HYDROGEN TURBOMACHINERY Readying Pipeline Compressor Stations for 100% Hydrogen by PETER ADAM, RALF BODE, & MARKUS GROISSBOECK

Total Page:16

File Type:pdf, Size:1020Kb

HYDROGEN TURBOMACHINERY Readying Pipeline Compressor Stations for 100% Hydrogen by PETER ADAM, RALF BODE, & MARKUS GROISSBOECK SPECIAL REPORT: HYDROGEN HYDROGEN TURBOMACHINERY Readying Pipeline Compressor Stations For 100% Hydrogen BY PETER ADAM, RALF BODE, & MARKUS GROISSBOECK lue hydrogen, and more long-term, green The compression of hydrogen with turbo- hydrogen (i.e., hydrogen produced via compressors is more complicated. Although cen- Brenewable-powered water electrolysis), trifugal compressors for hydrogen recycle service holds enormous potential in helping the world have been used in downstream and petrochem- achieve its decarbonization goals. In particular, ical applications for decades, their efficiency is green hydrogen promises to bring flexibility lower than that of reciprocating compressors. and dispatchability to emissions-free power For a given impeller tip speed in a turbo- from intermittent sources like solar and wind. compressor, the pressure increase is directly Two central building blocks are needed to proportional to the molecular weight of the gas. make this reality: Hydrogen’s molecular weight is approximately 1) A sufficient source of blue/green hydro- 1/16th of methane, which means that achieving Figure 1: Sulfide-stress-cracked gen production a comparable pressure ratio to an existing nat- impeller from a plant where the 2) A needs-based storage and transportation ural gas line would require much higher impel- operator failed to specify network that can reliably and cost-effec- ler tip speeds or a much higher number of com- hydrogen sulfide in the gas. tively supply hydrogen to end-users. pressor stages in several compressor casings. Given the high costs and complexity associ- Impeller mechanical strength limits are ated with developing new transportation infra- directly correlated with tip speed. The maxi- structure, many pipeline operators and regula- mum allowable tip speed of the impeller varies tory bodies are asking the question, “How depending on the material used. Typically, these much effort would be required to repurpose material strength limitations are not a concern existing natural gas infrastructure to accommo- when designing compressors for service with air, date hydrogen?” CO2, or natural gas. In the case of low weight Let’s look at some specific changes required gas compositions, like hydrogen, however, they to make pipeline assets ready for hydrogen can be approached. Therefore, the design of a operation, focusing on the rotating equipment compressor for hydrogen operation is not dic- within compression stations. tated by aerodynamic limits, so much as it is by the impellers’ mechanical strength limits. HYDROGEN COMPRESSION Extensive studies on the design of blades Contrary to popular belief, the effective trans- and impeller geometry have shown that when port energy density of hydrogen in an existing high-strength titanium alloys are used, these gas pipeline is only slightly lower than that of stress levels can be reduced to allow for pressure natural gas. Therefore, the switch from natural ratios of up to 1.45:1 per stage. Therefore, a six- gas to hydrogen would have little impact on a stage machine with a total pressure ratio of 4:1 pipeline’s capacity to transport energy. However, with 100% hydrogen is technically possible. It the much lower molecular weight and heating can be assumed that the commercial availabil- value of hydrogen relative to natural gas have ity of these machines will increase in the com- implications on the type and design of rotating ing years when the market demands them. equipment used in compression stations. Overall, the extent to which compression For pipelines transporting 100% hydrogen, equipment will need to be adapted will depend reciprocating compressors are currently the most on the pipeline’s hydrogen content. If the admix- economical solution. With reciprocating com- ture is less than 10% hydrogen, the compressor pressors, the gas is efficiently compressed in the can be operated without any significant changes. cylinders. By increasing the number of cylinders When the admixture is under 40% hydro- and drive power, as well as a parallel arrange- gen, the compressor housing can be main- ment of compressors, a viable transport