Wednesday, October 10, 2007

Abstract

The aircraft industry has always been fast and very advanced in multiple aspects of engineering field. Aircraft propulsion is a fast-moving field of research and development. Today we are striving towards the Ultra Efficient Engine Technology (UEET) that has 3 main challenges: have an engine accommodating all kinds of speeds; increase efficiency and reduce emissions; reduction in NOx emissions. To meet these goals, 7 technology areas are being looked into under the UEET program.

Most, if not all, commercial aircrafts today are using the turbofan and this is not mere coincidence. From the humble beginnings of propulsion where piston engines were employed, propulsion has seen a wide variety of engines. This report will be looking into a timeline involving the various engine types and why these engines became history soon after they surfaced, leaving the jet engine to dominate to propulsion field. Even while the jet engine emerged the obvious choice, there were numerous modifications made to the jet engine. This report will weigh the benefits of the different variations: turbojet, turbofan, turboprop and ramjet. Each of these engines excels in their own range of flight conditions but for the commercial aircraft, turbofans were the most suitable and practical.

While turbofans remain the choice of today, research carries on under the UEET program and there are several design drivers that are being looked into. Market demand is always high, strict and asking for prices as low as possible. These are always compromised by regulatory standards and technical limitations. Regulatory standards revolve around aircraft noise and pollutant emissions. These factors are actually being looked into in the development of UEET. Technical limitations include material limitations and structural limitations. Every material can only handle a certain range of conditions and will fail no matter how strong it is. Despite this, new materials are constantly being produced with composite materials and superalloys being the current favourites.

From where the forefathers of aircraft propulsion left us, we have certainly made leaps and bounds of improvements to the engine. The UEET program by NASA is the latest step towards perfection of the engine. This program is worldwide and involves numerous big names in the aviation industry. The continuous search for materials and methods to withstand harsher conditions is going strong.

With all these ongoing efforts, ‘engines of the future’ are something to look forward to in the near future. In fact, the ideals of an ultra efficient engine may have already been achieved and being improved further upon.

1.0 Introduction

1.1 Background

It takes cutting edge technology and out of the world innovativeness to survive in the aircraft industry. Pratt and Whitney (P&W), a world leader in design, manufacture and service of aircraft engines, is developing technology with the potential to reduce fuel consumption and hence, cut down on the emissions of harmful greenhouse gases CO2. For the average Boeing 777-200ER, this would reduce annual fuel costs by about $1 million and CO2 emissions by about 11,700 metric tons. Besides the above mentioned, P&W’s TALON (Technology for Advanced Low NOx) combustor reduced NOx emissions on the PW4000 by 30% versus the originally certified combustor. In addition, P&W’s next generation of TALONs will make engines like the PW6000 even cleaner and quieter. One can expect P&W to continue their environmental leadership, but they are not alone.

Rolls-Royce (RR), with 50 other partners across Europe, has been conducting research into aircraft noise since 2001 in the largest aircraft noise research project ever supported by the European Commission (EC). SILENCE(R) (Significantly Lower Community Exposure to Aircraft Noise) is performing large-scale validation of over 20 noise technologies that were initiated through EC and national projects in 1998.

While leading aircraft companies like P&W and RR engage in vastly different projects with their respective partners and research centres, their goals are similar:

· Increase efficiency to reduce CO2 emissions and fuel cost savings
· Reduce aircraft noise
· Reduce NOx emissions

It is no mere coincidence that these large companies are working towards the same goals. They are all part of the NASA’s Ultra-Efficient Engine Program (UEET) that is one of the main design drivers powering modern and subsequent future aircraft designs. In the long run, UEET will enable the planet to enjoy cleaner air and the aircraft industry to leave lesser imprint on the environment.


1.2 Objectives and scope

The purpose of this project is to explore the possibilities the UEET program aims to achieve, particularly in the context of commercial aircrafts.

