ME925-Fundamentals of Gas Turbine Engines
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Easy Access Rules for Auxiliary Power Units (CS-APU)
APU - CS Easy Access Rules for Auxiliary Power Units (CS-APU) EASA eRules: aviation rules for the 21st century Rules and regulations are the core of the European Union civil aviation system. The aim of the EASA eRules project is to make them accessible in an efficient and reliable way to stakeholders. EASA eRules will be a comprehensive, single system for the drafting, sharing and storing of rules. It will be the single source for all aviation safety rules applicable to European airspace users. It will offer easy (online) access to all rules and regulations as well as new and innovative applications such as rulemaking process automation, stakeholder consultation, cross-referencing, and comparison with ICAO and third countries’ standards. To achieve these ambitious objectives, the EASA eRules project is structured in ten modules to cover all aviation rules and innovative functionalities. The EASA eRules system is developed and implemented in close cooperation with Member States and aviation industry to ensure that all its capabilities are relevant and effective. Published February 20181 1 The published date represents the date when the consolidated version of the document was generated. Powered by EASA eRules Page 2 of 37| Feb 2018 Easy Access Rules for Auxiliary Power Units Disclaimer (CS-APU) DISCLAIMER This version is issued by the European Aviation Safety Agency (EASA) in order to provide its stakeholders with an updated and easy-to-read publication. It has been prepared by putting together the certification specifications with the related acceptable means of compliance. However, this is not an official publication and EASA accepts no liability for damage of any kind resulting from the risks inherent in the use of this document. -
The Evolution of Diesel Engines
GENERAL ARTICLE The Evolution of Diesel Engines U Shrinivasa Rudolf Diesel thought of an engine which is inherently more efficient than the steam engines of the end-nineteenth century, for providing motive power in a distributed way. His intense perseverance, spread over a decade, led to the engines of today which bear his name. U Shrinivasa teaches Steam Engines: History vibrations and dynamics of machinery at the Department The origin of diesel engines is intimately related to the history of of Mechanical Engineering, steam engines. The Greeks and the Romans knew that steam IISc. His other interests include the use of straight could somehow be harnessed to do useful work. The device vegetable oils in diesel aeolipile (Figure 1) known to Hero of Alexandria was a primitive engines for sustainable reaction turbine apparently used to open temple doors! However development and working this aspect of obtaining power from steam was soon forgotten and with CAE applications in the industries. millennia later when there was a requirement for lifting water from coal mines, steam was introduced into a large vessel and quenched to create a low pressure for sucking the water to be pumped. Newcomen in 1710 introduced a cylinder piston ar- rangement and a hinged beam (Figure 2) such that water could be pumped from greater depths. The condensing steam in the cylin- der pulled the piston down to create the pumping action. Another half a century later, in 1765, James Watt avoided the cooling of the hot chamber containing steam by adding a separate condensing chamber (Figure 3). This successful steam engine pump found investors to manufacture it but the coal mines already had horses to lift the water to be pumped. -
Failure Analysis of Gas Turbine Blades in a Gas Turbine Engine Used for Marine Applications
INTERNATIONAL JOURNAL OF International Journal of Engineering, Science and Technology MultiCraft ENGINEERING, Vol. 6, No. 1, 2014, pp. 43-48 SCIENCE AND TECHNOLOGY www.ijest-ng.com www.ajol.info/index.php/ijest © 2014 MultiCraft Limited. All rights reserved Failure analysis of gas turbine blades in a gas turbine engine used for marine applications V. Naga Bhushana Rao1*, I. N. Niranjan Kumar2, K. Bala Prasad3 1* Department of Marine Engineering, Andhra University College of Engineering, Visakhapatnam, INDIA 2 Department of Marine Engineering, Andhra University College of Engineering, Visakhapatnam, INDIA 3 Department of Marine Engineering, Andhra University College of Engineering, Visakhapatnam, INDIA *Corresponding Author: e-mail: [email protected] Tel +91-8985003487 Abstract High pressure temperature (HPT) turbine blade is the most important component of the gas turbine and failures in this turbine blade can have dramatic effect on the safety and performance of the gas turbine engine. This paper presents the failure analysis made on HPT turbine blades of 100 MW gas turbine used in marine applications. The gas turbine blade was made of Nickel based super alloys and was manufactured by investment casting method. The gas turbine blade under examination was operated at elevated temperatures in corrosive environmental attack such as oxidation, hot corrosion and sulphidation etc. The investigation on gas turbine blade included the activities like visual inspection, determination of material composition, microscopic examination and metallurgical analysis. Metallurgical examination reveals that there was no micro-structural damage due to blade operation at elevated temperatures. It indicates that the gas turbine was operated within the designed temperature conditions. It was observed that the blade might have suffered both corrosion (including HTHC & LTHC) and erosion. -