capacity tained, but the impellers and feedback stages of up to 750,000 Nm³/h can be achieved. and gears require adjustment. For pipelines 18 www.turbomachinerymag.com November/December 2020 • Turbomachinery International SPECIAL REPORT: HYDROGEN Figure 2: Hydrogen content possible in various Siemens Energy models. with greater than 40% hydrogen content, the nium impellers require reliable surface coatings. entire compressor must be replaced. Design changes can be made to reduce the likelihood of HIC in compressor impellers, for MATERIAL CONSIDERATIONS example, better interstage cooling. Ultimately, The switch from natural gas to hydrogen also however, better alloys must be developed with warrants consideration of the materials used for greater component reliability. rotating equipment and the physical pipelines. A test method has been developed to sim- Hydrogen embrittlement, or hydrogen-induced ulate high-speed impeller conditions in a tur- cracking (HIC), is a type of deterioration that bocompressor operating in pure hydrogen ser- occurs when atomic hydrogen diffuses into an vice. The technique will be presented at a alloy (see Figure 1). Depending on the steel technical conference late in 2020. It challenges grade and the operating conditions of the pipe- a historical specification limit within the oil line, this reduction in toughness can lead to the and gas production work. The goal is to pro- growth of existing crack-like defects, thus reduc- vide guidance on a new NACE standard for ing the service life of the line or component. testing HIC and identify fit-for-service envi- Although HIC can occur in pipeline walls, ronments, much like the limits for stress cor- it is unlikely as there are rarely dynamic pres- rosion cracking (SCC) in NACE MR0175 sure fluctuations during regular operation, and (Figure 3). no atomic hydrogen is produced during trans- port. It is generally accepted that both are TURBINE ADAPTATION required for the phenomenon to occur. HIC, Gas turbines that drive compressors draw their however, is a concern in impellers, which are drive energy directly from the line. They must be subject to stress due to high speeds. adapted accordingly to the hydrogen admixture. While the titanium alloys used for high- The combustion characteristics of hydrogen speed impellers offer excellent strength, they are differ from natural gas and other hydrocarbon subject to hydrogen embrittlement and HIC in fuels. This poses challenges for the design of hot the presence of high concentrations of hydrogen. gas path components. It is a challenge to control To avoid these deteriorating mechanisms, tita- the flame, maintain combustion system integ- Turbomachinery International • November/December 2020 www.turbomachinerymag.com 19 SPECIAL REPORT: HYDROGEN rity, and reach the desired level of emissions. Many gas turbines are already capable of operating on high percentages of hydrogen fuel, some at 100% hydrogen (Figure 2). The capa- bility of each unit depends on multiple factors, one being the type of combustion system the turbine utilizes, either dry-low emissions (DLE) or wet-low emissions (WLE). Existing turbines can be upgraded to allow increasing hydrogen content in the fuel or even work with 100% hydrogen in the future. In gas turbines with DLE combustion sys- tems, fuel and air are mixed before combustion to control flame temperature. This, in turn, controls the rate of emissions. The relative pro- portions of fuel and air are one of the driving factors for NOx and flame stability. Hydrogen’s higher reactivity poses challenges for the mix- ing technology in DLE systems, including: • Higher flame speeds increase the risk of the Figure 3: Siemens Energy proposes a test method where corrosion-resistant autoclaves are required to perform the tests on pre-stressed specimens at elevated flame burning closer to the injection points, pressures and temperatures. traveling back into mixing passages, or burn- ing too close to liner walls. This risk increases as hydrogen content rises and with increasing changes in the balance of volumetric flow combustion inlet and flame temperature. between the compressor and turbine. This issue • Hydrogen’s lower auto-ignition delay com- can typically be managed by making modifica- pared to methane increases the likelihood tions to the compressor or turbine. of igniting the fuel in the mixing passages. • Changes to thermoacoustic noise patterns THE