P R a T T & W H I T N
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DUMS I{ATIONALADVISORY COMMITTEE for AERONAUTICS
,- TECHN1CAL MEMO.RAI?DUMS i{ATIONAL ADVISORY COMMITTEE FOR AERONAUTICS. No. 309 —. LIGHT AEROPLANE ENGINE DEVELOPIM1lT. ... By Lieut. -Col. L. F. R, Fell. (Paper read at a joint meeting of the Royal Aeronautical Society and of the In8tit~~tion of Au_kornobileEngineersj February 19, 1925.) ..,’ —.—->... ,.. ,, April, 1925. —- .-— — 31176014410519 “LIGHT AEROPLANZ ENGINE.D~EIJOp~JE]TT~* ByLieut.-Col.-F ..F. R. Fell. It has frequently been stated and written that in order to popularize li,ght aircraft the”first essential is the production of a reliable engine capable of being easily maintained and.h,av- ing a long lif~, at the same time selling at a low figure. In the first part of this lecture it” is desired to point out the difficulties in the way of realizing this ideal before re~krking on the claims of the various types for adoption. Difficulties in the way of the Production of Light Aircraft Engines In the first place the public, and even aircraft designers, have been misled as to the t-ypeof engine that”is required by statements made in the nontechnical and sclilitcchnicalPress to the effect that it is possible to fly an aeroplane satisfactorily with a motorcycle engine. At this stage it is desired to state quite definitely that this is’impossible, as figures, which will be given later, cl-earlyindicate. T’nemethod of rating on capacity, instead of on a “~. basis - the normal manner for aircraft engines - has also caused—. consid- * Paper read at a joint mcetingof the Roycl Aeronautical Society and of the Institution of--ktomobile Engineers, February N, 19250 .— .-— .... -
Pratt & Whitney Overview
Pratt & Whitney Pratt & Whitney, a United Technologies Corp. company (NYSE:UTX), is a world leader in the design, manufacture and service of aircraft engines, industrial gas turbines and space propulsion systems. Pratt & Whitney reported an operating profit of $2.0 billion in 2011 on revenues of $13.4 billion. The company has approximately 36,000 employees who support more than 11,000 customers around the world. Pratt & Whitney was founded in Hartford, Conn., MAJOR PRODUCTS COMPANY PROFILE in 1925 by Frederick Rentschler. Pratt & Whitney’s first aircraft engine was the 410-horsepower, air- Commercial Engines Financials cooled Wasp, which delivered unprecedented PW2000 for Boeing 757 Revenues: $13.4 billion (2011) performance and reliability for the time and PW4000 for Boeing 747, 767 and 777 Operating Profit: $2.0 billion (2011) transformed the aviation industry. Pratt & Whitney and Airbus A300, A310 and A330 has been leading change ever since. PW6000 for Airbus A318 Current Employment GP7000 for Airbus A380 Approximately 36,000 employees worldwide Pratt & Whitney develops game-changing V2500 for Airbus A319, A320 and A321 technologies for the future, such as the PurePower PW1000G engine for Customers PurePower® PW1000G engine, with patented Bombardier CSeries Aircraft More than 500 customers operate Geared Turbofan™ technology, for next generation Mitsubishi Regional Jet Pratt & Whitney large commercial engines of passenger aircraft. Pratt & Whitney Global Airbus A320neo and in 136 countries. Service Partners, the company’s worldwide large Irkut MC-21 Aircraft commercial engine maintenance, repair and Nearly 30 customers operate aircraft overhaul network, provides innovative services Military Engines powered by Pratt & Whitney military that delight customers around the globe. -
FINAL PROJECT “Design a Radial Engine”
FINAL PROJECT “Design a Radial Engine” Project and Engineering Department Student: Maxim Tsankov Vasilev Tutors: Dr. Pedro Villanueva Roldan Dk. Pamplona, 27.07.2011 1 Contents I. Radial Engine ................................................................................................................................ 5 II. History of the Radial Engine ........................................................................................................... 7 III. Radial engines nowadays ......................................................................................................... 15 I. Kinematical and Dynamical Calculations ..................................................................................... 