Chinese Engine Development

latenlazy

Brigadier
F129 and F135 use the same core. F135 is at close to 200KN, isn't it?
Right, but it's a higher bypass turbofan, and cannot supercruise.

The post makes some pretty remarkable claims. It says that the WS-15 achieves the same performance with two compressor stages to the F119's three. I find that a bit hard to believe.
 

i.e.

Senior Member
Right, but it's a higher bypass turbofan, and cannot supercruise.

The post makes some pretty remarkable claims. It says that the WS-15 achieves the same performance with two compressor stages to the F119's three. I find that a bit hard to believe.

No, some one mentioned that
WS-10A has 2 stage LP compressor and 7 stage HP compressorl. that 2 stage fan roughly achieve the same compression and bypass ratio as variants of F110's 3 stage.

Right, but it's a higher bypass turbofan, and cannot supercruise.

The post makes some pretty remarkable claims. It says that the WS-15 achieves the same performance with two compressor stages to the F119's three. I find that a bit hard to believe.

supercruise has very little to do with by-pass ratio.

design the right intake and given the right drag polar you can supercruise.
 

latenlazy

Brigadier
No, some one mentioned that
WS-10A has 2 stage LP compressor and 7 stage HP compressorl. that 2 stage fan roughly achieve the same compression and bypass ratio as variants of F110's 3 stage.
Hmm, might've misread then. I'll go back and check it out again later.
supercruise has very little to do with by-pass ratio.

design the right intake and given the right drag polar you can supercruise.
Well, it's actually not just about the intake and the drag. Those are important but the engine itself plays a key role. The specific impulse of the exhaust is the final determinant on top speed. If your exhaust cannot reach supercruising speeds neither can the engine (and whatever's strapped onto it). Though a higher bypass ratio doesn't have a direct effect on whether an engine can supercruise, a higher bypass ratio can lower the specific impulse of the exhaust. In the case of the F135, if I'm not mistake they sacrificed the specific impulse of the engine to achieve a higher thrust by having a higher bypass ratio engine.

Nope, didn't misread.

我国在风扇上早就没有问题了(08年展出的二级风扇性能基本可与F119的三级抗衡),完整版的涡扇15应该快出来。
Our Country no longer has problems with the compressor/fan (The performance of the 2 stage compressor developed in 2008 can basically compete with the F119's three stage compression).
 
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i.e.

Senior Member
Hmm, might've misread then. I'll go back and check it out again later.

Well, it's actually not just about the intake and the drag. Those are important but the engine itself plays a key role. The specific impulse of the exhaust is the final determinant on top speed. If your exhaust cannot reach supercruising speeds neither can the engine (and whatever's strapped onto it). Though a higher bypass ratio doesn't have a direct effect on whether an engine can supercruise, a higher bypass ratio can lower the specific impulse of the exhaust. In the case of the F135, if I'm not mistake they sacrificed the specific impulse of the engine to achieve a higher thrust by having a higher bypass ratio engine.

Nope, didn't misread.

我国在风扇上早就没有问题了(08年展出的二级风扇性能基本可与F119的三级抗衡),完整版的涡扇15应该快出来。
Our Country no longer has problems with the compressor/fan (The performance of the 2 stage compressor developed in 2008 can basically compete with the F119's three stage compression).

No, specific impulse means energy imparted per unit mass of working fluid. I think you got some science messed up in the terms.

having a relatively high by-pass ratio doesn't mean air coming out of end can't be supersonic.

and what was that " fan displayed in 08? "
 

latenlazy

Brigadier
No, specific impulse means energy imparted per unit mass of working fluid. I think you got some science messed up in the terms.

having a relatively high by-pass ratio doesn't mean air coming out of end can't be supersonic.

and what was that " fan displayed in 08? "
WS-10. Doof. He's still saying that the performance WS-10's two stage compressor can match the F119's. I don't know if I buy that.

And you're right. I pulled the wrong term. I was thinking about exhaust impulse, and not specific impulse.

This is what happens when you stay up all night trying to finish your Russia readings -_____-;.

I know higher bypass fans can still have supersonic exhaust (hence why I emphasized a very loose relationship), but using the same core with a higher bypass ratio will slow the exhaust down, and in the case of the F-35 enough for it to prevent supercruising.
 

Hendrik_2000

Lieutenant General
A very long and exhaust study on Chinese Low bypass Turbo fan for military but as usual full of inaccuracy , conjecture, bias, and conflicting statement. Check this link it got a lot of graph and sources

Please, Log in or Register to view URLs content!


First he said that china is 3 decaded away from US based on similiar chinese paper that required more study He even acknowledge that it is probably a ploy to get more funding the same strategy in keep updating fighter in US inventory

Then He guess that china doesn't have clue about maintenance of high performance engine but at the same time he cite plant 529 in Sichuan that improve the russian engine life from 900 hr to 1500 hr

Then he imply China use simple CAD like Autocad or single purpose CAD system and not dassault system but we know that China use CATIA which own by Dassault system

Then he mention weakness in material science but also acknowledge there is improvement here but from very low base But we know that Certain Mr Shi Changxu is given public commendation for inventing the single crystal metal after working 30 years in the field

He also give primer on high precision machining oblivious to the fact that China together with Taiwan own 55% of the market for CNC machinery.Yup china is backward here