From this project, we will be able to appreciate:

· The UEET program by NASA;
· technical accounts of the evolution of aircraft engines that led to the popular turbofan engine in the present day;
· important economic and regulatory standards and factors that drive the design towards conceptualization of ultra efficient engines;
· technical challenges faced in the conceptualization of UEET program;
· critical view of “the engine of the future”.

2.0 Ultra-Efficient Engine Technology (UEET)

Present engines have several weaknesses and limitations. Hence, ultra efficient engines are being looked into to provide better efficiencies, lower fuel consumption rates, reduction of noise and reduction of pollution levels.

Ultra-Efficient Engine Technology Program (UEET) is a 5 year program of NASA that plans for the next generation of aircraft engines. This program requires the close partnership with several organizations as well as the utilization of NASA’s expertise and research facilities to come up with technologies that can overcome three main challenges.

The first challenge is to have an engine that can provide for all kinds of speeds including subsonic, transonic, hypersonic and supersonic. Presently, different engines are designed for different speeds. For instance, turboprop and turbofan are limited to low speed airplane and ramjet is built for high but limited range of speeds.

The second challenge is to increase efficiency so as to reduce CO2 emissions based on fuel savings of up to 15%.

The last challenge is to develop technologies for 70% reduction in NOx emissions during takeoff and landing conditions. This is important as there are air quality concerns and potential ozone depletion issues linked with NOx emissions.

The UEET program has 7 technology areas, namely:

1) Propulsion Systems Integration and Assessment
2) Emissions Reductions
3) Highly-Loaded Turbomachinery
4) Engine Materials and Structures for High Performance
5) Propulsion-Airframe Integration
6) Intelligent Propulsion Controls
7) Integrated Component Technology Demonstrations


1) Propulsion Systems Integration and Assessment
This section takes the technologies developed in other projects, integrates them into the conceptual system and assesses how successful they are in meeting UEET goals. The assessments act as a guide to the program and help to identify any shortfalls.

2) Emissions Reductions
This section aims to develop combustion technologies to reduce NOx emissions by 70% during the landing and take-off cycle from the 1996 International Civil Aviation Organization standards and also reductions of reasonable standards during cruising.

3) Highly-Loaded Turbomachinery
This section will address the efficiency and fuel burn goals of the program through providing flow controlled turbomachinery technology for the higher UEET cycle pressure ratios.

4) Engine Materials and Structures for High Performance
This section will develop computational material science tools and advanced high temperature materials to cater for quality performance, high efficiency and environmentally friendly propulsion system.

5) Propulsion-Airframe Integration
This section will try to determine the best nacelle position and the optimum nacelle and airframe shaping so as to reduce aerodynamic drag. The reduction of aerodynamic drag will improve performance and efficiency, leading to fuel burn reduction and hence less CO2 emissions.

6) Intelligent Propulsion Controls
This section will develop intelligence technology through the use of sensors, actuators, control logic and propulsion system integration to help improve engine hardware maintenance, increase flight safety.

7) Integrated Component Technology Demonstrations
This section will carry out tests on the technologies developed to make sure they are functional when integrated into the overall system. This confidence is necessary to reduce risk.

3.0 Evolution Of Aircraft Designs

This section will consist of the following sub-topics:

3.1 Overview
3.2 Timeline Leading to The Jet Engine
3.3 Different Types of Jet Engines
3.4 Choice of Engine for Today

3.1 Overview

The history of propulsion goes back a long way, for more than 100 years since the Wright brothers started building a simple engine with only 3-hp and one cylinder. It was a considerable feat in that era. Engineers, regardless of which era, strived for more power, longer durability and higher efficiency in the smallest and lightest designs possible. Above all that, there were costs and maintenance considerations. Advances in propulsion have been great for the past 100 years and continue to strive for even better engines.

The first engine to take flight was the piston engine. As time passed, different types of engines emerged, including today’s very popular jet engines. Jet engines have variations and today, the turbofan remains the most popular in commercial aircrafts. Even in combat aircrafts, turbofans with afterburners are also very popular. A timeline in the next section will exemplify everything more clearly in the following page.

