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contributor authorC. B. Meher-Homji
date accessioned2017-05-08T23:53:18Z
date available2017-05-08T23:53:18Z
date copyrightOctober, 1997
date issued1997
identifier issn1528-8919
identifier otherJETPEZ-26771#783_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/118606
description abstractThis paper describes the pioneering work of Anselm Franz who, while working for the Junkers Engine company in Germany, designed and made operational the world’s first production jet engine, the Junkers Jumo 004, which was the powerplant for the formidable Messerschmitt ME 262 fighter. The paper covers the historical background of jet engine development in Germany during the Second World War and discusses design details of this remarkable axial flow, 1980 lb (900 kg) thrust engine. The development represented a historic achievement for Anselm Franz and his design team at Junkers. Approximately 6000 engines were built at the end of the Second World War in the face of acute shortages and damage to German industry. The Jumo was brought from conceptual design to production in a span of four years. Franz joined Avco Lycoming in 1952 and worked for 16 years. He retired as Vice President in 1968 after making prolific contributions to the development of several Lycoming engines including the T53, the T55, and the AGT-1500. Anselm Franz passed away at the age of 94 in Stratford, Connecticut. This paper is a modest tribute to a jet engine pioneer who, in spite of his extensive contributions to gas turbine technology, will always be remembered as the man who designed the world’s first production turbojet.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Development of the Junkers Jumo 004B—The World’s First Production Turbojet
typeJournal Paper
journal volume119
journal issue4
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2817055
journal fristpage783
journal lastpage789
identifier eissn0742-4795
keywordsTurbojets
keywordsEngines
keywordsJet engines
keywordsDesign
keywordsWarfare
keywordsConceptual design
keywordsGas turbines
keywordsPower stations
keywordsAxial flow
keywordsTeams AND Thrust
treeJournal of Engineering for Gas Turbines and Power:;1997:;volume( 119 ):;issue: 004
contenttypeFulltext


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