Progress and Challenges in Liquid Rocket Combustion Stability Modeling
Seventh International Conference on ICCFD7-3105 Computational Fluid Dynamics (ICCFD7), Big Island, Hawaii, July 9-13, 2012 Progress and Challenges in Liquid Rocket Combustion Stability Modeling V. Sankaran∗, M. Harvazinski∗∗, W. Anderson∗∗ and D. Talley∗ Corresponding author: [email protected] ∗ Air Force Research Laboratory, Edwards AFB, CA, USA ∗∗ Purdue University, West Lafayette, IN, USA Abstract: Progress and challenges in combustion stability modeling in rocket engines are con- sidered using a representative longitudinal mode combustor developed at Purdue University. The CVRC or Continuously Variable Resonance Chamber has a translating oxidizer post that can be used to tune the resonant modes in the chamber with the combustion response leading to self- excited high-amplitude pressure oscillations. The three-dimensional hybrid RANS-LES model is shown to be capable of accurately predicting the self-excited instabilities. The frequencies of the dominant rst longitudinal mode as well as the higher harmonics are well-predicted and their rel- ative amplitudes are also reasonably well-captured. Post-processing the data to obtain the spatial distribution of the Rayleigh index shows the existence of large regions of positive coupling be- tween the heat release and the pressure oscillations. Dierences in the Rayleigh index distribution between the fuel-rich and fuel-lean cases appears to correlate well with the observation that the fuel-rich case is more unstable than the fuel-lean case. Keywords: Combustion Instability, Liquid Rocket Engines, Reacting Flow. 1 Introduction Combustion stability presents a major challenge to the design and development of liquid rocket engines. Instabilities are usually the result of a coupling between the combustion dynamics and the acoustics in the combustion chamber. -
2.0 Axial-Flow Compressors 2.0-1 Introduction the Compressors in Most Gas Turbine Applications, Especially Units Over 5MW, Use Axial fl Ow Compressors
2.0 Axial-Flow Compressors 2.0-1 Introduction The compressors in most gas turbine applications, especially units over 5MW, use axial fl ow compressors. An axial fl ow compressor is one in which the fl ow enters the compressor in an axial direction (parallel with the axis of rotation), and exits from the gas turbine, also in an axial direction. The axial-fl ow compressor compresses its working fl uid by fi rst accelerating the fl uid and then diffusing it to obtain a pressure increase. The fl uid is accelerated by a row of rotating airfoils (blades) called the rotor, and then diffused in a row of stationary blades (the stator). The diffusion in the stator converts the velocity increase gained in the rotor to a pressure increase. A compressor consists of several stages: 1) A combination of a rotor followed by a stator make-up a stage in a compressor; 2) An additional row of stationary blades are frequently used at the compressor inlet and are known as Inlet Guide Vanes (IGV) to ensue that air enters the fi rst-stage rotors at the desired fl ow angle, these vanes are also pitch variable thus can be adjusted to the varying fl ow requirements of the engine; and 3) In addition to the stators, another diffuser at the exit of the compressor consisting of another set of vanes further diffuses the fl uid and controls its velocity entering the combustors and is often known as the Exit Guide Vanes (EGV). In an axial fl ow compressor, air passes from one stage to the next, each stage raising the pressure slightly. -
CHAPTER 9 Design and Optimization of Turbo Compressors
CHAPTER 9 Design and optimization of Turbo compressors C. Xu & R.S. Amano Department of Mechanical Engineering, University of Wisconsin-Milwaukee, USA. Abstract A compressor has been refereed to raise static enthalpy and pressure. A successful compressor design greatly benefi ts the performance of the whole power system. Lean design methodologies have been used for industrial power system design. The compressor designs require benefi t to both OEM and customers, i.e. lowest cost for both OEM and end users and high effi ciency in all operating range of the compressor. The compressor design and optimization are critical for the new com- pressor development and compressor upgrade. The design experience and design considerations are also critical for a successful compressor design. The design experience can accelerate compressor lean design process. An optimization pro- cess is discussed to design compressor blades in turbo machinery. The compressor design process is not only an aerodynamic optimization, but structure analyses also need to be combined in the optimization. This chapter discusses an aerodynamic and structure integration optimization process. The design method consists of an airfoil shape optimization and a three-dimensional gradient-based optimization coupled with Navier–Stokes solvers. A model airfoil of a transonic compressor is designed by using this approach, with an effi ciency improvement. Airfoil sections were stacked up to a three-dimensional rotor blade of a compressor. The effi ciency is improved over a wide range of mass fl ow. The results indicate that the optimiza- tion process can provide improved design and can be integrated into a compressor design procedure. -