3.2 Timeline leading to the jet engine

3.3 Different types of jet engines

The jet engine is clearly the choice for aircraft propulsion due to all its advantages over the other engine types as seen in the previous section. The term “jet engine” is often used as a generic name for a variety of engines, including the turbojet, turbofan, turboprop, and ramjet. These engines all operate by the same basic principles, but each has its own distinct advantages and disadvantages. All jet engines operate by forcing incoming air into a tube where the air is compressed, mixed with fuel, burned, and exhausted at high speed to generate thrust. Following we shall compare briefly the differences between the types of jet engines.

Table 3.3.1 below shows some specifications of a few selected engine models. This is a very limited list but nonetheless provides us with figures that will show why the turbofan remains the choice of today.

1.1.1 Turbojet

This is the most basic of the jet engines. Most of today’s turbojets are fitted with axial-flow compressors due to their aerodynamic properties and compact packing. Afterburners can be fitted just before the nozzle to burn additional fuel, providing an extra boost. This however, consumes a lot of fuel and is hence only used for brief periods (eg.: in dog fights). Despite being able to provide higher thrust to weight ratio, the fuel consumption of these engines were very high, making flights more expensive for civilians.


Figure 3.3.1.1 (a) Schematics of a centrifugal flow turbojet; (b) Schematics of an axial flow turbojet (Source: http://en.wikipedia.org)

1.1.2 Turbofan

The turbofan has a similar structure to the turbojet except for a fan section in front of the compressors. The fan is also driven by the turbine, but instead of compressing air like the other rotating blades, its primary purpose is to force more air through outer ducts that go around the engine core. Despite this cooler air travelling at much lower speeds, the sheer mass of air that is accelerated by the fan produces a significant thrust on top of what the turbojet core engine is producing. This additional thrust is obtained without burning extra fuel since the fan is powered by the turbine. Thus, the turbofan is much more fuel efficient than the turbojet. In addition, the low-speed air helps to cushion the noise of the core jet’s exit air making the engine much quieter. This is highly desirable in commercial aircrafts as there are residential areas near the vicinity of most airports.

Figure 3.3.2.1 (a) Schematics of a low bypass turbofan; (b) Schematics of high bypass turbofan (Source: http://en.wikipedia.org)

1.1.3 Turboprop

The turboprop is similar to the turbofan; however, the fan is not ducted and is a completely external propeller. In turboprops, it is not surprising to see more than 80% of the thrust coming from the propeller. This is attractive because of its very high fuel efficiency, even higher than the turbofan’s. But the mechanical structure of the turboprop introduces a lot of noise and vibration, making it unsuitable for commercial aircrafts. The centre of rotation of the propeller is never in the centre of the engine, causing violent and noisy vibrations. It is, however, a clear choice when it comes to engine selection for long-range planes that require high endurance.


Figure 3.3.3 Schematics of a turboprop (Source: http://en.wikipedia.org)

1.1.4 Ramjet

Figure 3.3.4.1 Schematic of a ramjet (Source: www.answers.com)

The ramjet looks very different from all the other jet engines in that it has no more rotating components. It is simply a jet engine with all its interior components removed, for greater simplicity and efficiency. The only drawback is that it needs to be moving at very high speeds in air for co mbustion to occur. The lack of a compressor means the engine needs to ram through air at speeds fast enough to cause the air to compress and combust on its own. This implies that it is impossible to be used on commercial aircrafts since commercial aircrafts only fly at subsonic speeds. The ramjet is used on missiles. From the table, it is seen that the ramjet has excellent thrust to weight ratio. However, the fuel consumption of the ramjet is very bad below supersonic speeds. The operating speed is between M2 to M5. When the speed is sufficient, the engine will switch to the ramjet for better efficiency.