ROAD AHEAD because of the different flame heat release A building block of a low-carbon energy system distribution can lower component life. is a needs-based storage/transportation network DLE combustion systems are available using to supply hydrogen to end-users. In parts of swirl stabilized flames combined with lean pre- Europe, establishing a hydrogen infrastructure mixing that can achieve low NOx emissions may be possible with little effort. The pipeline without diluting the fuel. Hardware and control networks can gradually be converted to hydro- system changes are also required for higher gen operation with an investment of an esti- hydrogen fuel content to allow systems to operate mated 10-15% of the cost of new construction. ■ safely, meet NOx emissions limits, and manage varying fuel compositions. A goal has been set of making industrial turbines with DLE capable of Peter Adam is Vice President burning 100% hydrogen by 2023. Business Development for Oil Non-DLE technology
Recommended publications
  • Engineering the Future – Since 1758
    MAN Energy Solutions MAN Energy Solutions Product range und product centres 3 Steinbrinkstr. 1 2 46145 Oberhausen, Germany Turbomachinery P + 49 208 692-01 F + 49 208 692-021 [email protected] www.man-es.com Factories Engineering turbomachinery Turbo- the future – Bangalore, India MAN Turbomachinery India Private Limited since 175 8 Plot No. 113 | Jigani link Road KIADB Industrial Area | Jigani | 560105 Bangalore, India Phone +91 80 6655 2200 | Fax +91 80 6655 2222 machinery We are MAN Energy Solutions SE, the force of Berlin, Germany innovation behind the world’s leading large-bore MAN Energy Solutions SE engines and turbomachinery for marine and Egellsstr. 21 13507 Berlin, Germany stationary applications. Our home is in Augsburg, Phone +49 30 440402-0 | Fax +49 30 440402-2000 Germany. But we are also close to you, in over 100 countries, with more than 15,000 employees Changzhou, China who dedicate each workday to our customer’s MAN Diesel & Turbo China Production Co. Ltd. Fengming Road 9, Wujin High-Tech Industrial Zone satisfaction. 213164 Changzhou, P. R. China Phone +86 519 8622-7001 | Fax +86 519 8622-7002 Our products are an integral part of Between 1893 and 1897, Rudolf custom, fully integrated train solutions most energy and transportation solu- Diesel and a group of M.A.N. engineers that are unsurpassed in performance, Deggendorf, Germany tions that surround you every day. We developed the first diesel engine in efficiency and reliability. MAN Energy Solutions SE produce world-class marine propulsion Augsburg, and in 1904 we produced Werftstr. 17 systems, turbomachinery for the our first steam turbine in Oberhausen.
    [Show full text]
  • Modelling of a Turbojet Gas Turbine Engine
    The University of Manchester Research Modelling of a turbojet gas turbine engine Document Version Accepted author manuscript Link to publication record in Manchester Research Explorer Citation for published version (APA): Klein, D., & Abeykoon, C. (2015). Modelling of a turbojet gas turbine engine. In host publication (pp. 198-204) Published in: host publication Citing this paper Please note that where the full-text provided on Manchester Research Explorer is the Author Accepted Manuscript or Proof version this may differ from the final Published version. If citing, it is advised that you check and use the publisher's definitive version. General rights Copyright and moral rights for the publications made accessible in the Research Explorer are retained by the authors and/or other copyright owners and it is a condition of accessing publications that users recognise and abide by the legal requirements associated with these rights. Takedown policy If you believe that this document breaches copyright please refer to the University of Manchester’s Takedown Procedures [http://man.ac.uk/04Y6Bo] or contact [email protected] providing relevant details, so we can investigate your claim. Download date:02. Oct. 2021 Modelling of a Turbojet Gas Turbine Engine Dominik Klein Chamil Abeykoon Division of Applied Science, Computing and Engineering, Division of Applied Science, Computing and Engineering, Glyndwr University, Mold Road, LL11 2AW, Wrexham, Glyndwr University, Mold Road, LL11 2AW, Wrexham, United Kingdom United Kingdom E-mail: [email protected] E-mail: [email protected]; [email protected] Abstract—Gas turbines are one of the most important A.
