的压气机,空气流过风扇后,一部分流入核心机称为内涵气流由喷管高速排出产生推力,另一部分围绕核心机的外围流过,称为外涵气流,也产生推力。

这种有内外二个涵道的涡轮风扇发动机又称为内外涵发动机。流经外涵和内涵的空气流量之比称为涵道比或流量比,战斗机通常采用迎风面积小适宜于高速飞行的小涵道比、带加力燃烧室的涡轮风扇发动机。
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这个帖子可以小小地顶一下
很好的帖子,真的不愧为工业之花,顶一个
拆的这么碎,你会装上吗?;funk
原帖由 哦皑皑系 于 2008-1-20 10:07 发表
拆的这么碎,你会装上吗?;funk

I am not a assemblagist but I can take pics
还是LZ厉害啊~~顶一个~
原帖由 sophie_anny 于 2008-1-20 11:16 发表
I am not a assemblagist but I can take pics


你拍的照片?Gary Brossett
http://www.enginehistory.org/brossett_galleries.htm
http://www.enginehistory.org/f110ge100.htm
原帖由 aliasmaya 于 2008-1-20 15:46 发表


你拍的照片?Gary Brossett
http://www.enginehistory.org/brossett_galleries.htm
http://www.enginehistory.org/f110ge100.htm

Oh! take means "get".
有MAYA领导的贴必是精品:D
大饱眼福!谢谢楼主!
要顶一下,知识性强。
想上去咬一口的说
技术贴
技术贴
工程进行中,希望多多支持... ...

Engine 04.jpg
Engine 05.jpg
Engine 07_缩小大小.jpg
Engine 09.jpg
Engine 11.jpg
哇,挖坟啊。
好东西啊,我们要是有的话。。。
嗯  不赖 坐等lz更新 想看看核心机实物剖视图
我敢说目前装在T-50上的发动机肯定还不如 F110-GE-132 和F100-PW-229好,即将首飞的丝带的发动机肯定也不如毛子延寿改进型苏27SM用的31FM1,这就是毛子和TG的怀具之处。。。
挺好的帖子,看着很明白,是哪个博物馆里的吧。
楼主很牛逼,支持
TG什么时候能搞出这个级别的发动机啊 {:lei:}
en, 看着也没多难,就是得找个手艺好一点的钣金工而已。:D
工业之花
supermarrang 发表于 2010-11-30 20:35


    这坟挖的太有技术含量了!
楼主厉害这都能找到!!!
TG现在的发动机有这个水平吗?