3.4 Choice of Engine for Today

When selecting an engine for a commercial aircraft, the two most crucial factors are fuel economy and meeting regulatory standards. Of course, there are other factors such as maximum power or thrust and operating velocity that comes into the design process.

In the case of a commercial aircraft, cruising flight is about M=0.8, hence ramjets are impossible to be used. Also, flights need to be stable and quiet. This implies that turboprops are not practical for use in large airliners.

The turbofan is ideal because it not only has very high fuel efficiency, the reduced speed of the air at the nozzles also reduce noise pollution. This is why the turbofan remains the choice of today.

As mentioned earlier, engineers of today are still not satisfied with the turbofan’s superior performance. Research and development is still striving for an even better engine that will meet the goals of the UEET. While these researches are on-going, the turbofan continues serving on almost all of today’s commercial aircrafts.

4.0 Design Drivers

This section will consist of the following sub-topics:

4.1 Overview
4.2 Economic
4.3 Regulatory Standards
4.4 Engine Materials & Structures

4.1 Overview

When airlines choose which engine to use, there are several factors that they look at. As a business, money is always an issue. Hence fuel efficiency, maintainability, lifespan and cost of engine are important factors to consider. It would be ideal to have an engine that has very high fuel efficiency and high thrust with specifications that can power any aircraft with ease. However, there are always limitations in this industry where safety is never compromised. For an engine to be airworthy it would have to withstand extreme conditions and these will come with a price tag.

Also, there are limitations imposed by governments. Aircraft engines are known to be noisy and emitting greenhouse gases and other pollutants. Since such costs are not borne by airline companies, the government has set regulations to ensure that emissions and noise levels are kept low enough. As engineers, the strive for higher efficiency, less waste/ emission is always on. Despite the long development to have obtained the turbofan today, research and design carries on to meet demands and limitations from all aspects.

4.2 Economic

When purchasing air tickets, the fuel surcharge ranges from S$100 to S$400, which is sometimes more than the air ticket itself. Despite advertisers placing prices as low as S$1 from Singapore to Thailand, the true prices are always much more because of expensive fuel surcharges. When measuring performances of an engine, the thrust-to-weight ratio and SFC are often used, and these are priority specifications that airlines look at when they decide which engine to purchase.

From the evolution of engines from piston engine to turbojet engine and then to turbofan engine, we see that the turbojet was invented after piston engine because turbojet engines are able to have a higher power-to-weight ratio as compared to the piston engine. Turbofan was later invented because turbojet was notorious for its high fuel consumption and hence the turbofan to reduce the fuel consumption and increase efficiency. As we see here, fuel consumption is an important factor in the design of engines. We need to keep this as low as possible in order to save cost and to improve performance.

Ways to achieve fuel savings include increasing the turbine inlet temperature and decreasing the engine weight. Under the ultra efficient engine program, advanced disk alloy will be evaluated to test if it can withstand the high turbine inlet temperature. Advanced thermal barrier coatings will also be explored together with advanced cooling systems for the same reason.

To reduce the engine weight, innovative lightweight materials and structural concepts will be developed. In addition, the fan will also be designed to reduce weight and improve efficiency. Reducing engine weight in general will contribute to reduction of overall fuel consumption.

In respond to the relatively low efficiency of current engines, ultra efficient engines program will include the ultra-high-loaded axial compressor technology to target a pressure ratio of 12:1 in four stages with a polytropic efficiency of 92%.

4.3 Regulatory Standards

International Civil Aviation Organisation (ICAO) is the global forum for international civil aviation and has succeeded for more than 40 years in bringing the world together around increasingly stringent regulations for aircraft emissions and noise. Besides ICAO that works in close co-operation with various UN bodies, there exist other regulatory governance bodies that set regulatory standards for the civil aviation industry in aspects of noise and emissions regulations. These bodies include the influential Federal Aviation Authority (FAA) who imposes strict Federal Aviations Regulations (FARs) on aircrafts flying to and within the United States of America (USA) and these FARs are at the same time widely adopted by air carriers worldwide. The Environmental Protection Agency (EPA) of the USA standards are equivalent to the NOx emission standards of the UN International Civil Aviation Organization (ICAO) too. Hence, it may seem that there exist various agencies whose regulatory standards aircrafts must adhere to but, eventually, they originate back to those of ICAO’s.