    [Show full text]
  • The Effect of the Process on Turbomachinery Reliability)
    “DO AS I SAY” (THE EFFECT OF THE PROCESS ON TURBOMACHINERY RELIABILITY) by William E. Forsthoffer President Forsthoffer Associates Inc., Washington Crossing, Pennsylvania William E. (Bill) Forsthoffer spent six years at the Delaval Turbine Company, as Manager of Compressor Project Engi- neering, where he designed and tested centrifugal pumps and compressors, gears, steam turbines, and rotary (screw) pumps. Mr. Forsthoffer then joined the Mobil Research and Development Corporation. For five years, he directed the application, selection, design, testing, site precommis- sioning, and startup of the Yanbu Petrochemical complex in Yanbu, Saudi Arabia. Following that, he returned to MRDC and established a technical service program for Mobil affiliates to provide application, troubleshooting, and Figure 1. Diagram of Centrifugal Pump. training services for rotating equipment. He left Mobil in 1990 to found his own company, Forsthoffer Associates, Inc., to provide training, critical equipment selection, and troubleshooting services to the refining, petrochemical, utility, and gas transmission industries. Mr. Forsthoffer is a graduate of Bellarmine College with a B.A. degree (Mathematics) and from the University of Detroit with a B.S. degree (Mechanical Engineering). ABSTRACT This tutorial examines the primary cause of lower than expected reliability in turbomachines, the effect of the process on machinery component life. Over 95 percent of the rotating equipment installed in any refinery, petrochemical, or gas plant is the dynamic or “turbo” type. Their characteristics are limited energy output and variable flow rate determined by process energy requirements. INTRODUCTION Figure 2. Centrifugal Pump Component Damage and Causes. The objective of this tutorial is to emphasize the importance of understanding the effect of the process on turbomachinery reliability.
    [Show full text]
  • Turbomachinery Technology for High-Speed Civil Flight
    4 NASA Technical Memorandum 102092 . Turbomachinery Technology for High-speed Civil Flight , Neal T. Saunders and Arthur J. Gllassman Lewis Research Center Cleveland, Ohio Prepared for the 34th International Gas Turbine Aepengine Congress and Exposition sponsored by the American Society of Mechanical Engineers Toronto, Canada, June 4-8, 1989 ~ .. (NASA-TH-102092) TURBOHACHINERY TECHPCLOGY N89-24320 FOR HIGH-SPEED CIVIL FLIGHT (NBSEL, LEV& Research Center) 26 p CSCL 21E Unclas G3/07 0217641 TURBOMACHINERY TECHNOLOGY FOR HIGH-SPEED CIVIL FLIGHT Neal T. Saunders and Arthur J. Glassman ABSTRACT This presentation highlights some of the recent contributions and future directions of NASA Lewis Research Center's research and technology efforts applicable to turbomachinery for high-speed flight. For a high-speed civil transport application, the potential benefits and cycle requirements for advanced variable cycle engines and the supersonic throughflow fan engine are presented. The supersonic throughf low fan technology program is discussed. Technology efforts in the basic discipline areas addressing the severe operat- ing conditions associated with high-speed flight turbomachinery are reviewed. Included are examples of work in internal fluid mechanics, high-temperature materials, structural analysis, instrumentation and controls. c INTRODUCTION Future Emphasis Shifting to High-speed Flight Two years ago, the aeronautics community commemorated the 50th anniversary of the first successful operation of a turbojet engine. This remarkable feat by Sir Frank Whittle represents the birth of the turbine engine industry, which has greatly refined and improved Whittle's invention into the splendid engines that are flying today. NASA, as did its predecessor NACA, has assisted indus- try in the creation and development of advanced technologies for each new gen- eration of engines.
    [Show full text]
  • Application Note Acoustic Excitation of Turbomachinery Blisks
    www.mpihome.com Application Note Acoustic Excitation of Turbomachinery Blisks ■ Generating an engine order excitation ■ m+p’s acoustic blisk excitation software ■ Analyzing the dynamic responses of ■ m+p Analyzer for data capture and post-processing turbomachinery blisks ■ m+p VibRunner acquisition hardware ■ Four sine excitation modes During operation wind, gas and steam turbine blades are subject to high dynamic forces introduced by the working fluid. In order to assess the structural health of the blades, dynamic analyses are carried out in laboratory tests. Highly specialized test rigs are designed for analyses of blades in rotating and stationary operating conditions. Especially for stationary tests, it is crucial to artificially replicate the typical excitations acting on the rotor blades during operation, known as engine order excitation. m+p international designed a software package which enables engineers to generate an engine order excitation and analyze the dynamic responses of the turbomachinery blisks in the safety of the laboratory. Application Note Acoustic Excitation of Turbomachinery Blisks 1 Background: During operation the working fluid acts on the rotating turbine blades, creating a pulsating pressure field. Circumferentially expanding this pressure field yields a harmonic series whose coefficients are called engine orders. Basically, an engine order describes the number of sine waves traveling along the circumference of the rotor (figure 1). The corresponding excitation frequency is the product of the rotational speed and the specific engine order, EO. Only a few engine orders will be encountered during operation. Thus, it is often possible to reduce the whole pressure field to a single engine order. m+p international’s acoustic blisk excitation software replicates this engine order excitation by controlling the given actuators accordingly.
