2010年巴基斯坦将获得F100-PW-229 EEP型发动机

PW称，EEP的设计检修间隔达6000TAC，大概3000飞行小时等级...
F100-PW-229
June 13,2008

Reliable, High Performance for the F-15 Eagle and the F-16 Fighting Falcon

A Proud Tradition of Dependable Performance: 1974 marked the operational introduction of the first Pratt & Whitney F100 engine model, the F100-PW-100, in the F-15 Eagle air superiority fighter.  Since then, various models of the F100 have been selected by the U.S. Air Force, Navy, Air Force Reserve, Air National Guard, and 21 allied nations for all versions of the F-15 and the F-16 Fighting Falcon multi-role lightweight fighter.  F100 engines power 100 percent of U.S. Air Force F-15 aircraft and 62 percent of F-16 fighters worldwide.  Over 7200 F100 engines have been produced and have accumulated more than 21,000,000 flight hours under the most rigorous operational environments found around the world.  The F100 record of dependability, performance and safety has set a worldwide standard for fighter engine excellence.  The F100-PW-229 is an improved, high-thrust evolution of the F100-PW-220, Pratt & Whitney's electronically-controlled high-performance fighter engine that entered production in the mid-1980’s for F-15 and F-16 fighters.  Pratt & Whitney’s F100-PW-229 Increased Performance Engine (IPE), already the most widely used advanced technology fighter engine in the world, continues to capture market share and to boost weapon system capabilities with proven enhancement packages and growth options.

An Unmatched Safety Record: The most significant accomplishment of the F100 family is its extraordinary flight safety record.  The current safety record of the F100 engine family represents the progress achieved using Pratt & Whitney’s advanced system safety program approach.  Identified refinements designed to enhance the maturity of the F100-PW-229 are expected to continue to sustain long-term safety rates significantly better than those of the F100-PW-220; the safest fighter engine in U.S. Air Force history.  The F100-PW-229 engine has the best safety record of any IPE engine.

Full Production and Operational Maturity: The F100-PW-229 is the latest production model in the F100 family of fighter aircraft engines.  It incorporates proven technological innovations and generates over 29,100 pounds of thrust.  It has been specifically designed to operate at full performance in all existing and future F-15 or F-16 aircraft.  It provides a thrust-to-weight ratio close to eight-to-one and features a state-of-the-art digital electronic engine control (DEEC) system with enhanced, real-time engine monitoring and fault isolation capability.  The F100-PW-229 entered production in December 1989 and began full operational service in September 1991.  In 1994, the Republic of Korea became the first U.S. ally to go operational with the F100-PW-229 in its F-16C/Ds.  The F100-PW-229 engine is clearly the engine of choice with over 1050 engines in service with the U.S., Korea, Saudi Arabia, Singapore, Polish, Greece and Israel air forces.  The F100-PW-229 engine powers over 71 percent of the IPE market for international F-15 and F-16 aircraft.

Proven Mission Sustainment: The F100-PW-229 entered service in the most demanding operational and climatic environment in the U.S. Air Force; the F-15E air-to-ground mission at Elmendorf Air Force Base, Alaska.  Due to its evolutionary derivation from earlier F100 models, the F100-PW-229 entered this service with a full-service hot section life of 4300 thermal cycles (total equivalent cycles or TAC) or over seven years between required depot visits.  The F100-PW-229 incorporates a number of improvements including the insertion of the latest technologies into the high pressure turbine — second generation single crystal airfoils with the latest serpentine cooling technology and advanced thermal barrier coatings, super-conductive shroud air seals, low leakage combustor brush seals, more aerodynamically efficient bowed stators, and various mechanical and coating enhancements designed to reduce wear, eliminate leakage and simplify assembly. These improvements greatly enhance durability and provide substantial margin for future thrust growth.

Redefining Full Life:  For over 30 years, the U.S. Air Force’s F100 Component Improvement Program (CIP) has supported the development of significant reliability, maintainability and safety improvements for all F100 models.  In 1993, the Air Force recognized that the F100-PW-229 had reached a level of technological development that would ensure its full-life maturity at 4300 TAC.  As a result, the Air Force initiated the development of an Engine Enhancement Package (EEP) with the objective of achieving a F100-PW-229 engine specification of 6000 TAC’s.  Incorporation of the F100-PW-229 EEP — successfully demonstrated in 2004 — achieves the objective of increasing the engine depot inspection interval from 4300 to 6000 TAC.  This increase is equivalent to extending the depot interval from seven years to ten years.  In addition, the EEP provides a 30 percent life cycle cost reduction over the life of an F100-PW-229 engine.  The EEP also offers significant safety benefits; reducing the predicted in-flight shutdown rate by 25 percent.  The F100-PW-229 engine is the only fighter engine funded and qualified by the U.S. Air Force to the 6000 cycle capability.