Using super alloy production and consumption in China he said china will have trouble meeting the production of jet engine because China is not self sufficient in super alloy production. But but Even though China is the world largest steel producer in the world China still import steel that is because there is such a huge demand of steel in this particular time that might not be there tomorrow So buidling plant to meet temporary demand is a folly

he then teach us about thermal stress as if Chinese engineer has no clue about thermal stress because it wasn't taught at Chinese university. He also said China need to learn about modelling These day you can buy ANSYS or NASTRAN that run on PC Boot legged version are aplenty in Asia

Sir the proof is in the pudding WE know that at least 4 regiments of J !!B or more are now equipped with WS 10A Taihang and none of them has fell off from the sky

So nothing more than your usual western exceptionalism Here is the article


Executive Summary:

–Engines commonly used in Chinese and other modern aircraft may be divided into several major categories: (1) low-bypass turbofans typically power military jets; (2) high-bypass turbofans typically power jet airliners; (3) turboprops typically power more fuel-efficient, usually lower-speed aircraft, including civilian commuter aircraft and military transports and surveillance and battle management aircraft; and (4) turboshafts typically power helicopters. This study will address the first category, low-bypass turbofan engines; other categories will be addressed in follow-on China SignPost™ reports.

–China’s inability to domestically mass-produce modern high-performance jet engines at a consistently high-quality standard is an enduring Achilles heel of the Chinese military aerospace sector and is likely a headwind that has slowed development and production of the J-15, J-20, and other late-generation tactical aircraft.

–The Chinese aerospace industry is driven by four key strategic imperatives as it pursues the ability to manufacture large volumes of high-performance tactical aircraft[1] engines: (1) parts dependence avoidance, (2) Russian supply unwillingness, (3) aircraft sales autonomy, and (4) poor Russian after-sales service.

–To address these shortcomings, AVIC is treating engine development as a high priority and plans to invest 10 billion RMB (US$1.53 billion) into jet engine research and development over the next 5 years.

–However, evidence still suggests that AVIC’s engine makers are having trouble maintaining consistent quality control as they scale up production of the WS-10, causing problems with reliability and keeping China’s tactical aircraft heavily reliant on imported Russian engines.

–Key weak points of the Chinese military jet engine industry include: turbine blade production and process standardization.

–Standardization and integration may be the one area in which the costs of China’s ad hoc, eclectic approach to strategic technology development truly manifest themselves. The Soviet defense industrial base failed in precisely this area: talented designers and technicians presided over balkanized design bureaus and irregularly-linked production facilities; lack of standardization and quality control rendered it “less than the sum of the parts.”

–We estimate that based on current knowledge and assuming no major setbacks or loss of mission focus, China will need ~2-3 years before it achieves comprehensive capabilities commensurate with the aggregate inputs in the jet engine sector and ~5-10 years before it is able to consistently mass produce top-notch turbofan engines for a 5th generation-type fighter.

–If China’s engine makers can attain the technical capability level that U.S. manufacturers had 20 years ago, China will be able to power its 4th generation and5th-generation aircraft with domestically made engines (3rd and 4th-generation in Chinese nomenclature, respectively). These developments would be vital in cementing China as a formidable regional air power and deserve close attention from policymakers.

China has a clear strategic interest in developing indigenous high-performance aeroengines to power its military aircraft. This is one of the greatest aerospace engineering challenges, however, one that only a small handful of corporations worldwide have truly mastered. This should not be surprising: an engine is effectively an aircraft’s cardiovascular system; it can be transplanted but not easily modified. Unlike a human system, it can be designed and developed independently, but faces temperature, pressure, and G-force challenges that only the most advanced materials, properly machined and operated as an efficient system, can handle. While China has made progress in recent years with materials and fabrication, it appears to remain limited with respect to components and systems design, integration, and management—the keys to optimizing engine performance in practice—and to making logistical and operational plans at the force level based on reliable estimates thereof.

Based on available open source evidence, Chinese progress in this critical area remains uneven and the whole remains “less than the some of the parts.” Given the overall capabilities inherent in China’s defense industrial base and the resources likely being applied to this problem, we expect that China will make significant strides, but barring major setbacks or loss of mission focus, it will take ~2-3 years before it achieves comprehensive capabilities commensurate with the aggregate inputs in this sector and ~5-10 years before it is able to consistently mass produce top-notch turbofan engines for a 5th generation-type fighter. When it does, however, the results will have profound strategic significance, as China will have entered an exclusive club of top producers in this area and eliminated one of the few remaining areas in which it relies on Russia technologically.

How is domestic engine production strategically relevant?

The Chinese aerospace industry is driven by four key strategic imperatives as it pursues the ability to manufacture large volumes of high-performance tactical aircraft engines: (1) parts dependence avoidance, (2) Russian supply unwillingness, (3) aircraft sales autonomy, and (4) poor Russian after-sales service. First, China likely seeks to avoid dependence on Russian suppliers for vital parts. Chinese leaders will not want the country’s most modern fighter aircraft to be dependent on foreign inputs for a core system such as propulsion. Second, Russia’s own armed forces are likely to buy significantly more of its jet engines in the next 10 years than they did over the 20 years since the Soviet Union dissolved. This is an important development given that the collapse in military procurement after the Soviet Union fell was the key driver of Russian jet engine sales to China.