    [Show full text]
  • Selection of Turbomachinery-Centrifugal Compressors
    View metadata, citation and similar papers at core.ac.uk brought to you by CORE provided by Texas A&M Repository SELECTION OF TURBOMACHINERY-CENTRIFUGAL COMPRESSORS by Gary A. Ehlers Senior Supervising Engineer Ralph M. Parsons Company Pasadena, California INTRODUCTION Gary A. Ehlers, is Senior Supervising Selection of a centrifugal compressor starts with performance Engineer in the Rotating Equipment Engi­ calculations. After basic machine performance is determined, neering group ofthe Engineering Department the mechanical construction is addressed. The primary areas of at Ralph M. Parsons Company, Pasadena, concern are metallurgy, shaft sealing and rotordynamics. California. He supervises the activities re­ Rotordynamics analysis (RDA) of turbomachinery designs lated to the rotating equipment engineering should be made during selection. A lateral critical speed study on projects. Thetypes of machineryrespon­ includes undamped critical speed analysis, plot of the undamped sibilities include centrifugaland reciprocat­ critical speeds as a functionof stiffness, synchronous unbalance ing compressors, axial flow compressors, response analysis, and stability analysis. The stability analysis is steam and gas turbines, centrifugal and concerned with all calculated subharmonic, self-excited vibra­ reciprocating pumps, and gas expanders. tions of the rotor. Oil whirl is one such common example of He has been employed at Parsons for the last 20years and previously subharmonic instability of concern in design of the rotor bearing at Worthington Compressor and Engine International as an Appli­ support of turbomachinery. Other instabilities result from dis­ cation Engineer in power and process marketing. turbing/destabilizing forces from aerodynamic sources or shaft Hehas worked on primarily refinerytype projects domestically,in seal design. the Middle East, and Asia and on cogeneration and oil production Rotordynamics of a centrifugal compressor with oil film seals type projects.
    [Show full text]
  • An Investigation of Turbomachinery Concepts for an Isothermal Compressor Used in an S-CO2 Bottoming Cycle
    The 6th International Supercritical CO2 Power Cycles Symposium March 27 - 29, 2018, Pittsburgh, Pennsylvania An Investigation of Turbomachinery Concepts for an Isothermal Compressor Used in an S-CO2 Bottoming Cycle Jin Young Heo Seong Gu Kim Jeong Ik Lee PhD Candidate PhD Candidate Associate Professor KAIST KAIST KAIST Daejeon, South Korea Daejeon, South Korea Daejeon, South Korea ABSTRACT Various technology options are under progress to investigate the benefits of using an isothermal compressor for the s-CO2 bottoming cycle applications. In previous works, the partial heating cycle has been investigated to show that there can be great increase in total net work when an isothermal compressor is applied to the system. The research covers the investigation on mainly three different turbomachinery concepts to realize the isothermal compressor, the radial-type compressor with impeller cooling, the multistage compressor with intercoolers, and the axial-type compressor with rotor and stator cooling. As a result, the concepts are mainly limited by the realistic cooling flux level that can be applied to the heat transfer surface, but the multistage compressor with intercoolers may be a viable candidate as long as the pressure drop in intercoolers remains low. INTRODUCTION To combat the issue of global warming, the development of various technologies is currently under progress to improve the performance of the conventional waste heat recovery systems. Various sources of waste heat, from glass manufacturing, steel manufacturing, and gas turbine exhaust, can be recovered to generate electricity by adopting another power cycle [1]. Among the candidates to enhance the current performance limits, the supercritical CO2 power cycle (s-CO2 cycle) has been considered a viable option to replace the conventional steam Rankine cycle, the system most often utilized for the bottoming cycle.