Infusion of Advanced Technologies: The F100-PW-229 Engine Enhancement Package (EEP) includes a sixth-generation digital electronic engine control system, which incorporates advanced engine health monitoring (prognostics and diagnostics) and aircraft interactive capabilities, as well as the advanced hot section technology developed for the F-22 Raptor F119 engine and the F-35 Lightning II F135 propulsion and lift system.  The F100-PW-229 EEP significantly increases the life capability of the turbine hardware by incorporating these low-risk technologies developed and matured for the fifth-generation fighter engines – Pratt & Whitney’s F119 and F135.  No other production fighter engine manufacturer in the world has this unique opportunity for incorporating these proven advanced technologies into its near-term products.

Improving F-15 Fleet Longevity, Performance and Affordability: The U.S. Air Force (USAF) continues to invest in the F100-PW-229 EEP, through the CIP, in order to increase time-on-wing and to expand the inspection interval as Air Force maintainers move toward improved and more streamlined maintenance practices. The EEP program is especially important to the Air Force in increasing the depot maintenance interval and reducing operating cost of its F-15 fleet, which is expected to continue to play a critical roll in U.S. combat readiness beyond 2035.  Reduced removal rates, increased depot intervals and usage-based maintenance capability, as provided by the sixth-generation digital electronic control system and advanced engine software, mean the engine stays in operation much longer, resulting in significantly reduced maintenance infrastructure and maintenance expense.  The EEP will be incorporated in all production F100-PW-229 engines beginning in 2009.  These engines will be available for new F-15 and F-16 production and for the replacement of engines in existing fleets where the benefits of low cost of ownership and improved performance and reliability are considered important.  The EEP features have also been specifically designed so that they can be easily installed in all existing pre-2009 F100-PW-229 engine assets. The F100-PW-229 EEP engine combines proven design features with evolutionary technology enhancements to effectively balance low technical risk, affordability and high performance for all existing and future F-15 and F-16 applications.

Customer Support and Satisfaction is Key:  Pratt & Whitney is proud of the F100 engine family’s track record  over the last 30 years of operational service, and with the new F100-PW-229 EEP, the F100 remains the engine of choice for F-15 and F-16 fighter aircraft around the globe.

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作为发动机小白，进来看一下我们和西方差距有多大。。。。。。。
被郁闷了。。。。。。。:D

如果给FC20配这个，那改动得有多大？？？？？:hug:

229EEP应该可以当成235使用。

我们买不到或者说买不到好的先进的，那就只有自己造！发展好了，以后还要卖！作为大国，眼光要远一点！

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看着眼谗
跟老美打个商量?;P

与其临渊羡鱼，不如退而结网。

原帖由 rainy_heart79 于 2009-4-2 13:20 发表

这个比M2好很多吗?

如果按照纸面上的数据对比的话，99M2要求是14100公斤（实际能不能达到现在没有确切消息可以证明），因此最大推力229EEP处于下风。不过其他诸如重量，推重比，寿命而言，99M2皆处于下风，而且差距比较大。

原帖由 damo56030 于 2009-4-2 02:03 发表
如果给FC20配这个，那改动得有多大？？？？？:hug:

给屁股减减肥就是了

可怜

相信有朝一日 太行一定能做到这样

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好东西啊， 到时候，从巴铁那里弄回几台，再好好山寨吧！

呵呵，给了小巴，就等于给了我们了吧？至少就研究而言。

老米很精明,给的都是土鳖快有的东西,给JF-17配上F414EFE才是河蟹啊[:a6:]

原帖由 kktv206 于 2009-4-5 23:14 发表
老米很精明,给的都是土鳖快有的东西,给JF-17配上F414EFE才是河蟹啊[:a6:]

