Sandbox

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Example 2 - dumb-down to Copy
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<dc:subject>T Technology--TL Motor vehicles. Aeronautics. Astronautics</dc:subject> <dc:subject>T Technology--TL Motor vehicles. Aeronautics. Astronautics</dc:subject>
- <dc:description>The design, analysis and performance of a brushless PM motor that is integrated in the + <dc:description>The design, analysis and performance of a brushless PM motor that is integrated
- structure of a miniature 50 mm diameter propeller thruster is considered; the stator + in the structure of a miniature 50 mm diameter propeller thruster is considered;
- is fitted in the aired thin duct that surrounds the propeller to improve its efficiency + the stator is fitted in the aired thin duct that surrounds the propeller to
- and protect it from damage, and the rotor is fitted to the rim of the propeller. Such a + improve its efficiency and protect it from damage, and the rotor is fitted to the
- thruster is intended for use on small autonomous underwater vehicles that are being + rim of the propeller. Such a thruster is intended for use on small autonomous
- developed for defence, scientific and industry applications. Fitting a relatively large + underwater vehicles that are being developed for defence, scientific and industry
- airgap motor with protective coating within the volume of a thin propeller duct + applications. Fitting a relatively large airgap motor with protective coating
- (<10 mm thick) imposes extreme constraints on the dimensions of the machine, including a + within the volume of a thin propeller duct (<10 mm thick) imposes extreme
- very thin rotor and stator radial thickness and relatively short axial length in addition + constraints on the dimensions of the machine, including a very thin rotor and
- to the relatively large airgap, which raises theoretical and practical issues that have not + stator radial thickness and relatively short axial length in addition to the
- been considered in the literature. The design of such a machine is discussed, a demonstrator + relatively large airgap, which raises theoretical and practical issues that have
- device is described and FEA and experimental results are reported.</dc:description>+ not been considered in the literature. The design of such a machine is discussed,
- + a demonstrator device is described and FEA and experimental results are reported.
 + </dc:description>
 +
<dc:identifier>http://eprints.soton.ac.uk/22934/</dc:identifier> <dc:identifier>http://eprints.soton.ac.uk/22934/</dc:identifier>

Revision as of 09:25, 3 August 2006

The Sandbox is an experimental area for new users. Feel free to edit this page in order to practice editing and wiki formatting.

To view a preview of your work, click 'show preview' at the bottom of the edit page. To save your work, click 'save page'. The contents of this page will be regularly cleared, so do not input any text here that you wish to return to or re-use.

For help with editing pages, please see the Editing help.

Example 2 - dumb-down to Copy 

<?xml version="1.0"?>
<!DOCTYPE rdf:RDF PUBLIC "-//DUBLIN CORE//DCMES DTD 2002/07/31//EN"
   "http://dublincore.org/documents/2002/07/31/dcmes-xml/dcmes-xml-dtd.dtd">
<rdf:RDF xmlns:rdf="http://www.w3.org/1999/02/22-rdf-syntax-ns#"
   xmlns:dc="http://purl.org/dc/elements/1.1/">

 <rdf:Description rdf:about="http://scitation.aip.org/getpdf/servlet/GetPDFServlet?filetype=pdf&id=
                             IEPAER000151000005000513000001&idtype=cvips&prog=normal">

   <dc:title xml:lang="en">Structurally integrated brushless PM motor for miniature propeller 
                           thrusters</dc:title>

   <dc:subject>T Technology--TC Hydraulic engineering. Ocean engineering</dc:subject>
   <dc:subject>T Technology--TK Electrical engineering. Electronics Nuclear engineering</dc:subject>
   <dc:subject>T Technology--TL Motor vehicles. Aeronautics. Astronautics</dc:subject>

   <dc:description>The design, analysis and performance of a brushless PM motor that is integrated 
                   in the structure of a  miniature 50 mm diameter propeller thruster is considered; 
                   the stator is fitted in the aired thin duct that surrounds the propeller to 
                   improve its efficiency and protect it from damage, and the rotor is fitted to the 
                   rim of the propeller. Such a thruster is intended for use on small autonomous 
                   underwater vehicles that are being developed for defence, scientific and industry 
                   applications. Fitting a relatively large airgap motor with protective coating 
                   within the volume of a thin propeller duct (<10 mm thick) imposes extreme 
                   constraints on the dimensions of the machine, including a very thin rotor and 
                   stator radial thickness and relatively short axial length in addition  to the 
                   relatively large airgap, which raises theoretical and practical issues that have 
                   not been considered in the literature. The design of such a machine is discussed, 
                   a demonstrator device is described and FEA and experimental results are reported.
                   </dc:description>
   <dc:identifier>http://scitation.aip.org/getpdf/servlet/GetPDFServlet?filetype=pdf&id=
                  IEPAER000151000005000513000001&idtype=cvips&prog=normal</dc:identifier> 

   <dc:creator>Lai, S.H.</dc:creator>
   <dc:creator>Turnock, S.R.</dc:creator>
   <dc:creator>Abu Sharkh, S.M.A. (Suleiman)</dc:creator>

   <dc:language>en</dc:language>

   <dc:date>2004</dc:date>

   <dc:type>http://purl.org/eprint/type/JournalArticle</dc:type>
   <dc:type>http://purl.org/eprint/status/PeerReviewed</dc:type>
   <dc:type>http://purl.org/eprint/entitytype/Copy</dc:type>