According to the recent publication of the ICAO environmental report, initiatives to promote the sustainability of aviation activities in synchronization with the growth of the industry over the past four decades have successfully reduced aircraft noise by a whopping 75%, and CO2 emissions intensity by 70%. While research and development work in improving environmental standards in the aviation industry has been intensely ongoing for major turbine manufacturers such as General Electric (GE) and Pratt & Whitney (P&W), regulatory standards must definitely be in place, stringent as ever, and constantly looked into to review them according to current and projected trends in aviation travel. Of these regulatory standards, amongst are aircraft engine emissions and noise control standards that are of most relevance to the UEET program and in producing ‘the engine of the future’ as aircraft engines’ designers strive for a more environmental approach towards their conceptualization of their future engines.




4.3.1 Aircraft engine emissions

While engine emissions of aircraft may seemingly be grouped together with those of automobile vehicles on the road, it is more accurate to identify aircraft engine emissions with a significant portion emitted at altitude. With relations to the turbofan engine that is widely used in commercial aircrafts today. Figure 4.3.1.1 below shows the schematic production of emissions from the engine.

These emissions at high altitude will alter the atmospheric concentration of greenhouse gases and trigger the formation of condensation trails and may increase cirrus cloudiness, all of which will contribute to the change of climate. Indirectly, aircraft engine emissions have also greatly contribute to the consequences felt by the world as with rising sea-levels and extreme weather changes.

The jet exhaust usually contains harmful gases like oxides of nitrogen, carbon monoxide and particulate matter. These components can lead to ozone depletion and global warming. Other components of the exhaust such as aerosols and particulates are harmful as they are suspected of producing clouds that could affect the earth’s climate changes. Currently, most combustors in engine meet the 1996 International Civil Aviation Organization landing and takeoff NOx limits by small margins.

The famous Kyoto Protocol signed in Japan in 1997 has excluded international aviation emissions from their targets, while also stating that the responsibility for cutting down or limiting greenhouse gases from aircrafts will work through ICAO.

The Council of ICAO and the Committee on Aviation Environmental Protection (CAEP) has hence adopted engine certification standards contained in Annex 16 – Environmental Protection, Volume II – Aircraft Engine Emissions to the Convention on International Civil Aviation. Since this inception, technological innovations in aircraft engines have resulted in reductions of key air pollutants.

As can be observed in figure 4.3.1.2 below with respect to P&W’s engines, pollutant especially that of unburned hydrocarbons (UHC) has dropped significantly for the transformation of the older JT8D-200 to the more technologically sound JT8D-EKIT.


To achieve certification, it must be demonstrative that the characteristic emissions of the engine type for HC, CO, NOx and smoke are below the limits defined by ICAO. The certification process is performed on a test bed, where the engine is run at four different thrust settings, to simulate the various phases of the LTO cycle, as follows:

- take-off (100% available thrust) for 0.7 min;
- climb (85% available thrust) for 2.2 min;
- approach (30% available thrust) for 4.0 min; and
- taxi (7% available thrust) for 26 min.

The test bed process is as depicted in figure 4.3.1.3 below:


With certification, the next step for these OEMs is to work towards the goal of UEET’s aim to fulfill several emissions criteria. The engine should have a combustor that can reduce the NOx emissions by 70% over the landing and take-off cycles from the 1996 International Civil Aviation Organization standards, with no increase in other emission constituents such as smoke, unburned hydrocarbons and carbon monoxide. Gas turbine propulsion technologies that allow carbon dioxide reductions will be developed. With regards to the problems caused by aerosols and particulates, levels of emission will be assessed and reduced if possible. The operability for safe flights, cost of engines and ease of maintenance should not be affected by this emission reduction. The ultra efficient engine should also reduce the threat of ozone depletion by 90% through the use of combustor technologies.

