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End Leakage of Aerospace Homopolar Alternators

An accurate knowledge of the magnetic field distribution is of great importance in finding the best designs for electrical machinery. It is the purpose of this paper to present a new numerical method for the determination of three-dimensional flux distribution in the end zone of a highspeed aerospac...

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Published in:	IEEE transactions on aerospace and electronic systems 1970-09, Vol.AES-6 (5), p.684-691
Main Author:	Sarma, Mulukutla S.
Format:	Article
Language:	English
Subjects:	Aerospace engineering Alternators Machine windings Magnetic analysis Magnetic fields Magnetic flux Magnetostatics Permeability Shape Stator windings
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description	An accurate knowledge of the magnetic field distribution is of great importance in finding the best designs for electrical machinery. It is the purpose of this paper to present a new numerical method for the determination of three-dimensional flux distribution in the end zone of a highspeed aerospace homopolar alternator, and for the calculation of end leakage reactance. The new analysis is applied to an experimental 95 kVA, 115/200 V, 3400 Hz, 40 800 r/min, three-phase, wye-connected, homopolar alternator.
doi_str_mv	10.1109/TAES.1970.310070
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The new analysis is applied to an experimental 95 kVA, 115/200 V, 3400 Hz, 40 800 r/min, three-phase, wye-connected, homopolar alternator.</description><subject>Aerospace engineering</subject><subject>Alternators</subject><subject>Machine windings</subject><subject>Magnetic analysis</subject><subject>Magnetic fields</subject><subject>Magnetic flux</subject><subject>Magnetostatics</subject><subject>Permeability</subject><subject>Shape</subject><subject>Stator windings</subject><issn>0018-9251</issn><issn>1557-9603</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1970</creationdate><recordtype>article</recordtype><recordid>eNo9j0tLw0AUhQdRMFb3gpv8gcR7M6_MMpRohYAL63qYzEOqaRNmsvHfm1Dp6nLgfofzEfKIUCKCet437UeJSkJJEUDCFcmQc1koAfSaZABYF6rieEvuUvpeIqsZzUjZnlzeefNjvnw-hrzxcUyTsT7fjcdxGgcT82aYfTyZeYzpntwEMyT_8H835POl3W93Rff--rZtusJWAudCMRCO8mCFrI2XlNkeqAmV4hZFvSTLTeDQ0-BcTx2rnXD9AvjeSYHM0A2Bc69d5qTog57i4Wjir0bQq69effXqq8--C_J0Rg7e-8s7Q6BcMfoHlnFRKQ</recordid><startdate>197009</startdate><enddate>197009</enddate><creator>Sarma, Mulukutla S.</creator><general>IEEE</general><scope>AAYXX</scope><scope>CITATION</scope></search><sort><creationdate>197009</creationdate><title>End Leakage of Aerospace Homopolar Alternators</title><author>Sarma, Mulukutla S.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c261t-9406d35fc678ae734cb03af295c1684cbc5af50b3fddb3d48d6dbd35ebd7614a3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1970</creationdate><topic>Aerospace engineering</topic><topic>Alternators</topic><topic>Machine windings</topic><topic>Magnetic analysis</topic><topic>Magnetic fields</topic><topic>Magnetic flux</topic><topic>Magnetostatics</topic><topic>Permeability</topic><topic>Shape</topic><topic>Stator windings</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Sarma, Mulukutla S.</creatorcontrib><collection>CrossRef</collection><jtitle>IEEE transactions on aerospace and electronic systems</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Sarma, Mulukutla S.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>End Leakage of Aerospace Homopolar Alternators</atitle><jtitle>IEEE transactions on aerospace and electronic systems</jtitle><stitle>T-AES</stitle><date>1970-09</date><risdate>1970</risdate><volume>AES-6</volume><issue>5</issue><spage>684</spage><epage>691</epage><pages>684-691</pages><issn>0018-9251</issn><eissn>1557-9603</eissn><coden>IEARAX</coden><abstract>An accurate knowledge of the magnetic field distribution is of great importance in finding the best designs for electrical machinery. It is the purpose of this paper to present a new numerical method for the determination of three-dimensional flux distribution in the end zone of a highspeed aerospace homopolar alternator, and for the calculation of end leakage reactance. The new analysis is applied to an experimental 95 kVA, 115/200 V, 3400 Hz, 40 800 r/min, three-phase, wye-connected, homopolar alternator.</abstract><pub>IEEE</pub><doi>10.1109/TAES.1970.310070</doi><tpages>8</tpages></addata></record>
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language	eng
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source	IEEE Electronic Library (IEL) Journals
subjects	Aerospace engineering Alternators Machine windings Magnetic analysis Magnetic fields Magnetic flux Magnetostatics Permeability Shape Stator windings
title	End Leakage of Aerospace Homopolar Alternators
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