The Russian Air Force’s plans to enhance its aircraft through refurbishment and re-engineering of existing systems and acquisition of new platforms like the SU-34, SU-35, and T-50/PAK FA could stretch Russian engine makers to the point that they have little export willingness, and perhaps restrained export capacity. The Kremlin, which controls Russia’s jet engine makers, will likely prioritize the export of entire aircraft such as Sukhoi Flankers that require advanced engines and the Indo/Russian 5thgeneration fighter project, which will also demand the most advanced engines Russia’s defense suppliers can produce. The bottom line is that the combination of new Russian Air Force aircraft purchases, continued exports of late model Flankers, and Russia’s joint 5th generation fighter project with India will stretch suppliers enough that even if the People’s Liberation Army Air Force (PLAAF) can get some advanced Russian engines, it likely will not be able to obtain enough to support its desired levels of aircraft production.

Exhibit 1: Estimated Total Chinese Demand for Non-Russian Military Turbofans (2011-20)




Sources: Sukhoi, Ria Novosti, Reuters, India MoD, UMPO, Jane’s, Sinodefence.com

Third, China is a growing exporter of advanced combat aircraft, as shown by its recent deals to sell FC-1 and J-10 fighters to Pakistan, and will not want foreign engine suppliers having veto power over its arms sales. A major hang-up in the FC-1 deal was that the aircraft uses the same Russian-made RD-33 engines as the MiG-29, but sells for a much lower price and is thus a threat to Russian aircraft exports in the developing world. Russia finally granted China permission to make the FC-1 sale to Pakistan, but the experience almost certainly taught Chinese aircraft makers that it will be much easier to export Chinese-made aircraft if they use Chinese engines.

This is especially true given the fact that China’s J-10 and J-11B (if SAC is permitted to export it) are comparable to existing Russian tactical aircraft exports and would likely be formidable competitors in terms of price and capability. We note here that a January 2011 editorial in Nanfang Daily anticipates China becoming a major jet engine exporter within the next 10 years.[1] High aspirations by no means imply the ability to actually achieve the desired capability, but these sentiments shed light on the broad importance Chinese policymakers and thinkers place on bolstering domestic jet engine production capabilities.

Fourth, China has had painful experience with poor Russian after-sales service for components, e.g., engines. This includes engineering and spare parts support that is expensive, delayed, or simply nonexistent and manuals that are limited, in Russian only, or not available at all.

Where does China’s tactical turbofan sector stand today?

In an April 2011 interview, China Aviation Industry Corporation (AVIC) head Lin Zuoming noted that despite China’s rapid development as an aerospace power, the country’s ability to produce modern jet engines remains a glaring weakness.[2] To address these shortcomings, AVIC is treating engine development as a high priority and plans to invest 10 billion RMB (US$1.53 billion) into jet engine research and development over the next 5 years.

China’s WS-10 Taihang turbofan engine and its derivatives have performance parameters on par with the Pratt & Whitney (P&W) F100 and GE F110 engine families, which power the U.S. F-15 and F-16 fighters. The Taihang family is said to power the J-11B and is also likely slated to eventually take over from the Russian AL-31 as the main powerplant for the J-10 and J-15. Media reports from November 2010 state that a version of the WS-10 Taihang turbofan producing 27,500 lbs of thrust is now in series production and is being used to power the J-11B fighter-bomber.[3]Exhibit 2 (below) shows a timeline of China’s advanced military turbofan production.

Exhibit 2: China Military Turbofan Development and Production Timeline (WS-10, WS-15)




Sources: Jane’s, Global Times, China.com

However, evidence still suggests that AVIC’s engine makers are having trouble maintaining consistent quality control as they scale up production of the WS-10, causing problems with reliability and keeping China’s tactical aircraft heavily reliant on imported Russian engines. Russia’s defense industry appears to believe that China will continue to be unable to attain reliable mass production of high-performance military turbofans. For example, NPO Saturn, a key Russian military jet engine maker, forecasts that it will continue serving as the primary engine supplier for China J-10 and FC-1 fighter programs through 2019.[4] Saturn’s optimism may stem in part from the fact that is it currently in talks with China over the possible sale of 190 D-30KP-2 turbofans, which could be used on China’s IL-76 aircraft.[5]

The lack of a sufficient supply of reliable domestically made jet engines could significantly impede future production of the J-10, J-11, J-15, and J-20 fighter aircraft. The J-20 program especially needs domestic engine development and production breakthroughs because the Russia appears reluctant to sell the 117S series engines that could enable the J-20 to have sufficient power to allow the aircraft to supercruise (sustain supersonic flight without using inefficient afterburners) and match the performance of 5th-generation fighters such as the Lockheed Martin F-22 and Sukhoi T-50/PAK FA.

Software is a vital aspect of aeroengines, one that China will have to master to produce its own high-performance engines; and one that it will likely consider controlling carefully should it decide to market them when they reach the requisite quality and price level. Many aeroengine performance parameters can be adjusted using software; a manufacturer may charge a customer significantly for upgrades that are easily implemented but may alter engine function significantly. There is a tremendous disparity between civilian (uncertificated) and military (certificated) source codes: the former may have explanations embedded in them, while the latter may have source codes and explanations stored separately.

Military source codes can take up to twenty times longer to produce on a per-line basis because of requirements concerning annotation, documentation, line traceability, integration, and module- and robustness-testing. How to handle the relevant engine source code is therefore a key question for any exporter of packages that include aeroengines. The U.S. is typically able to avoid divulging source codes, despite repeated requests from such customers as Israel, because its military aircraft are so desirable.