18 1. Ratio .............................................................................................................................................. 18 2. Angular velocity ............................................................................................................................ 18 3. Current Piston Stroke ................................................................................................................... 18 4. Area of the piston head: ............................................................................................................... 21 5. Different forces acting on the master-rod: .................................................................................. 21 II. Strength calculations of some of the major parts of the engine................................................ -
Master of Engineering Thesis Modelling a Novel Orbital Ic
Department of Mechanical Engineering University of Canterbury Te Whare Wānanga o Waitaha Telephone: +64-3-366 7001 Private Bag 4800 Facsimile: +64-3-364 2078 Christchurch 8020, New Zealand Website: www.mech.canterbury.ac.nz MASTER OF ENGINEERING THESIS MODELLING A NOVEL ORBITAL IC ENGINE TO AID FURTHER DESIGN By Lindsay Muir BE (Hons) 31 August 2014 Requirements for the degree of MASTER OF ENGINEERING IN MECHANICAL ENGINEERING Approved by: Dr Dirk Pons, Project Supervisor 1 COPYRIGHT LINDSAY MUIR 24/10/2015 0 TABLE OF CONTENTS 1 INTRODUCTION ................................................................................................ 11 1.1 Scenario ............................................................................................................. 11 1.2 Purpose .............................................................................................................. 13 1.3 Scope ................................................................................................................. 14 2 BACKGROUND .................................................................................................. 15 2.1 The Radial and Rotary engine .......................................................................... 15 2.1.1 History ............................................................................................................. 15 2.1.2 Multi-row radials .............................................................................................. 18 2.1.3 Diesel radials ................................................................................................. -
The History of the Boeing Model 40 a Contribution to Corporate and Air Line Growth
The History of the Boeing Model 40 A Contribution to Corporate and Air Line Growth Boeing Historical Archives Boeing Historical Archives 45th AIAA Aerospace Sciences Meeting and Exhibit January 7-10, 2008 Grand Serra Resort Hotel Reno, Nevada Mike Lavelle, Associate Fellow AIAA Fellow, Royal Aeronautical Society Museum of Flight Seattle, Washington Dedication This paper is dedicated to Mr. William E. Boeing Jr. for his stewardship and continuous support of aviation/aerospace education. Author and Mr. William E. Boeing Jr. Boeing Model 40B Roll Out Wenatchee, WA. October 6, 2007 This paper is copy write by author and The American Institute of Aeronautics and Astronautics 2008 2 Acknowledgements This paper has been supported in one way or another by many people with whom I work. I like to thank them all for their time, assistance and feedback they provided while the paper was in the process of being researched and written. The Museum of Flight Staff • Alison Bailey - Associate Director of Development Museum of Flight • Andrew Boike - Annual Fund Coordinator Museum of Flight • Meredith Downs – Photo Archivist Museum of Flight • John Little – Exhibits Technician and Aviation Historian • Ernst Marris – Security Officer Museum of Flight • Dennis Parks – Director of Collections Museum of Flight • Katherine Williams – Archivist Dahlberg Center for Military Aviation History, Museum of Flight The Boeing Company Archives Staff • Mike Lombardi - The Boeing Company – Corporate Historian • Tom Lubbesmeyer – Boeing Historian \Archivist Museum of Flight Trustee • Brien S. Wygle – Retired Boeing Vice President and Company Test Pilot I would especially like to thank Andrew Boike and Brien Wygle who spent their own time helping with the papers editing and format. -