Combustion Turbines
Section 3. Technology Characterization – Combustion Turbines U.S. Environmental Protection Agency Combined Heat and Power Partnership March 2015 Disclaimer The information contained in this document is for information purposes only and is gathered from published industry sources. Information about costs, maintenance, operations, or any other performance criteria is by no means representative of EPA, ORNL, or ICF policies, definitions, or determinations for regulatory or compliance purposes. The September 2017 revision incorporated a new section on packaged CHP systems (Section 7). This Guide was prepared by Ken Darrow, Rick Tidball, James Wang and Anne Hampson at ICF International, with funding from the U.S. Environmental Protection Agency and the U.S. Department of Energy. Catalog of CHP Technologies ii Disclaimer Section 3. Technology Characterization – Combustion Turbines 3.1 Introduction Gas turbines have been in use for stationary electric power generation since the late 1930s. Turbines went on to revolutionize airplane propulsion in the 1940s, and since the 1990s through today, they have been a popular choice for new power generation plants in the United States. Gas turbines are available in sizes ranging from 500 kilowatts (kW) to more than 300 megawatts (MW) for both power-only generation and combined heat and power (CHP) systems. The most efficient commercial technology for utility-scale power plants is the gas turbine-steam turbine combined-cycle plant that has efficiencies of more than 60 percent (measured at lower heating value [LHV]35). Simple- cycle gas turbines used in power plants are available with efficiencies of over 40 percent (LHV). Gas turbines have long been used by utilities for peaking capacity. -
Security & Defence European
a 7.90 D European & Security ES & Defence 4/2016 International Security and Defence Journal Protected Logistic Vehicles ISSN 1617-7983 • www.euro-sd.com • Naval Propulsion South Africa‘s Defence Exports Navies and shipbuilders are shifting to hybrid The South African defence industry has a remarkable breadth of capa- and integrated electric concepts. bilities and an even more remarkable depth in certain technologies. August 2016 Jamie Shea: NATO‘s Warsaw Summit Politics · Armed Forces · Procurement · Technology The backbone of every strong troop. Mercedes-Benz Defence Vehicles. When your mission is clear. When there’s no road for miles around. And when you need to give all you’ve got, your equipment needs to be the best. At times like these, we’re right by your side. Mercedes-Benz Defence Vehicles: armoured, highly capable off-road and logistics vehicles with payloads ranging from 0.5 to 110 t. Mobilising safety and efficiency: www.mercedes-benz.com/defence-vehicles Editorial EU Put to the Test What had long been regarded as inconceiv- The second main argument of the Brexit able became a reality on the morning of 23 campaigners was less about a “democratic June 2016. The British voted to leave the sense of citizenship” than of material self- European Union. The majority that voted for interest. Despite all the exception rulings "Brexit", at just over 52 percent, was slim, granted, the United Kingdom is among and a great deal smaller than the 67 percent the net contribution payers in the EU. This who voted to stay in the then EEC in 1975, money, it was suggested, could be put to but ignoring the majority vote is impossible. -
Water, Air and Fire at Work in Hero's Machines
Water, air and fire at work in Hero’s machines Amelia Carolina Sparavigna Dipartimento di Fisica, Politecnico di Torino Corso Duca degli Abruzzi 24, Torino, Italy Known as the Michanikos, Hero of Alexandria is considered the inventor of the world's first steam engine and of many other sophisticated devices. Here we discuss three of them as described in his book “Pneumatica”. These machines, working with water, air and fire, are clear examples of the deep knowledge of fluid dynamics reached by the Hellenistic scientists. Hero of Alexandria, known as the Mechanicos, lived during the first century in the Roman Egypt [1]. He was probably a Greek mathematician and engineer who resided in the city of Alexandria. We know his work from some of writings and designs that have been arrived nowadays in their Greek original or in Arabic translations. From his own writings, it is possible to gather that he knew the works of Archimedes and of Philo the Byzantian, who was a contemporary of Ctesibius [2]. It is almost certain that Heron taught at the Museum, a college for combined philosophy and literary studies and a religious place of cult of Muses, that included the famous Library. For this reason, Hero claimed himself a pupil of Ctesibius, who was probably the first head of the Museum of Alexandria. Most of Hero’s writings appear as lecture notes for courses in mathematics, mechanics, physics and pneumatics [2]. In optics, Hero formulated the Principle of the Shortest Path of Light, principle telling that if a ray of light propagates from a point to another one within the same medium, the followed path is the shortest possible. -