Recent developments increasingly suggest that it is unwise to underestimate China’s defense-industrial complex. We believe that barring major unforeseen disruptions or shifts in focus, China’s aerospace industry already has sufficient financial support and is close to attaining a critical mass of human capital that over the next ~2-3 years will help it make substantial breakthroughs in its ability to produce sufficient volumes of reasonably dependable jet engines, and reach the ability to consistently produce 5th-generation fighter performance-level aeroengines in ~5-10 years. This, in turn, will help enable robust growth of modern Chinese airpower if the country’s civilian and military leaders choose to expand and upgrade China’s Air Force and Navy tactical air fleets. Ongoing limitations in tooling, design capability, and systems operations and maintenance and will be key areas to monitor, however, as these may limit the performance parameters of Chinese engines and shape their development in “path dependent” ways (meaning that future options are limited by are limited by past actions, even after the circumstances that shaped those actions are no longer relevant).

Strong and Weak Points of China’s Jet Engine Industry

High performance jet engines are exceedingly hard to produce, as they can contain tens of thousands of parts that must be made of durable exotic materials machined to tolerances measured in microns. In addition, jet engines used in tactical fighter and strike aircraft must be able to operate reliably under extreme conditions including high temperatures, high speeds, intensive maneuvering, and frequent throttle changes. Jet engine compressor blades, for instance, can experience centrifugal forces as high as 20,000 times the force of gravity during flight.[6] The challenge that a turbofan blade faces in performing without significant deflection despite being exposed to heat that exceeds the melting point of most metals, and consequent materials and metallurgical requirements, has been likened to stirring hot soup with a spoon made of ice.

Chinese design capabilities remain uncertain, though manufacturing capabilities are clearly improving. To reach the pinnacle of aeroengine development and performance, China must model, refine, and optimize the total system, which can only be done with top-level total lifecycle tools, software, and cradle-to-grave support. Even in a less complex machine such as an automobile, for instance, it is relatively easy to manufacture a crankshaft, but relatively difficult to make the system perform well as a unified whole and to understand the complex interaction of its components under different conditions.

To consider an aeroengine-specific example, for optimum aerodynamics, it is necessary to model the airflow implications of a turbofan blade changing slightly. A high-pressure turbine might be strengthened, but if its thermal characteristics change, then it might not expand in the same way, and the resulting discontinuity in surface geometry could lead to a failure that destroys the engine. Important areas to design for and model therefore include airflow, fatigue, and reliability.

The most important aeroengine performance metrics include mean time between failure (MTBM)—i.e., how long an engine lasts; and mean time before overhaul (MTBO)—i.e., how often an engine must be serviced fully. This, in turn, is linked to the degradation pattern/structure, which is vital to managing engine maintenance and anticipating performance. “Hitting the wall,” or experiencing a sudden and marked decline in engine performance, is particularly hazardous in military aviation, where even slight deviation from optimum performance parameters can be highly problematic. Unpredictable dynamics, or lack of knowledge of existing patterns, can be make it much more difficult to make the best use of engines—even in training, but especially in combat.

Compensating for shortcomings in either of these areas might require factoring in a substantial margin of error by dedicating additional engines and airframes; were the need great enough, something like 200 Flankers might be needed to ensure the mission fulfillment capabilities of roughly 100 F-15s. Other important metrics include acceleration/deceleration patterns, foreign object damage (FOD) resistance (Russian engines have historically fallen significantly short in this regard), and cold/hot temperature starts (the former is usually more difficult than the latter, but the amount of difference varies by engine model).

In short, an aeroengine system is only as good as its design, monitoring, and lifecycle management. This may be an area of particular weakness for China, as it has traditionally relied heavily on copying and emulating foreign designs. This approach does not confer ability to design and manage aeroengines; on the contrary, it can impose path-dependent limitations that lead to dead ends or substandard, poorly integrated systems that are costly and difficult to alter and thus remain “less than the sum of their parts.”

While this systemic component of Chinese turbofans remains uncertain, however, the techniques and processes to support their manufacture are clearly improving. Chinese gas turbine experts say the country’s aerospace industry has improved its jet engine manufacturing abilities in key areas, including:[7]

–Precision cutting, welding, and machining, e.g., five-axis milling for production of turbine blades.

–Special materials blade production. China’s largest turbine blade production facility, located at Xi’an Aero-Engine, can now undertake mass-production of turbine blades made from superalloys, titanium alloys, cobalt alloys, and stainless steel. The turbine blade quality rate is now said to exceed 95%.

–Hollow fan blade production. China is entering the nascent stages of being able to produce hollow fan blades. Hollow titanium fan blades are 15-20% lighter than their equivalents and make an engine more fuel efficient. They also reduce rotating mass and allow a tactical aircraft engine to spool up more quickly during maneuvers.[8]

–Greater automation. This improves standardization and efficiency.

–Process modeling. Computer-aided process modeling help manufacturers anticipate problems with materials, welds, and behavior of parts under heat stress. Flagging potential trouble spots before machines are started helps save time and money and also ultimately helps produce a higher quality, more durable engine.[9]

–Enhanced ability to use numerically-controlled milling machines to produce turbine disks.

–Better ability to produce high-quality, standardized spare parts. Reliable access to such parts is essential to supporting aircraft performance, particularly at the high and unpredictable operational tempo inherent in many operational scenarios. Spare parts have traditionally represented an area of weakness in China’s aviation industry.

Still unclear, however, are key design, system, software, and reliability aspects of engine systems and components. Vibration testing of components is important (e.g., under high-G forces for military engines). It is difficult to determine China’s stage of development for Fully Automatic Digital Engine Control (FADEC), or the capability of the engine to communicate with the cockpit; and for Engine Control Units (ECU), the “brain” of the engine, which helps it to regulate itself.