The effect and impact the UEET had created is apparent in the present day. Of technical achievements accomplished most recently, Rolls Royce’s Trent 1000 engine, used in the new Boeing Dreamliner B787, is designed and built such that the fuel burnt during operation in 15% lesser compared to engines 1 decade ago. In addition, emissions will be decreased by 40% as compared to current international legislation and regulations. Airbus, on the other hand, is not lagging in this competitive race. Its brand new A380, the largest civil commercial aircraft to date, has the lowest fuel consumption per passenger of any large commercial aircraft yet built.

While OEMs work on the technical and engineering aspect of such improvements, researchers are in search of an alternative fuel that might cut down on the harmful emissions that contribute to the greenhouse effect. Presently, the fuel used in the civil aviation industry is kerosene that is derived from crude oil, providing a good balance of energy density, operational issues, cost and safety, all properties required of an aviation fuel. As fuel costs rise and the future looks bleak for the downtrend of the fuel prices and the depleting supply of fuel, R&D work are in process to find a fuel replacement. Apart from better economical and environmental-friendly impacts, a viable alternative aviation fuel could possible stabilize world fuel price fluctuations and hence, reduce uncertainties and vulnerabilities from over-reliance on a single type of fuel.

Aircraft and engine manufacturers are currently looking into the possibility of using synthetic jet fuels from coal, natural gas or other hydrocarbons feedstocks and also biogas. Ideally, the fuel should not require OEMs to change or re-design the engines.

As we can see, the trends for the designs of new aircrafts are heading towards that of economical and environmentally friendly at the same time. Perhaps, the ‘engine of the future’ will have even better performance than the B787 and A380 economically-wise and also more environmentally friendly.




4.3.2 Aircraft noise

Besides aircraft emissions, the other aspect of regulatory standards most often discussed and focused on is aircraft noise. Aircraft noise is the most apparent source of aircraft pollution for many, especially felt by residents residing near airports. This is a significant cause of adverse community reaction related to the operation and expansion of airports both in developed and developing countries.

ICAO has been addressing the issue of aircraft noise since the 1960s. The first Standards and Recommended Practices (SARPs) for aircraft noise certification were published in 1971. They are contained in Annex 16 to the Convention on
International Civil Aviation (Volume I - Environmental Protection — Aircraft Noise). These Standards have been updated since then to reflect improvements in technology.

Reducing or limiting noise originating from aircraft is therefore paramount and one of ICAO’s important goal set out to achieve. Although aircrafts coming out of production lines these days are 75% quieter than 40 years ago according to ICAO’s researchers, aircraft manufacturers are still competing to design even quieter aircrafts to market their products as the world becomes more environmentally conscious. For instance, Boeing’s new Dreamliner aircraft (B787) is also expected to deliver significant improvements in noise, about 15 to 20 decibels (dB) below the Chapter 4 limits, and therefore at least 10dB better than the older aircraft (e.g. B767, A330) it replaces. Figures 4.3.2.1 and 4.3.2.2 below show the progress of noise reduction at source over the last 40 years.




As depicted above, noise has been greatly reduced over the last four decades since the inception of aircraft noise regulation. There is substantial belief that the ‘engines of the future’ will probably have even greater reduction of noise as compared to present standards.

The number of people exposed to aircraft noise is the metric normally used to estimate aircraft noise impact. ICAO’s Committee on Aviation Environmental Protection (CAEP) has developed a computer model for assessing global exposure to the noise of transport aircraft, known as MAGENTA Recent estimates from the MAGENTA model have shown an improvement in the global noise situation with a reduction in the size of the population within the 65 dB DNL1 contours of about 30 percent in 2006, relative to the 2000 level. Noise insulation programs and other noise management and reduction initiatives are often developed around airports to reduce the noise experienced by the exposed population.

