The Historical Evolution of Turbomachinery
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Capabilities of Midlands Aerospace Companies 2010-2011 Midlands Capability for the World’S Aerospace Industry
Capabilities of Midlands Aerospace Companies 2010-2011 Midlands capability for the world’s aerospace industry The Midlands Aerospace Alliance is pleased to present you with the updated 20010-11 edition of our member capability directory. It has been designed to help you identify world-class Midlands partners and suppliers for your aerospace programmes and projects. The Midlands is home to one of the world’s biggest aerospace clusters, and aerospace systems designed and made in the Midlands can be found on the world’s most advanced aircraft. Leading names such as Aero Engine Controls, Goodrich, Meggitt, Moog and Rolls- Royce are major players in a region world-renowned for its core competency technologies: tTZTUFNTUIBUQPXFSBJSDSBGUoHBTUVSCJOFFOHJOFTBOEPUIFSQSPQVMTJPOTZTUFNT tTZTUFNTUIBUDPOUSPMUIFNPWJOHQBSUTPGBJSDSBGUBOEFOHJOFToFMFDUSJDBM NFDIBOJDBM electronic, hydraulic and pneumatic tTQFDJBMJTUNFUBMBOEDPNQPTJUFNBUFSJBMTUIBUFOBCMFUIFTFTZTUFNTUPQFSGPSNXJUI precision in exacting environments tTQFDJBMJTUFOHJOFFSJOHEFTJHOTFSWJDFT GBDUPSZFRVJQNFOUBOEUPPMJOH The Midlands business environment fosters the highest levels of innovation. Aerospace supply chains extend deep into our world-class advanced engineering economy. We access and invest in a dynamic skills base, with more than 45,000 skilled people working in the region’s aerospace industry. The mission of the Midlands Aerospace Alliance is to enhance cooperation between customers, suppliers and partners in the Midlands and globally, to help improve the performance of all our companies and organisations. We invite you to join us, using this directory to identify your new partners and suppliers. Dr Andrew Mair Chief Executive Midlands Aerospace Alliance The Midlands Aerospace Alliance (MAA) website provides further information and access to all MAA publications. The information in this directory is available and constantly updated, as a searchable database on the website. -
Capabilities of Midlands Aerospace Companies
Capabilities of Midlands Aerospace Companies 2017-2018 Midlands capability for the world’s aerospace industry he Midlands Aerospace Alliance is pleased to present you with the updated 2017-18 edition of our member capability directory T– which marks our fourteenth annual edition. It has been designed to help you identify world-class Midlands partners and suppliers for your aerospace programmes and projects. The Midlands is home to one of the largest aerospace clusters in the world. Aerospace technologies designed and made in the Midlands can be found on the world’s most advanced aircraft. Leading names such as Meggitt, Moog, Rolls-Royce and UTC Aerospace Systems are major players in a region renowned for its core competency technologies: • systems that power aircraft – gas turbine engines and other propulsion systems • systems that control the moving parts of aircraft and engines – electrical, mechanical, electronic, hydraulic and pneumatic • specialist metal and composite materials that enable these systems to perform with precision in exacting environments • specialist engineering design services, factory equipment and tooling. The Midlands business environment fosters the highest levels of innovation. Aerospace supply chains extend deep into our cluster’s world-class advanced engineering economy. We access and invest in a dynamic skills base, with more than 45,000 skilled people working in our aerospace industry. The mission of the Midlands Aerospace Alliance is to enhance cooperation between customers, suppliers and partners in the Midlands and globally, so that we can improve the performance of all our companies and organisations. We invite you to join us, using this directory to identify the new partners and suppliers you need to make your projects successful. -
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. -
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. -
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. -
High Temperature Parts