Many of the Chinese jet engine industry’s recent improvements center on turbine blade production, which is logical given turbines’ location at the heart of any jet engine. However, a comprehensive analysis by experts from the China Gas Turbine Establishment, which played a major role in designing the WS-10 engine, does not discuss improvements in engine reliability. Thus, better blade manufacturing and machining may still not have brought about commensurate improvements in quality control and engine reliability. The WS-10A is now said to be flying in the PLAAF’s J-11B, and as engines accumulate flight hours it will be telling to see how powerful and efficient they are, how they hold up, and how frequently they require overhaul. The PLA is notably opaque about aircraft losses, but occasional reports do slip through, providing a barometer of reliability to watch as domestically-made engines spend more time in the air.

What challenges do Chinese military jet engine makers continue to face?

China’s attempts to mass produce P&W F100-class jet engines and develop an engine powerful enough to give the J-20 true 5th generation performance levels face a range of technical and process challenges. On the technical side, Chinese gas turbine researchers say weaknesses remain in turbine casting, powder metallurgy for creating turbine disks, and molding hollow titanium parts.[10] Many of these areas were named as ones in which substantial progress has taken place in recent years. Nonetheless, progress may be from a very low baseline, making the claims that problems remain while progress has occurred compatible with each other.

Chinese engine makers likewise need to create advanced production lines to ensure effective logistical support for domestically-made engines and must also automate their production facilities to a greater extent. Part of the technical challenge stems from the fact that machining the tough superalloys used in jet engines requires twice the cutting force of other types of machining and that cutting tools may have to be changed up to 10 times more often than when machining softer materials like those used for making auto parts.[11]

While this necessitates highly specialized production lines, however, a given engine needs to be produced on the same line to ensure economies of scale and quality consistency. Once systems are optimized, separating production into different lines should be avoided, as a stand alone approach could disrupt or crack the system. It is one thing to make a single turbofan blade in a laboratory, and another entirely to ramp up to mass production of several thousand (a single engine contains 400-500 blades in up to two dozen stages of 2-3 dozen blades each) blades of standardized, reliable quality. This requires mastering both the metallurgy grade and mastering the industrial process to reliably produce a high-quality product.

In the very limited publicly available discussions of China’s jet engine manufacturing weaknesses, local experts focus heavily on process weaknesses as major constraints on China’s ability to produce high-performance turbofans of consistently good quality. Chinese analysts cite the need to better integrate the research and manufacturing segments of the industry, creating databases to save knowledge that can be used to make construction more effective, reducing the boundaries between the jet engine design, materials, and fabrication sectors, and doing a better job training new technical and engineering staff.[12] Exhibit 3 (below) depicts key technical and process weaknesses currently affecting China’s tactical turbofan production.

Exhibit 3: Where China’s Military Jet Engine Makers Continue to Experience Problems




Source: Defense Manufacturing Technology, USCC, China SignPost™

To put these weaknesses into context, they suggest that in some areas Chinese engine makers are roughly three decades behind their U.S. peers. Technical reports by U.S. manufacturers discussing challenges of actually making hollow fan blades that date back to 1977, implying that Chinese engine fabricators could be three decades behind the state-of-the-art curve at present.[13]

Abstracts of P&W technical papers from 1976 discuss using nickel superalloy powders to forge turbine discs for the F100 engine.[14] In contrast, as mentioned above, researchers from the China Gas Turbine Establishment cite powder metallurgy for turbine disc production as an enduring weak spot for China’s jet engine industry.[15]Of course, this may represent an attempt to secure additional funding, as opposed to a true reflection of current status; when did the U.S. Air Force (USAF) ever run out of update programs for its fighters?

One cautionary point here is that Chinese jet engine makers have a latecomer advantage, which allows them to learn from other engine makers’ successes and failures and potentially to shave years from their own research-development-production sequence. To put matters in perspective, the P&W F119 engine that powers the F-22 Raptor was developed and refined in the 1980s and ’90s, so China does not necessarily need to attain the current 2011 state-of-the-art in tactical jet engine technology to field formidable propulsion systems that could give the J-20 true 5thgeneration fighter performance characteristics.

What China must achieve, however, is a methodology akin to Six Sigma or Total Quality Management (TQM) to ensure quality control and sufficient organizational honesty to ensure that actual problems are reported and that figures are not doctored. Otherwise, standardization and integration may be the one in which the costs of China’s ad hoc, eclectic approach to strategic technology development truly manifest themselves. The Soviet defense industrial base failed in precisely this area: talented designers and technicians presided over balkanized design bureaus and irregularly-linked production facilities; lack of standardization and quality control rendered it “less than the sum of the parts.”

Mapping China’s Key Jet Engine R&D and Production Assets: Size and Resources

Chinese jet engine makers may remain slightly understaffed relative to U.S./UK producers of military jet engines, but comparably staffed relative to their Russian and French peers. Liming Aero-Engine and Xi’an Aero-Engine, AVIC’s flagship large military jet engine makers, have a combined staff of less than 20,000. By comparison, P&W, Rolls-Royce, and GE Aviation, the world’s largest military jet engine makers, each have more than 35,000 staff (Exhibit 4).