Aircraft acoustic certification involves measuring the noise level of an aircraft in
Effective Perceived Noise Level (EPN) dB at three points: two at take-off (flyover and sideline), and the third during the approach. These steps are illustrated in figure 4.3.2.3 below.





4.4 Engine Materials & Structures

4.4.1 Overview

Different types of materials used in engines include plastics, metals, ceramics and composites. Each of these has its own advantages and disadvantages. Plastics cannot withstand high temperatures but are lighter than many other materials, less breakable and rust-free. Metals used in engines usually refer to alloys and superalloys that have high strength and can withstand high temperatures and stresses. The three main groups of superalloys are nickel-based, cobalt-based and iron-based. Ceramics can withstand high temperatures but are quite fragile. They are usually combined with other material to form composites. Composites are able to withstand high temperatures and are light in weight. The three main types include polymer matrix composite (PMC), metallic matrix composite (MMC) and ceramic matrix composite (CMC).




4.4.2 Turbofan

Different parts of the engine have different requirements for its material. We shall look into a turbofan engine and explore the usual requirements in the materials of the fan, compressor, combustor, turbine, mixer and nozzle. Figure 4.4.2.1 below outlines the 6 main parts of a turbofan engine and the requirements and materials used for these 6 parts are elaborated in table 4.4.2.1.




As seen from table 4.4.2.1 above, different materials are used in different parts of the engine due to different requirements and temperature working range. Materials are being constantly improved upon to facilitate the best functioning of engine. Most of the time, materials of fans, combustors and turbine are being looked into for better efficiencies. For instance, General Electric has introduced the use of composite fan blade of the typical titanium ones. The advantage of using composite is that the engine will become lighter and the engine can have a higher bypass ratio. These allow the engine to have lower fuel consumption and hence are more efficient.

Below is a diagram taken from Rolls Royce that highlights the improvements in efficiency of engines in relation to the bypass ratio.

Combustors in jet engines require high temperatures for optimum combustion process. The higher the temperature, the better the fuel burns to completion and hence the higher the fuel efficiency and the lower the emissions. Usually, combustion temperatures exceed the melting point of most materials. As such, air must be cooled by a cooling system before entering the turbine. Alternatively, materials that can withstand this high heat can be used together with some insulating coatings.

Under the ultra efficient engine technology, ceramic matrix composite, polymer matrix composites and advanced disk alloys will be looked into for use in combustor liners and turbine vanes in order to withstand high temperatures so that complete combustion of fuel can take place. As for the static engine structures, lightweight materials will be developed to reduce the overall weight and hence reduce fuel consumption.

In addition, ultra efficient engines will also make use of active combustor control to achieve a lower combustor pattern factor and hence reduce the turbine cooling requirements. An extra benefit generated by this method is that thermal fatigue and failure can be reduced.

5.0 Conclusion

Aircraft designers and manufacturers are designing and building better aircrafts as compared to those produced four decades ago. Through the evolution of aircraft engines leading to the jet engines, with turbofans dominating the civil aviation industry, substantial R&D and regulations are in place for continual improved performance of the aircrafts with respect to the 2 important aspects powering the aviation industry. These two aspects comprise of OEMs vying to have the most economical engine designs and yet, at the same time have the least environmental impact on the planet. These two aspects justify why the turbofan remains the choice engine of today since the turbofan is much more fuel efficient than the turbojet and the low-speed air helps to cushion the noise of the core jet’s exit air making the engine much quieter.

At the same time, Ultra-Efficient Engine Technology Program (UEET), a 5 year program of NASA, plans for the next generation of aircraft engines to improve aircraft performance in terms of noise and emissions reduction. This program requires the close partnership with several organizations as well as the utilization of NASA’s expertise and research facilities to come up with technologies that can overcome the challenges.