何以见得？说得难听点，TG现在的TH比91年定型的PW1129都不如呢。为什么美国佬会给巴基斯坦这么一款好发动机呢？那是美国佬想给一种差一点的发动机都比较难。:L
其实，给FC-1配上F414-GE-400就很河蟹了，其他不用多想。:D

MMD，跟LZ同感，要是能给FC1安上一台EJ200···········································
那可就太爽了

是呀 如果能搞到来山寨的话 还是不错的

PW也拿這一顆來台兜售~針對台灣現有的F16機群
美國現在要賣的這批f-16~事前已跟小巴約法三章~要洩出不容易~

以台灣的經驗
台灣的愛國者就是被美國人管制著
不管零件調度甚至是維修都有美國的代表看管著(住在台灣)
要仿要偷受到很大限制

原帖由 kktv206 于 2009-4-5 23:14 发表
老米很精明,给的都是土鳖快有的东西,给JF-17配上F414EFE才是河蟹啊[:a6:]

你这个“快有”指的是10年还是20年，弓虽啊

是不是TG经常想让别人包括毛子、EU、MD，认为自己快有了

PW的这款发动机与土星的117S相比如何？117S刚在乌发厂批产，可靠性怎样尚不得而知。。。

近几年的美国发动机出口，(五个外国客户) PW已4：1远远把GE抛到后边 ，最大原因
就是EEP的6000TAC。太诱人了。

关我们p事，你又摸不着

langge945 发表于 2009-4-6 16:22

很难山在

damo56030 发表于 2009-4-2 02:03


    机甲位置倒了个头

PRINCEBUSTER 发表于 2009-4-4 15:47

C/C复合材料还是SiC/SiC 复合材料？


重量减轻不少哎。

板岗丁 发表于 2010-8-9 01:21


    PW客机发动机比较悲剧， 军用的把GE压住了。 一涨一跌。

[:a9:]
这个~与其穿白裤衩不如裸奔的好，一台顶N台，让人活不活

kktv206 发表于 2009-4-5 23:14


    。。。。。。跟土鳖有没有有什么关系，给这个纯粹是因为找不到还在量产却更差得可以出售了。 米国人这次给小巴的已经是他手头能拿出来的最差的东西了，只不过米国人手头最差的东西么，却都是很强的

真是流口水啊，国内要加油啊

    maya老大，我知道TG和美国对航空发动机寿命的测定标准不同。

PW宣传：The F100-PW-229 EEP engine increases the engine depot inspection interval from seven years to 10 years and provides up to a 30 percent cost reduction over the life the engine.  The EEP will also offer significant safety benefits, with an expected 25 percent reduction in the already low probability of in-flight shutdown.

6000TAC，3000飞行小时---库房检修间由7提升到10年，那么如果通俗一些，我个人把这个标准往TG的标准来套，F100-PW-229EEP的总寿命超过6000-8000小时，不知你是否认同？一台航空发动机只要在必要的时间进行热端等大部件更换，完全可以满足配备该飞行器全寿命飞行时间。即发动机与飞机同寿。

PW称，EEP的设计检修间隔达6000TAC，大概3000飞行小时等级...
F100-PW-229
June 13,2008

Reliable, H ...
aliasmaya 发表于 2009-4-2 01:27

    maya老大，我知道TG和美国对航空发动机寿命的测定标准不同。

PW宣传：The F100-PW-229 EEP engine increases the engine depot inspection interval from seven years to 10 years and provides up to a 30 percent cost reduction over the life the engine.  The EEP will also offer significant safety benefits, with an expected 25 percent reduction in the already low probability of in-flight shutdown.

6000TAC，3000飞行小时---库房检修间由7提升到10年，那么如果通俗一些，我个人把这个标准往TG的标准来套，F100-PW-229EEP的总寿命超过6000-8000小时，不知你是否认同？一台航空发动机只要在必要的时间进行热端等大部件更换，完全可以满足配备该飞行器全寿命飞行时间。即发动机与飞机同寿。

无论什么时候，总有人希望突破尺寸限制，小飞机装大发动机，看着爽啊
FC20要想换这个，首先后机身尺寸不够，重心还严重后移，把这些问题解决了自身重量已经大增，翼负荷暴涨，瞬盘和巡航效率骤降，于是再增加翼面积，改完了发现尺寸也和16差不多了。
关于16和废柴的比较，这帖子以前有人在XH发过，这里应该还有不少人有印象