    [Show full text]
  • Gas Turbines in Simple Cycle and Combined Cycle Applications
    GAS TURBINES IN SIMPLE CYCLE & COMBINED CYCLE APPLICATIONS* Gas Turbines in Simple Cycle Mode Introduction The gas turbine is the most versatile item of turbomachinery today. It can be used in several different modes in critical industries such as power generation, oil and gas, process plants, aviation, as well domestic and smaller related industries. A gas turbine essentially brings together air that it compresses in its compressor module, and fuel, that are then ignited. Resulting gases are expanded through a turbine. That turbine’s shaft continues to rotate and drive the compressor which is on the same shaft, and operation continues. A separate starter unit is used to provide the first rotor motion, until the turbine’s rotation is up to design speed and can keep the entire unit running. The compressor module, combustor module and turbine module connected by one or more shafts are collectively called the gas generator. The figures below (Figures 1 and 2) illustrate a typical gas generator in cutaway and schematic format. Fig. 1. Rolls Royce RB211 Dry Low Emissions Gas Generator (Source: Process Plant Machinery, 2nd edition, Bloch & Soares, C. pub: Butterworth Heinemann, 1998) * Condensed extracts from selected chapters of “Gas Turbines: A Handbook of Land, Sea and Air Applications” by Claire Soares, publisher Butterworth Heinemann, BH, (for release information see www.bh.com) Other references include Claire Soares’ other books for BH and McGraw Hill (see www.books.mcgraw-hill.com) and course notes from her courses on gas turbine systems. For any use of this material that involves profit or commercial use (including work by nonprofit organizations), prior written release will be required from the writer and publisher in question.
    [Show full text]
  • Turbomachinery Technology for Reduced Fuel Burn
    NASA SBIR 2016 Phase I Solicitation A1.07 Propulsion Efficiency - Turbomachinery Technology for Reduced Fuel Burn Lead Center: GRC System and technology studies have indicated that advanced gas turbine propulsion will remain critical for future subsonic transports. Turbomachinery includes the rotating machinery in the high and low pressure spools, transition ducts, purge and bleed flows, casing and hub. We are interested in traditional gas turbine turbomachinery, as well as in innovative concepts as exo-skeletal engines, intercooled gas turbines, cooled cooling air, waste heat recovery, and other concepts. NASA is looking for improvement in aeropropulsive efficiency. Areas of interest include: Improved components of current architectures and cycles, novel components and cycles to improve cycle limits, and novel architectures to improve mission efficiency limits. In the compression system, advanced concepts and technologies are required to enable higher overall pressure ratio, high stage loading and wider operating range. In the turbine, the very high cycle temperatures demanded by advanced engine cycles place a premium on the cooling technologies required to ensure adequate life of the turbine component. New capabilities as well as challenges are provided with expected increased use of ceramic matrix composites (CMC’s). Reduced cooling flow rates and/or increased cycle temperatures enabled by these technologies have a dramatic impact on the engine performance. Such improvements will enable reduced fuel burn, reduced weight and part count, and will enable advanced variable cycle engines for various missions. Innovative proposals in the following turbomachinery and heat transfer areas are solicited: Small core turbomachinery - Higher fan Bypass Ratio (BPR) will require more compact engine core sizes rather than by growing the fan diameter, resulting in large tip/endwall and purge flow losses.
    [Show full text]
  • Aero-Thermal Analysis and Design of Turbomachinery Blades Using Multi-Stage Adjoint Methods
    UNIVERSIDADE DE LISBOA INSTITUTO SUPERIOR TÉCNICO Aero-thermal analysis and design of turbomachinery blades using multi-stage adjoint methods Simão Santos Rodrigues Supervisor: Doctor André Calado Marta Thesis approved in public session to obtain the PhD Degree in Aerospace Engineering Jury final classification: Pass with Distinction 2019 UNIVERSIDADE DE LISBOA INSTITUTO SUPERIOR TÉCNICO Aero-thermal analysis and design of turbomachinery blades using multi-stage adjoint methods Simão Santos Rodrigues Supervisor: Doctor André Calado Marta Thesis approved in public session to obtain the PhD Degree in Aerospace Engineering Jury final classification: Pass with Distinction Jury Chairperson: Doctor Hélder Carriço Rodrigues, Instituto Superior Técnico, Universidade de Lisboa Members of the Committee: Doctor José Arnaldo Pereira Leite Miranda Guedes, Instituto Superior Técnico, Universidade de Lisboa Doctor João Eduardo de Barros Teixeira Borges, Instituto Superior Técnico, Universidade de Lisboa Doctor Pedro Vieira Gamboa, Faculdade de Engenharia, Universidade da Beira Interior Doctor Miguel Ângelo Rodrigues Silvestre, Faculdade de Engenharia, Universidade da Beira Interior Doctor André Calado Marta, Instituto Superior Técnico, Universidade de Lisboa Doctor Sriram Shankaran, GE Aviation, EUA Funding Institutions Fundação para a Ciência e a Tecnologia 2019 Acknowledgments I would like to thank my supervisor Professor André Calado Marta for providing the the opportunity to follow this PhD in this project and for his support and knowledgeable words of advice during these past years. I would also like to thank General Electric for providing the opportunity to develop this work on their in-house solver and their funding of the first year of my studies through ID- MEC and Fundação para a Ciência e Tecnologia (FCT), Portugal, for the PhD scholarship SFRH/BD/97521/2013.