Exhibit 4: Number of Workers at Major Global Tactical Turbofan Makers



Source: Company reports

Examining overall employment figures tends to over count personnel relevant to “Big Three” engine production and undercounts it for other manufacturers, however. The total head count at the former includes individuals involved in civilian, military, and global services programs (typically fairly-evenly-subdivided), not just dedicated R&D personnel. That at the latter does not include many R&D and metallurgy-relevant individuals employed in other organizations.

China’s jet engine complex may increase staffing somewhat if it seeks to become largely or fully self-sufficient in military turbofan production. With 15,000 workers, Russian manufacturer UMPO planned to produce 109 AL-31 and AL-41 engines in 2010.[16] Larger firms like GE Aviation, by contrast, can deliver approximately 200 high performance turbofans and 800 total military jet engines and helicopter engine turboshafts per year.

Technical Challenges

High-performance tactical jet engines are difficult to produce, but the work does not stop there, as the engines often undergo demanding usage and pose key maintenance and logistical challenges. Key potential constraints China will likely face in operating the high-performance tactical turbofans it is beginning to series-produce include issues involving technical, performance, and environmental factors, the ability to obtain sufficient materials for mass production of multiple engine families, and political/economic challenges.

Thermal cycling. The engines on a large transport or tanker typically run at a fairly steady speed setting for most of a flight. Engines on tactical aircraft, by contrast, undergo extreme speed changes as pilots frequently and quickly change throttle settings during high-intensity maneuvering. As the engine undergoes rapid temperature changes, thermal cycling generates significant wear. The experiences of the USAF with the first truly high-performance U.S. afterburning turbofan, the P&W F100, exemplify the unexpected safety and maintenance challenges that thermal cycling can generate.

While developing the F100, P&W engineers believed that the key determinant of stress on engine parts would be the length of time spent at the highest temperatures (i.e. full power and/or very high speed flight).[17] In practice, however, the F100’s unprecedented performance enabled new air combat techniques and training regimens that emphasized rapid and frequent maneuvering. This incurred relatively little time at full power or high Mach numbers, but entailed far more throttle changes than the engine designers had anticipated.

In fact, while the F100 design requirements called for being able to accommodate 1,765 full throttle transients during the engine’s service life, actual operational use showed that engine life ended up being more than 30% lower than expected because the engine was undergoing more than five times the number of full throttle transients it had been designed for—10,360 cycles (Exhibit 5).

Exhibit 5: Key usage parameters of the F100 afterburning turbofan, November 1979




Source: The Great Engine War

As China develops indigenous high performance tactical turbofan engines, more intensive air combat training will make shortened engine life from thermal cycling an important issue to resolve. It is unclear how much experience China has in this area to date given that most Chinese pilots do not fly nearly as much as their U.S. counterparts and also may not be engaging in as intensive or realistic training. PLAAF and PLA Navy (PLAN) newspapers and other documents describe exercises in which engine use in particular is minimized wherever possible, as well as a variety of accidents that were caused by engine failures. Likewise, lower flight times in the Soviet/Russian air force, combined with different tactics, may mean that Russian engine makers are not able to draw on the same firsthand experience with combating thermal cycling wear that their American peers have.

Chinese technicians are making real progress in learning how to improve engines that are already fielded and wring the maximum life possible out of them. China’s 5719 Jet Engine Repair Plant has allegedly found a way to extend the operating life of Russian-made AL-31F engines from 900 hours to 1,500 hours.[18] It is almost certain that the WS-10 and any new jet engines made in China will incorporate any life extension and other improvements that the PLAAF and PLAN Aviation have gleaned from the Russian engines that are currently the backbone of their flight operations.

Other Environmental Factors

Vibration resistance is another key determinant of engine performance. If an engine sucks in a small stone, for instance, it can nick a plate, thereby producing a small vibration, which in turn can lead to performance degradation and even failure. Environmental factors that can have negative impact include high/hot airfields (H&H), “sandy” air, salt-water corrosion, and FOD. Russian engines, for example, typically have less FOD resistance than those of Western design. Indian Air Force Su-30MKI aircraft reportedly exhibited significant limitations at the Red Flag 2008 exercises at Nellis Air Force Base because of the FOD vulnerabilities of their Russian engines. These problems were not caused by Indian maintenance procedures; agreements with Russia require that any damaged engines be shipped back to Russia for servicing.[19]

Performance Possibilities

It remains to be seen whether China can develop reliable engines with key high-performance capabilities essential for world-class military aircraft. These include thrust vectoring, the ability to control an aircraft’s attitude or angular velocity by redirecting its exhaust slightly; continuous power-output at all speed and altitude settings without performance drops; and stall resistance. The last two factors could be particularly important, yet difficult, for China to master. The engine used in the Russian Su-27, the AL-31F turbofan, reportedly experiences performance power drops at certain power demands, e.g., high angle of attack (AoA) maneuvers. Under such conditions, there is a risk of disturbed air and fuel flow.

Particularly in a non-thrust vectored aircraft, if the engine becomes air-strained at a high AoA, the engine can suddenly have difficulty in using fuel, possibly leading to blade stall or discontinuous airflow, thereby starving the engine of oxygen. China’s J-11 variant uses these engines, and its canards suggest that it is designed for precisely these sorts of maneuvers. The key to avoiding such problems is to design the engine inlet to optimize its cross-section geometry while avoiding a tendency toward stalling. Sophisticated modeling is needed to deconflict these countervailing factors, however; hence the importance of determining Chinese capabilities and approaches in these critical areas.