As the aviation industry booms, regulatory standards are in place to ensure the aviation industry do not leave a negative impact on the planet and that living standards and quality are not affected by the industry. ICAO, the global platform for such regulatory standards, is the main driving body that oversees R&D, imposes stringent regulatory standards on aircraft carriers and promotes initiatives to improve standards. And indeed, current evidences show that the success of these programs and stringent standards has vastly improved noise and emissions reduction and is enjoyed by the aviation industry as seen by the economical fuel efficiency and reduced noise of the new A380 and B787.

However, the technical challenges remain for OEMs to find suitable materials to withstand the more demanding operating conditions and to adhere to regulatory standards. ‘Engines of the future’ will make use of active combustor control to achieve a lower combustor pattern factor and hence reduce the turbine cooling requirements and thermal fatigue and failure. In addition, it is of paramount importance to consider propulsion-airframe integration and not neglect effects of aerodynamics, flight stability and control, thermodynamics, amongst other considerations that designers might have.

In conclusion, the future looks set for ‘engines of the future’ as improved noise reduction and emissions continues. Coupled with ongoing projects, initiatives, stringent regulatory standards and fierce competition from aircraft companies, the conceptualization of ultra efficient engine is possibly already achieved and will definitely be improved further.

6.0 References and Acknowledgements

We would like to extend our thanks to the following sources of information for their valuable sharing and apologise to any sources that we are unable to duly cite.

Journal of Propulsion and Power - Volume 20 No. 4, July-August 2004
Raymer, Daniel P., 2006, Aircraft Design: A Conceptual Approach, American Institute of Aeronautics and Astronautics.
ICAO, Convention on International Civil Aviation, 9th Edition, 2006.
EPA, Emission Standards and Test Procedures for Aircraft and Aircraft Engines, 2005
Mattingly, Jack D., Elements of Propulsion : Gas Turbines and Rockets, American Institute of Aeronautics and Astronautics, 2006

Online references:

http://www.allstar.fiu.edu/aero/turbine2.html
www.lompraha.cz/files/publikaceaj.pdf
www.grc.nasa.gov/www/k-12/airplane/aturbf.html
http://mason/gmu.edu/~sazahari/analysisrevision.html
www.ueet.nasa/gov/overview.html
http://www.allstar.fiu.edu/aero/peakdesign.html
http://web.mit.edu/newsoffice/1995/noisepollution.html
http://www.yale.edu/ynhti/curriculum/units/1988/6/88.06.06.x.html#h
http://www.rolls-royce.com/community/downloads/environment04/environment.pdf
http://www.pw.utc.com/vgn-ext-templating/v/index.jsp?vgnextoid=995abc5f3e7fb010VgnVCM1000000881000aRCRD
http://www.aerospaceweb.org/question/propulsion/q0033.shtml
http://www.alt-accel.com/s-pogo/rkt-lst.htm
http://machinedesign.com/ContentItem/62642/100yearsofAircraftengines.aspx
http://commons.wikimedia.org/wiki/Image:Liberty_Aircraft_Engine_Number_1.JPG
http://www.epa.gov//
http://www.faa.gov/
http://www.caa.co.uk/default.aspx?catid=702&pagetype=68&gid=712
http://www.pw.utc.com/vgn-ext-templating/v/index.jsp?vgnextoid=995abc5f3e7fb010VgnVCM1000000881000aRCRD
http://www.enginehistory.org/OX5to3350.pdf
http://www.scienceandsociety.co.uk/Pix/TRN/11/10438911_T.JPG
http://www.warbirdsresourcegroup.org/LRG/images/lrg0727.jpg
http://www.jet-engine.net/civtfspec.html
http://www.memagazine.org/supparch/flight03/jetsfans/jetsfans.html
http://www.centennialofflight.gov/essay/Evolution_of_Technology/piston_engines/Tech23.htm
http://inventors.about.com/od/jstartinventions/ss/jet_engine_3.htm