    [Show full text]
  • How to Select Turbomachinery for Your Application
    How to Select Turbomachinery For Your Application 6325 West 55th Avenue Arvada, CO 80002 Kenneth E. Nichols P.E. How to Select Turbomachinery For Your Application Kenneth E. Nichols P.E. Barber-Nichols Inc. Abstract: Turbomachinery finds many applications in commercial, industrial, military, and aerospace applications. These turbomachines include pumps, compressors, fans and blowers, and turbines for prime movers. Other applications include turbines for generating shaft power. These turbines can be associated with closed Rankine or Brayton cycles for long duration power systems or open cycles where the driving fluid is expended to the atmosphere. The paper describes a method of predicting turbomachinery performance using dimensionless parameters of specific speed and specific diameter. This approach provides the preliminary designer information as to the best type of machine for an application. In addition, it provides parameters to determine the size of the machine. It also aids in the selection of the optimum speed for a turbine or pump, combination turbopump applications, or turbine-compressor matching in a Brayton cycle power system. Turbines that must operate over a range of power levels or with a changing exhaust pressure can be designed to have a broad performance range. Design techniques to improve the performance range of turbines are discussed. The paper presents examples of turbomachinery that have been designed for space applications. These include the turbines for a 15 KW closed Rankine Cycle Solar Power System, a hydrogen- oxygen fueled open cycle power system for short duration manned space missions, and a turbine driven hydraulic pump. Discussion: Through the technique known as dimensional analysis, the similarity parameters specific speed NS, specific diameter DS, Reynolds number Re*, and suction specific speed S, or Mach number Ma*, are derived which serve as convenient parameters for presenting the performance criteria of turbomachines.
    [Show full text]
  • Pumps, Fans and Turbines
    Turbomachinery { pumps, fans and turbines Fluid machinery Eciency Characteristic curves Turbomachinery { pumps, fans and turbines Pump/pipe systems SOE2156: Fluids Lecture 4 Pump/pipe systems Pump/pipe systems Turbomachinery { pumps, fans and turbines Fluid machinery Fluid machinery Fluid machine { a device exchanging energy (work) between a Eciency uid and a mechanical system. Characteristic curves In particular : a turbomachine is a device using a rotating Pump/pipe mechanical system. systems Pump/pipe The ow of energy can be in either direction : systems 1 Turbine ! the ow does work on the mechanical system Pump/pipe systems (i.e. energy is transmitted from the uid to the mechanical system) 2 Pumps, fans, compressors, blowers ! the mechanical system does work on the ow (i.e. energy is transmitted from the rotor to the uid) Contact between the mechanical and uid parts is via an impeller Turbomachinery { pumps, fans and turbines Types of turbine Fluid machinery Impulse turbine { e.g. Pelton wheel. Free jet of water impinges Eciency on revolving impeller (runner) and is de ected. Characteristic Change of momentum of water change of curves momentum (torque) for impeller. Pump/pipe systems Total available head converted into kinetic energy Pump/pipe systems head ! work done on impeller. Pump/pipe Reaction turbine { e.g. centrifugal, Kaplan turbine. Turbine systems completely enclosed in water, which can be pressurised. Shape of blades forces change in momentum of water { torque on blades { power. Reaction turbine uses available pressure
    [Show full text]