A Case Study of Pratt and Whitney Aircraft's Commercial Spares Planning
Communications of the IIMA Volume 6 Issue 3 Article 2 2006 A Case Study of Pratt and Whitney Aircraft's Commercial Spares Planning Vincent A. Mabert Indiana University Ashok Soni Indiana University Gerard Campbell Fairfield University Follow this and additional works at: https://scholarworks.lib.csusb.edu/ciima Part of the Management Information Systems Commons Recommended Citation Mabert, Vincent A.; Soni, Ashok; and Campbell, Gerard (2006) "A Case Study of Pratt and Whitney Aircraft's Commercial Spares Planning," Communications of the IIMA: Vol. 6 : Iss. 3 , Article 2. Available at: https://scholarworks.lib.csusb.edu/ciima/vol6/iss3/2 This Article is brought to you for free and open access by CSUSB ScholarWorks. It has been accepted for inclusion in Communications of the IIMA by an authorized editor of CSUSB ScholarWorks. For more information, please contact [email protected]. A Case Study of Pratt and Whitney Aircraft's Commercial Spares Planning Mabert, Son & Campbell A Case Study of Pratt and Whitney Aircraft's Commercial Spares Planning^ Vincent A. Mabert Kelley School of Business, Indiana University, Bloomington, IN 47405 [email protected] Ashok Soni Kelley School of Business, Indiana University, Bloomington, IN 47405 [email protected] Gerard Campbell Charles F. Dolan School of Business, Fairfield University, Fairfield, CT 06824 [email protected] ABSTRACT This case study, which can be used as a teaching case, deals with jet engine spare parts planning at Pratt and Whitney Aircraft Company, a division of United Technologies Corporation. The case includes background on the company's history and an overview of their jet engine manufacturing operations. -
Wankel Engine
R -1 it ' ..^ . A SURVEY OF ROTARY TYPE INTERNAL COMBUSTION 1 ENGINES WITH PARTICULAR EMPHASIS , ON THE N.S.U.-WANKEL ENGINE \ 1 J . by , '4 HIRIYUR VEERANNA CHANDRA SHJilKA i \ B. S., Mysore University, India, 1958 1 1 \ \ •1 A MASTER ' S REPORT submitted in partial fulfillment of the ; requirements for the degree • 1 MASTER OP SCIENCE Department of Mechanical Engineering KANSAS STATE UNIVERSITY :i 1 Manhattan, Kansas 1 1966 V 1 "J Approved hy: 1 OM,. a/ Hy^^^Oa^ y Major i^ofessor .1 LP TABLE OP CONTENTS ^ ^ ^-, NOMENCLATURE iii INTRODUCTION 1 REVIEW OP LITERATURE ....',. 3 Rotary Piston Engines .... $ Rotary Cylinder Engines 11 Vane- type Engines 12 'Cat-and-mouse' Engines 13 N.S.U.-WANKEL ENGINE 1^ Optimum Shape l8 Principle of Operation 21 Engine Cycle 23 First Prototype ..... 25 COMPARISON WITH RECIPROCATING ENGINE 26 Combustion 26 Port Area 26 P-V Diagram 2? Sealing System 30 Cooling 32 DESIGN OP N.S.U.-WAMEL ENGINE 32 Output 2>k- Swept Volume 35 Engine Geometry - .•' 37 CONCLUSIONS . i^o ACKNOWLEDGMENT [^1 REFERENCES |j_2 Ill NOMENCLATURE e = eccentricity G = center of gravity h = thickness ,. N = rotational speed Pme ~ inean effective pressure P = output r = pitch circle radius R = generating radius V^ = volume of the chamber i_ = compression ratio ^ = angle of obliquity P = angle described by the line passing through the point of contact of the meshing gears and the center of the cir- cular hole in the rotor, with reference to a fixed axis 9 = angle of inclination of the line joining the center of the stator and the centroid of the rotor to the x-axis ,' ..• ^ = leaning angle , INTRODUCTION The conventional reciprocating internal combustion engine suffers from several fundamental shortcomings. -
Aircraft Propulsion C Fayette Taylor
SMITHSONIAN ANNALS OF FLIGHT AIRCRAFT PROPULSION C FAYETTE TAYLOR %L~^» ^ 0 *.». "itfnm^t.P *7 "•SI if' 9 #s$j?M | _•*• *• r " 12 H' .—• K- ZZZT "^ '! « 1 OOKfc —•II • • ~ Ifrfil K. • ««• ••arTT ' ,^IfimmP\ IS T A Review of the Evolution of Aircraft Piston Engines Volume 1, Number 4 (End of Volume) NATIONAL AIR AND SPACE MUSEUM 0/\ SMITHSONIAN INSTITUTION SMITHSONIAN INSTITUTION NATIONAL AIR AND SPACE MUSEUM SMITHSONIAN ANNALS OF FLIGHT VOLUME 1 . NUMBER 4 . (END OF VOLUME) AIRCRAFT PROPULSION A Review of the Evolution 0£ Aircraft Piston Engines C. FAYETTE TAYLOR Professor of Automotive Engineering Emeritus Massachusetts Institute of Technology SMITHSONIAN INSTITUTION PRESS CITY OF WASHINGTON • 1971 Smithsonian Annals of Flight Numbers 1-4 constitute volume one of Smithsonian Annals of Flight. Subsequent numbers will not bear a volume designation, which has been dropped. The following earlier numbers of Smithsonian Annals of Flight are available from the Superintendent of Documents as indicated below: 1. The First Nonstop Coast-to-Coast Flight and the Historic T-2 Airplane, by Louis S. Casey, 1964. 