Structural Challenges

China’s military jet engine sector faces a number of critical structural problems. Many of these are human and bureaucratic issues that can be much more difficult to resolve successfully than technical problems are. Two vulnerabilities stand out.

First, China’s defense officials will have to deal with single source contractor risks. China’s domestic military jet engine production all lies under the control of Aviation Industry Corporation of China (AVIC), a state-owned aerospace conglomerate. AVIC’s jet engine production facilities at Shenyang, Xi’an, and Guizhou compete to some extent, but we suspect that the competitive and innovative pressures are not as acute as those which companies like P&W and GE Aviation face. When present in moderation, competitive pressure helps produce innovative engines, lowers costs, speeds up development, and tends to incentivize better aftermarket service. In the late 1970s and early ’80s, the behavior of P&W, then a single-source supplier that the USAF felt was not being responsive to its concerns, prompted the government to foster competition between GE and P&W in the military jet engine sector. The resulting “Great Engine War” helped create architecture whereby U.S. combat aircraft can be designed around a range of powerplants produced by two competing firms. This organizational structure appears to work well. In China’s case, by contrast, there may be less “competition” at the macro level but more at the micro level. This may allow for localized bargaining and patronage that leads to duplication of effort, mismanagement of resources, and an increase in time to market. Here it will be necessary to determine how the “system” of organizations involved in Chinese aeroengine development and production actually work in practice, and whether and to what degree they are “more than the sum of the parts” in practice.

Second, analyses of jet engine development and production in the U.S. credit inter-service cooperation, management stability in both the companies and government, and the use of small teams that were allowed to take risks with a minimum of red tape helped foment jet engine development and production breakthroughs.[20]

Of these two areas, China is likely to struggle most deeply with issues of inter-service cooperation, since service chiefs in China likely view themselves as competitors for slices of the pie in any given budgetary period. Resource constraints will pose less of a challenge since military jet engines typically cost between US$2.5 million and US$5 million apiece. Supporting a very aggressive tactical aircraft buildout by producing 500 tactical turbofans per year would account for only about 2% of China’s total 2011 defense spending. Overall, structural issues pose major challenges, but can be dealt with incrementally once a country masters the basic technology and metallurgy of jet engine making.

Technologies and business practices to improve engine production

Quality control shortcomings have plagued Chinese indigenous jet engine production to date, particularly for high performance engines like the WS-10 series. In response to this and broader concerns, AVIC has declared 2011 to be a “year of quality” and pledges a tight focus on quality control across the aerospace production chain, which presumably will apply to aeroengine manufacturing as well.[21] AVIC’s motion follows on the heels of a September 2010 State Council document that outlines steps for achieving better quality control in military hardware production in China.[22] The report does not specially mention aerospace or jet engine production, but its existence implies that the commitment to improving China’s indigenous military systems production of all varieties runs straight to the top. How and to what extent these directives are realized in practice will hinge on design capability (e.g., involving materials, airflow, simulation and calculations, MTBF, systems integration, and FADEC/ECU design). It will be essential to avoid imbalances in which some parts are “better” than others, as this can introduce asymmetries and problems at the system level.

AVIC’s press statement covering its desire to bolster quality control does not discuss specific details. That said, well-documented quality control programs implemented by key global jet engine makers can shed light on the likely basic mechanics of how AVIC’s plans may take shape. P&W, one of the largest military jet engine makers in the world, has a system known as Achieving Competitive Excellence (ACE). ACE entails a focus on the following factors:

–Total productive maintenance

–Quality Clinic Process Chart

–Root Cause Analysis

–Mistake Proofing (this can be measured by first pass or final yield)

–Process Certification

–Setup Reduction

–Standard Work

China currently does not use total lifecycle (design) tools like the ones that Western corporations such as France’s Dassault employ. The CAD-CAM (computer-aided design and computer-aided manufacturing) stand-alone tools widely employed in China are optimized for design, not operational usage. Focusing only on design at the expense of buildability and maintainability can lead to situations in which fixing parts may be problematic because of problems with fitting hydraulic tubes between electric lines, etc.

There appears to be recognition that current approaches are inadequate. A number of sources reflect the Chinese jet engine industry’s interest in using process modeling and computer simulation to reduce build costs and construction time by envisioning problems before metal is cut.[23] China’s shipbuilding industry already uses these technologies on an industrial scale and there is significant potential for the aerospace and jet engine sectors to learn best practices from shipbuilders, with the caveat that different tolerances become a terrible problem for aircraft under extreme environmental conditions in ways that ships never experience.

China’s privately-owned shipyards are leading the way in this area. Jiangsu-based Rongsheng Heavy Industries is using concurrent design and computer simulation techniques to boost its production efficiency.[24] Concurrent design entails designing the ship hull, as well as electronics, internal components and other “guts” of the ship simultaneously using Tribon software.

Potential for Technology Transfer Between Civil and Military Industries

Military and commercial jet engines often have radically different performance parameters, but unlike other dual-use sectors like shipbuilding, the materials and construction techniques used to make key components of high-bypass turbofans for commercial airliners are in many cases quite similar to those used in making low-bypass turbofans for higher performance tactical aircraft. This is particularly true for the engine core. For example, the highly popular CFM56 commercial engine appears to share aspects of the core of the P&W F101 engine that powers the B-1B—at a minimum, there seems to be significant design overlap.