CHAPTER 10 Advances in Understanding the Flow in A
CHAPTER 10 Advances in understanding the fl ow in a centrifugal compressor impeller and improved design A. Engeda Turbomachinery Lab, Michigan State University, USA. Abstract The last 60 years have seen a very high number of experimental and theoretical studies of the centrifugal impeller fl ow physics at government, industry and uni- versity levels, which have been extensively documented. As Robert Dean, one of the well-known impeller aerodynamists stated, “The centrifugal impeller is prob- ably the most complex fl uid machine built by man”. Despite this, it is still the widest used turbomachinery and continues to be a major research and develop- ment topic. Computational fl uid dynamics has now matured to the point where it is widely accepted as a key tool for aerodynamic analysis. Today, with the power of modern computers, steady-state solutions are carried out on a routine basis, and can be considered as part of the design process. The complete design of the impeller requires a detailed understanding of the fl ow in the impeller and aerody- namic analysis of the fl ow path and structural analysis of the impeller including the blades and the hub. This chapter discusses the developments in the understand- ing of the fl ow in a centrifugal impeller and the contributions of this knowledge towards better and advanced impeller designs. 1 Introduction Centrifugal compressors have the widest compressor application area. They are reliable, compact, and robust; they have better resistance to foreign object dam- age; and are less affected by performance degradation due to fouling. They are found in small gas turbine engines, turbochargers, and refrigeration chillers and are used extensively in the petrochemical and process industry. -
Comparison of Helicopter Turboshaft Engines
Comparison of Helicopter Turboshaft Engines John Schenderlein1, and Tyler Clayton2 University of Colorado, Boulder, CO, 80304 Although they garnish less attention than their flashy jet cousins, turboshaft engines hold a specialized niche in the aviation industry. Built to be compact, efficient, and powerful, turboshafts have made modern helicopters and the feats they accomplish possible. First implemented in the 1950s, turboshaft geometry has gone largely unchanged, but advances in materials and axial flow technology have continued to drive higher power and efficiency from today's turboshafts. Similarly to the turbojet and fan industry, there are only a handful of big players in the market. The usual suspects - Pratt & Whitney, General Electric, and Rolls-Royce - have taken over most of the industry, but lesser known companies like Lycoming and Turbomeca still hold a footing in the Turboshaft world. Nomenclature shp = Shaft Horsepower SFC = Specific Fuel Consumption FPT = Free Power Turbine HPT = High Power Turbine Introduction & Background Turboshaft engines are very similar to a turboprop engine; in fact many turboshaft engines were created by modifying existing turboprop engines to fit the needs of the rotorcraft they propel. The most common use of turboshaft engines is in scenarios where high power and reliability are required within a small envelope of requirements for size and weight. Most helicopter, marine, and auxiliary power units applications take advantage of turboshaft configurations. In fact, the turboshaft plays a workhorse role in the aviation industry as much as it is does for industrial power generation. While conventional turbine jet propulsion is achieved through thrust generated by a hot and fast exhaust stream, turboshaft engines creates shaft power that drives one or more rotors on the vehicle. -
Hero's Engine Build Instructions
OMAHA MAKER GROUP Explore Technology, Science, & Art 8410 K Street, #5 – Omaha, NE 68127 [email protected] www.omahamakergroup.org How to Make a Hero’s Steam Engine Description: An easy steam engine (Hero's engine) is constructed from a soda can, some thread, and a heat source. Burning fuel heats the engine to produce steam. The chemical energy in the fuel is converted to a rotation of the can, illustrating the conversion of chemical energy to thermal energy to mechanical energy. Materials: Unopened soda can, thread, a small nail or pin, thread, something to hang the can over the fuel, candle or “Sterno” fuel, lighter, gloves Step 1 Do this outside or over a sink. Use a pin or small nail to make a hole in the side of a soda can. The can must still be unopened. When you pull the pin out there will likely be some spray. Step 2 Empty the can through the pinhole. Depending on the soda in the can, shaking it will increase the pressure in the can causing the soda to come out faster. Don't worry if there's a little soda left when you're done. Step 3 Make another hole in the other side of the can. Step 4 Put the pin back in one of the holes and pull it down as shown in the photos below. This modifies the hole enough for the steam to later come out at an angle with respect to the can. Step 5 Do the same for the other hole, pulling the pin in the same direction with respect to the can.