Turbine accessory drive gearbox assembly in an airplane engine such as a jet engine

The gearbox has a casing (10) mounted with a coiled stator (18) of an electric machine e.g. alternator (16), whose rotor (14) is guided in a bearing (24) e.g. roller bearing, carried by a support part (40). The support part is carried by an annular part (42) of the machine and is made of reduced the...

Full description

Saved in:
Bibliographic Details
Main Authors ABOUSLEIMAN, VINCENT, LINET, HUGUES
Format Patent
LanguageEnglish
French
German
Published 19.09.2012
Subjects
Online AccessGet full text

Cover

Loading…
Abstract The gearbox has a casing (10) mounted with a coiled stator (18) of an electric machine e.g. alternator (16), whose rotor (14) is guided in a bearing (24) e.g. roller bearing, carried by a support part (40). The support part is carried by an annular part (42) of the machine and is made of reduced thermal dilation coefficient material e.g. titanium. The annular part is applied on the casing and is made good heat conducting material e.g. aluminum, having thermal conductivity higher than the thermal conductivity of the support part for forming a thermal bridge between the stator and the casing.
AbstractList The gearbox has a casing (10) mounted with a coiled stator (18) of an electric machine e.g. alternator (16), whose rotor (14) is guided in a bearing (24) e.g. roller bearing, carried by a support part (40). The support part is carried by an annular part (42) of the machine and is made of reduced thermal dilation coefficient material e.g. titanium. The annular part is applied on the casing and is made good heat conducting material e.g. aluminum, having thermal conductivity higher than the thermal conductivity of the support part for forming a thermal bridge between the stator and the casing.
Author ABOUSLEIMAN, VINCENT
LINET, HUGUES
Author_xml – fullname: ABOUSLEIMAN, VINCENT
– fullname: LINET, HUGUES
BookMark eNqNy00KwjAUBOAsdOHfHd4FXBSpda1UXAp2X17j2EZiEvJasbc3Qg8gDAwM3yzVzHmHhbpVQ2yMA7HWEPFxpHs0b1ALjo3_EIvg1diRjCNOMTFYTh6u_d1k0F0yxPREP41rNX-wFWymXik6l9XpskXwNSSwhkNfl9fskBf7vDhmuz_IF_W4OWA
ContentType Patent
DBID EVB
DatabaseName esp@cenet
DatabaseTitleList
Database_xml – sequence: 1
  dbid: EVB
  name: esp@cenet
  url: http://worldwide.espacenet.com/singleLineSearch?locale=en_EP
  sourceTypes: Open Access Repository
DeliveryMethod fulltext_linktorsrc
Discipline Medicine
Chemistry
Sciences
DocumentTitleAlternate Zubehörgehäuse in einem Flugzeugmotor wie einem Turbinentriebwerk
Boitier d'accessoires dans un moteur d'avion tel qu'un turboréacteur
ExternalDocumentID EP1857657B1
GroupedDBID EVB
ID FETCH-epo_espacenet_EP1857657B13
IEDL.DBID EVB
IngestDate Fri Jul 19 14:56:50 EDT 2024
IsOpenAccess true
IsPeerReviewed false
IsScholarly false
Language English
French
German
LinkModel DirectLink
MergedId FETCHMERGED-epo_espacenet_EP1857657B13
Notes Application Number: EP20070290617
OpenAccessLink https://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20120919&DB=EPODOC&CC=EP&NR=1857657B1
ParticipantIDs epo_espacenet_EP1857657B1
PublicationCentury 2000
PublicationDate 20120919
PublicationDateYYYYMMDD 2012-09-19
PublicationDate_xml – month: 09
  year: 2012
  text: 20120919
  day: 19
PublicationDecade 2010
PublicationYear 2012
RelatedCompanies HISPANO SUIZA
RelatedCompanies_xml – name: HISPANO SUIZA
Score 2.8685682
Snippet The gearbox has a casing (10) mounted with a coiled stator (18) of an electric machine e.g. alternator (16), whose rotor (14) is guided in a bearing (24) e.g....
SourceID epo
SourceType Open Access Repository
SubjectTerms CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
DYNAMO-ELECTRIC MACHINES
ELECTRICITY
GENERATION
Title Turbine accessory drive gearbox assembly in an airplane engine such as a jet engine
URI https://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20120919&DB=EPODOC&locale=&CC=EP&NR=1857657B1
hasFullText 1
inHoldings 1
isFullTextHit
isPrint
link http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwfV3dS8MwED_GFPVNp-L8Ig_St6IlbVcfitAvhrCtaJW9jaZLtaJt6Qe6_95L6KYvCn0IaQnNkV_uLnf3C8BVwlDHUCNRNVwsKprUXI1TTtUbFpspAp1aqYjoTqbm-Em_nxvzHmTrWhjJE_opyRERUQnivZH7dflziOXJ3Mr6mmXYVdwFke0pnXcsCkERgZ5j--HMm7mK62JLmT7YgvLINEYOOkpbwooWNPv-syOKUsrfGiXYh-0QB8ubA-il1QB23fXFawPYmXTxbmx20KsP4TFqK_RiOYnlFYdFtSLLCrcq8oJrlRVfBK1g_sHeVyTLSYxPVpUikZVwyThI6jZ5xW9ITN5403UeAQn8yB2r-HeLjSQWfriZBz2Gfl7k_AQI1RLU89RCBzPW0xG3KF3ShHKDMkOjujGE4Z_DnP7z7gz2hEhFdoR2ew79pmr5Barghl1K4X0DhjWLww
link.rule.ids 230,309,786,891,25594,76906
linkProvider European Patent Office
linkToHtml http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwfV3fT4MwEL4s0zjfdGqcP_tg9kaUFBg-EJPBFtSxLYpmb4SyohgFAiy6_95rw6YvmvDQFNLQS7_eXe_uK8BFxFDHUD1SVFwsCprUXAljTpUrFhoxAp2asYjoemPDfdLuZvqsAcmqFkbyhH5KckREVIR4r-R-nf8cYjkyt7K8ZAl2ZTdD33K6tXcsCkERgU7fGkwnzsTu2ja2uuMHS1AeGXqvj47SRk-Q8wrL6bkvilLy3xpluAObUxwsrXahERdtaNmri9fasOXV8W5s1tAr9-DRXxToxXISyisOs2JJ5gVuVeQF1yrLvghawfyDvS9JkpIQn6TIRSIr4ZJxkJSL6BW_ISF541XduQ9kOPBtV8G_C9aSCAbT9TzoATTTLOWHQKgaoZ6nJjqYoRb3uEnpnEaU65TpKtX0DnT-HObon3fn0HJ9bxSMbsf3x7AtxCsyJdTrE2hWxYKfojqu2JkU5Dc4Lo6w
openUrl ctx_ver=Z39.88-2004&ctx_enc=info%3Aofi%2Fenc%3AUTF-8&rfr_id=info%3Asid%2Fsummon.serialssolutions.com&rft_val_fmt=info%3Aofi%2Ffmt%3Akev%3Amtx%3Apatent&rft.title=Turbine+accessory+drive+gearbox+assembly+in+an+airplane+engine+such+as+a+jet+engine&rft.inventor=ABOUSLEIMAN%2C+VINCENT&rft.inventor=LINET%2C+HUGUES&rft.date=2012-09-19&rft.externalDBID=B1&rft.externalDocID=EP1857657B1