   <dc:rights>(c) Institution of Engineering and Technology</dc:rights>

   <dc:format>application/pdf</dc:format>

   <dc:publisher>Institution of Engineering and Technology</dc:publisher>
 
   <dc:relation>http://eprints.soton.ac.uk/22934/</dc:relation>
   <dc:relation>IEE Proceedings - Electric Power Applications, 151, (5), 513-519 (2004)</dc:relation>
   <dc:relation>&ctx_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article
                &rft.atitle=Structurally+integrated+brushless+PM+motor+for+miniature+propeller+thrusters
                &rft.jtitle=IEE+Proceedings+-+Electric+Power+Applications
                &rft.volume=151&rft.issue=5&rft.spage=513&rft.date=2004&rft.issn=1350-2352
                &rft.aulast=Sharkh&rft.auinit=S+M+A&rfr_id=info:sid/eprints.soton.ac.uk</dc:relation>
   <dc:relation>http://dx.doi.org/doi:10.1049/ip-epa:20040736</dc:relation>
   <dc:relation>http://www.theiet.org/</dc:relation>
   <dc:relation>Institution of Engineering and Technology</dc:relation>
   <dc:relation>http://www.ietdl.org/</dc:relation>
   <dc:relation>IET Digital Library</dc:relation>

 </rdf:Description>
</rdf:rdf>

Example 2 - dumb-down to ScholarlyWork 

<?xml version="1.0"?>
<!DOCTYPE rdf:RDF PUBLIC "-//DUBLIN CORE//DCMES DTD 2002/07/31//EN"
   "http://dublincore.org/documents/2002/07/31/dcmes-xml/dcmes-xml-dtd.dtd">
<rdf:RDF xmlns:rdf="http://www.w3.org/1999/02/22-rdf-syntax-ns#"
   xmlns:dc="http://purl.org/dc/elements/1.1/">

 <rdf:Description rdf:about="http://eprints.soton.ac.uk/22934/">

   <dc:title xml:lang="en">Structurally integrated brushless PM motor for miniature propeller thrusters</dc:title>

   <dc:subject>T Technology--TC Hydraulic engineering. Ocean engineering</dc:subject>
   <dc:subject>T Technology--TK Electrical engineering. Electronics Nuclear engineering</dc:subject>
   <dc:subject>T Technology--TL Motor vehicles. Aeronautics. Astronautics</dc:subject>

   <dc:description>The design, analysis and performance of a brushless PM motor that is integrated 
                   in the structure of a  miniature 50 mm diameter propeller thruster is considered; 
                   the stator is fitted in the aired thin duct that surrounds the propeller to 
                   improve its efficiency and protect it from damage, and the rotor is fitted to the 
                   rim of the propeller. Such a thruster is intended for use on small autonomous 
                   underwater vehicles that are being developed for defence, scientific and industry 
                   applications. Fitting a relatively large airgap motor with protective coating 
                   within the volume of a thin propeller duct (<10 mm thick) imposes extreme 
                   constraints on the dimensions of the machine, including a very thin rotor and 
                   stator radial thickness and relatively short axial length in addition  to the 
                   relatively large airgap, which raises theoretical and practical issues that have 
                   not been considered in the literature. The design of such a machine is discussed, 
                   a demonstrator device is described and FEA and experimental results are reported.
                   </dc:description>
 
   <dc:identifier>http://eprints.soton.ac.uk/22934/</dc:identifier> 

   <dc:creator>Lai, S.H.</dc:creator>
   <dc:creator>Turnock, S.R.</dc:creator>
   <dc:creator>Abu Sharkh, S.M.A. (Suleiman)</dc:creator>

   <dc:language>en</dc:language>

   <dc:date>2004</dc:date>

   <dc:type>http://purl.org/eprint/type/JournalArticle</dc:type>
   <dc:type>http://purl.org/eprint/entitytype/ScholarlyWork</dc:type>

   <dc:rights>(c) Institution of Engineering and Technology</dc:rights>

   <dc:format>application/pdf</dc:format>

   <dc:publisher>Institution of Engineering and Technology</dc:publisher>
 
   <dc:relation>http://scitation.aip.org/getpdf/servlet/GetPDFServlet?filetype=pdf&id=
                  IEPAER000151000005000513000001&idtype=cvips&prog=normal</dc:relation>
   <dc:relation>IEE Proceedings - Electric Power Applications, 151, (5), 513-519 (2004)</dc:relation>
   <dc:relation>&ctx_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article
                &rft.atitle=Structurally+integrated+brushless+PM+motor+for+miniature+propeller+thrusters
                &rft.jtitle=IEE+Proceedings+-+Electric+Power+Applications
                &rft.volume=151&rft.issue=5&rft.spage=513&rft.date=2004&rft.issn=1350-2352
                &rft.aulast=Sharkh&rft.auinit=S+M+A&rfr_id=info:sid/eprints.soton.ac.uk</dc:relation>
   <dc:relation>http://dx.doi.org/doi:10.1049/ip-epa:20040736</dc:relation>
   <dc:relation>http://www.theiet.org/</dc:relation>
   <dc:relation>Institution of Engineering and Technology</dc:relation>
   <dc:relation>http://www.ietdl.org/</dc:relation>
   <dc:relation>IET Digital Library</dc:relation>

 </rdf:Description>
</rdf:rdf>
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