90 pages, 43 figures, appendix, bibliography. Price 60ff. 2. The First Airplane Diesel Engine: Packard Model DR-980 of 1928, by Robert B. Meyer. 1964. 48 pages, 37 figures, appendix, bibliography. Price 60^. 3. The Liberty Engine 1918-1942, by Philip S. Dickey. 1968. 110 pages, 20 figures, appendix, bibliography. Price 75jf. The following numbers are in press: 5. The Wright Brothers Engines and Their Design, by Leonard S. Hobbs. 6. Langley's Aero Engine of 1903, by Robert B. Meyer. 7. The Curtiss D-12 Aero Engine, by Hugo Byttebier. -
Counterpoise Defined Final
A WHITE PAPER DESCRIBING THE INTERNAL COMBUSTION ENGINE’S FINAL MODIFICATION THE COUNTERPOISE BI-RADIAL ENGINE Authored by Del Wolverton Chief Science Officer/Founder WolvertonBailey, Inc. SUMMARY This is the year, 2017, that we celebrate 140 years since Dr. Nikolas Otto patented the four-stroke internal combustion engine in 1877. His gasoline engine serves as the origin of the “Otto Cycle” which is used as the basis for seven internal combustion engine variants today. For purposes of this white paper, the four-cylinder Otto engine will be used as the “reference engine.” Since Dr. Otto’s engine was built around the origin of the four-stroke-cycle of the pistons, this allows us to have a piston per cycle. Many changes have taken place during the past century in the size and shape of the engine as designed for various uses, however, this original four-stroke cycle is still used even in the latest internal combustion engine, the Counterpoise Bi-Radial Engine. This discussion will first describe the “basis” Otto Cycle, providing a simple, “math-free” description of each of the four strokes in the cycle. Then, in order to help understand the operation, power, and weight advantages gained in the evolution, the author will take you through the existing variants, all the way to the latest internal combustion engine—complete with the final patented design, the WBI Counterpoise Bi-Radial Engine. CONTENTS Single-Piston of the Otto Cycle ..................................................................................................... 2 The Four -
East Hartford, CT Pratt & Whitney, a Recognized Leading Producer
Co-op, Core Structures Group Job Code: 123314-01 Location: East Hartford, CT Pratt & Whitney, a recognized leading producer of the world's most advanced jet engines, is looking for dedicated individuals to become a part of our organization. If you would like to work in a dynamic environment and possess the motivation to incorporate new ideas into practice, this may be the opportunity you've been waiting for! Pratt & Whitney, a United Technologies Corp. company (NYSE:UTX), is a world leader in the design, manufacture and service of aircraft engines, auxiliary and ground power units, small turbojet propulsion products and industrial gas turbines. We reported an operating pro?t of $1.6 billion in 2012 on revenues of $14 billion. Our company has approximately 36,000 employees who support more than 11,000 customers around the world. Frederick Rentschler founded Pratt & Whitney in Hartford, Connecticut, in 1925. Our ?rst aircraft engine transformed the aviation industry. It was the 410-horsepower, aircooled Wasp, which delivered unprecedented performance and reliability for the time. We have been leading change ever since Work with a team of Structures Engineers to develop state-of-the-art high cycle fatigue (HCF) and low cycle fatigue (LCF) models for use in evaluating the next generation of jet engine components. Post process engine strain gage and performance data to create library of vibratory responses to be used in the development of a probabilistic Goodman Diagram approach to assess the vibratory response of jet engine blades and vanes. Also work on the development of Advanced LCF program which incorporates elastic plastic behavior, creep, and multi-axial fatigue into one life system. -