China’s aerospace industry has a growing list of joint ventures (JVs) with foreign partners including GE Aviation, P&W, and SNECMA, primarily in the areas of final assembly (vice basic design and components) and maintenance, repair, and overhaul (MRO). A good example of the latter is MTU Maintenance Zhuhai, a 50-50 joint venture between MTU Aero Engines and China Southern Airlines.[25] MRO is perhaps the most important are of major aeroengine JVs for China, as it can help Chinese experts figure out how to perform after-market, in-service overhaul and how to feed repair data back into the design and MTBF loop to improve design and performance.

As such, these JVs hold real potential for transferring technology and know-how that then could trickle into military jet engine design, production, and maintenance and potentially provide tangible improvements in Chinese air combat capabilities. China’s 2010 Defense White Paper states explicitly that “Defense-related enterprises and institutions are regulated and guided to make use of civilian industrial capabilities and social capital to conduct research into and production of weaponry and equipment.” The concept of harvesting


Just to refresh the article abut Mr Shu Changxu

Stealth jet team proves its metal


Stephen Chen
Jan 15, 2011 SCMP.com

Metallurgist Shi Changxu won a top national science award yesterday for his contribution to the development of high-performance jet engines - three days after the first public test flight of the mainland's J-20 stealth fighter plane.

Professor Shi, former director of the Chinese Academy of Sciences' Institute of Metal Research in Shenyang, developed several families of top-secret, heat-resistant alloys, according to mainland scientists working on jet engines.

The secret alloys were developed decades ago, but because jet engine metals take a long time to test, Shi's alloys have only recently begun to be used in the mainland's jet engines.

In 1955, Shi left his teaching post at the Massachusetts Institute of Technology and boarded a ship for the East. He was one of 30 or so Chinese scientists held by the United States government to prevent them from returning to communist China. Shi left the US about the same time as Qian Xuesen, a rocket scientist from the California Institute of Technology, who later founded the Chinese space programme.

After he landed in Shanghai, Shi was immediately sent to Shenyang, a heavy industry base in the northeast province of Liaoning, to boost steel production. Beijing's relationship with Moscow then soured rapidly and the Russians stopped helping their old ally develop fighter jets. The military turned to Shi for help.

With hard work, genius and luck, Shi not only came up with the required alloys using the traditional approach he learned in the West, but also devised something entirely new.

The laboratory performance of the new alloys was so good that no one dared to use them. For safety concerns, plane designers stuck with traditional alloys for China's mass-produced jet engines, whose performance lagged significantly behind their overseas counterparts.

Shi's alloys then began a long march for industrial acceptance. Only recently, with their application in some of the mainland's most advanced fighter jets such as the J-20, have designers fully accepted them.

Professor Zhang Lanting, from the school of materials science and engineering at Shanghai Jiaotong University, said the mainland's aviation material science sector had been waiting too long for this award.

Some people thought China did not have the materials to make high-performance jet engines, but they were wrong, Zhang said.
"The fact is, we have lots of top-quality materials, but to convince plane designers to use them we need to test it for decades - normally 30 years - for absolute safety," he said. "Within 10 years Chinese engines will begin to replace foreign ones in the civilian sector. In the military sector the replacement has already begun."

Professor Wu Suojun, a specialist in new materials at Beihang University, China's top aviation research institute, said the mainland was quickly narrowing the technological gap with the world's leading engine makers.

"With the successful test flight of the J-20 and other new planes, it is time to reward the heroes behind the scenes," Wu said.
 
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Blitzo

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Oh I don't know, I think it's a fairly good write up and is closer to the truth than some other articles I've seen.
He makes a few assumptions -- which are not unreasonable, but are a tad stereotypical -- these add up and lowers the bar a bit.
I think his projection of China needing 5-10 years to reliably mass produce a 5th generation engine is pretty close.

Tphuang, review this article again on your blog? :D
 
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tphuang

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I read the entire document in full. I have to say that it was very well written in my opinion. The problems in the Chinese aeroengine industry are real. And I think the predictions about 5-10 years is pretty accurate too.
 

tphuang

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This one talks about a new and improved variant of an engine is under development for a naval J-XX fighter. Clearly, this is talking about a variant of WS-10A for J-15. It talks about the work that needs to be done in this project.
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【摘要】:某型发动机为舰载战斗机歼-XX飞机的动力装置,是在某型发动机这个高起点的基础上进行研制。重点解决起飞增推,满足歼-XX飞机舰上全状态起飞性能要求;改善加速性,满足舰载战斗机着舰、复飞、逃逸的性能要求;某五型附件配装某型发动机,是以原型某型发动机相应附件为基础进行研制,为满足发动机的要求需解决以下关键技术:起飞增推;改善加速性;舰载环境的特殊要求("三防"及电磁兼容性)。为此,按下述要求改变主燃油泵调节器,喷口加力调节器的调节规律。增加特殊功率状态要求:进入特殊功率状态后,相对最大状态提高最大机械液压限制转速;改进α2控制规律;改进自动加速供油控制规律;增加特殊功率状态功能,相应增大加力供油量;改变喷口控制规律;改变πT调节规律。为满足舰载环境的特殊要求,对原型附件暴露于大气中的零组件的材料及表面处理进行分析,并进行了改进设计;对电子产品提出了"三防"要求和电磁兼容要求;附件中的接插件、电磁阀和信号器的接插件全部按美军标电连接器标准进行筛选。本文对舰载机附件"三防"及起飞增推进行研究,通过"三防"设计、建模,工程化设计。产品性能通过了发动机试车验证,并通过了"三防"摸底试验,达到了主机要求,保证了主机研制节点。
 
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