AGARD-CP-317 SMaintenance in Service of High Temperature Parts II- C)3 .3 L DISTRIBUTION AND AVAILABILITY ON BACK COVER Best Available Copy AGARD-CP-317 NORTH ATLANTIC TREATY ORC iZATION ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT (ORGANISATION DU TRAITE DE L'ATLANTIQUE NORD) AGARD Conference Proceedings No.317 MAINTENANCE IN SERVICE OF HIGH-TEMPERATURE PARTS & Papers presented at the 53rd Meeting of the AGARD Structures and Materials Panel held in Noordwijkerhout, the Netherlands 27 September-2 October 1981. THE MISSION OF AGARD Mhe mission of' AARI) is to bring together tile leading peloRalitie,, of the NATO nations in tile fields of Neiencv- and technology relating to aerospace for the following purpose-% of scientific and technical infonnation: SExchanging .Continuously stimulating advances in the aerospace sciences relevant to strengthening thie coniion defence posture. lnpro'ing the co-operation among member nations in aerospace researclh and developmenrt: Providing scientific and tccmt,-al advice and assistance to the North Atlantic Military Committee in the field of aerospace research and de'. elopnment Rendering scicultit'ic and tc:hmeal aslIstancc. is requested. to oher NATI) bodies and to nmember nations in connection with leýsvearh and devclopnielt problelm, in tfie acro.pace field: r!'tosiding assistance to inemhbter nations for the purpose of increasing their scie ntitiL anid tech1nical pot en tiall Recollmllmlending effectisc ways for tile melmjllber nLlat.tIlo,tO Use their research and development capabilities Ifm the conut on benefit of the NAI 0 co0in t1LtN - I'lhc highest authority wit hini A(.A RI) is the National Delegates Board cowisising of officially appointcd senior representati', fiom each member nation. -
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. -
Examination of Material Variation on the Life of Gas Turbine Backing-Up Renewable Energy Sources
IOSR Journal of Mechanical and Civil Engineering (IOSR-JMCE) e-ISSN: 2278-1684,p-ISSN: 2320-334X, Volume 16, Issue 1 Ser. IV (Jan. - Feb. 2019), PP 60-68 www.iosrjournals.org Examination of Material Variation on the Life of Gas Turbine Backing-Up Renewable Energy Sources Ezeddin Ali*, Suresh Sampath, Pericles Pilidis, Saleh Mohammed Department of Power and Propulsion, School of Aerospace, Transport and Manufacturing, Cranfield University, Cranfield, Bedfordshire, MK43 0AL, UK *Corresponding Author: Ezeddin Ali Abstract: Gas turbine life and efficiencydepend on the operating environment and material performance. Material selection is of prime importance to achieve high life and efficiency. This paper focuses on the study of the effect of material properties and variation in alloy composition ofa high- pressure turbine blade on gas turbine life when works in the flexible mode as a pick-up of renewable sources.A tool has been developed wherein different scenarios can be simulated to obtain engine life consumption factors. The engine life is examined according to the different material for different operating scenarios. It is observed that blade life is highly affectedby changing material properties and moreoverit is noted that the smallchange in the mass percentage of some constituent elements of an alloy results in a significant difference in HPT blade life. Keywords: Renewable Energy; Flexibility; Power Demand; Gas Turbines; Creep-LCF life; Material Properties ; Material composition ----------------------------------------------------------------------------------------------------------------------------- -
Superalloys for High Temperatures—A Primer
© 2002 ASM International. All Rights Reserved. www.asminternational.org Superalloys: A Technical Guide (#06128G) Chapter 1 Superalloys for High Temperatures—a Primer How and When to Use This Chapter in the field, check the table of contents and index for valuable insights into what you can It is always difficult to locate concise but find in each succeeding chapter. precise information on a subject. Executives and managers, particularly in industries using few superalloys, often need just basic infor- Some History mation with the least extraneous or amplify- ing data. Purchasing agents or communica- Designers have long had a need for tions experts need a modest knowledge base stronger, more corrosion-resistant materials to do their jobs more appropriately. The en- for high-temperature applications. The stain- gineer may need more detail but still just a less steels, developed and applied in the sec- quick refresher about alloy types and design ond and third decades of the 20th century, to start. The ability to lay hands on enough served as a starting point for the satisfaction practical information to solve problems or of high-temperature engineering require- answer questions about the superalloys is the ments. They soon were found to be limited basis for this book. The ability to know in their strength capabilities. The metallurgi- enough to ask questions and/or delve further cal community responded to increased needs into the superalloy field is the basis for this by making what might be termed ‘‘super-al- chapter! loys’’ of stainless varieties. Of course, it was The primer provided in this chapter sup- not long before the hyphen was dropped and ports such needs as those described previ- the improved iron-base materials became ously by providing a concise overview of the known as superalloys. -
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. -
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. -
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.