AIR INTAKE LIP OF AN AIRCRAFT ENGINE NACELLE, COMPRISING AT LEAST ONE INFRARED EMISSION SOURCE
The invention relates to an air intake lip of an aircraft engine nacelle extending along an axis X, in which an air flow circulates from upstream to downstream, the lip extending annularly about the X-axis and having an inner wall facing the X-axis and an outer wall which is opposite the inner wall,...
Saved in:
Main Authors | , |
---|---|
Format | Patent |
Language | English |
Published |
14.07.2022
|
Subjects | |
Online Access | Get full text |
Cover
Loading…
Abstract | The invention relates to an air intake lip of an aircraft engine nacelle extending along an axis X, in which an air flow circulates from upstream to downstream, the lip extending annularly about the X-axis and having an inner wall facing the X-axis and an outer wall which is opposite the inner wall, the inner wall and the outer wall being connected by an upstream wall and a partition so as to delimit an annular cavity, in which at least one infrared emission source is housed, wherein at least one wall, selected among the inner wall, the outer wall and the upstream wall, is made of a material configured to transmit on an outer face at least 30% of the infrared received on an inner face. |
---|---|
AbstractList | The invention relates to an air intake lip of an aircraft engine nacelle extending along an axis X, in which an air flow circulates from upstream to downstream, the lip extending annularly about the X-axis and having an inner wall facing the X-axis and an outer wall which is opposite the inner wall, the inner wall and the outer wall being connected by an upstream wall and a partition so as to delimit an annular cavity, in which at least one infrared emission source is housed, wherein at least one wall, selected among the inner wall, the outer wall and the upstream wall, is made of a material configured to transmit on an outer face at least 30% of the infrared received on an inner face. |
Author | Rami, Jean-Paul Gonidec, Patrick |
Author_xml | – fullname: Gonidec, Patrick – fullname: Rami, Jean-Paul |
BookMark | eNqNyr8KwjAQgPEMOvjvHQ5cFWy76HjESz1MLyVJV0uROElbqO-PHXwApw8-fmu16Ic-rdQD2QNLxDuB5RqcARSYp_ZoIpCULASCmqylA2hX1Z4DSwkYwRKGCG4GLMajpytQxSGwEwiu8Zq2avnq3lPa_bpRe0NR345pHNo0jd0z9enTNiE_5XmeXc5Fhlnxn_oCxoA05A |
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 |
ExternalDocumentID | US2022219831A1 |
GroupedDBID | EVB |
ID | FETCH-epo_espacenet_US2022219831A13 |
IEDL.DBID | EVB |
IngestDate | Fri Sep 27 05:20:22 EDT 2024 |
IsOpenAccess | true |
IsPeerReviewed | false |
IsScholarly | false |
Language | English |
LinkModel | DirectLink |
MergedId | FETCHMERGED-epo_espacenet_US2022219831A13 |
Notes | Application Number: US202017614146 |
OpenAccessLink | https://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20220714&DB=EPODOC&CC=US&NR=2022219831A1 |
ParticipantIDs | epo_espacenet_US2022219831A1 |
PublicationCentury | 2000 |
PublicationDate | 20220714 |
PublicationDateYYYYMMDD | 2022-07-14 |
PublicationDate_xml | – month: 07 year: 2022 text: 20220714 day: 14 |
PublicationDecade | 2020 |
PublicationYear | 2022 |
RelatedCompanies | SAFRAN NACELLES |
RelatedCompanies_xml | – name: SAFRAN NACELLES |
Score | 3.4161496 |
Snippet | The invention relates to an air intake lip of an aircraft engine nacelle extending along an axis X, in which an air flow circulates from upstream to... |
SourceID | epo |
SourceType | Open Access Repository |
SubjectTerms | AEROPLANES AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS HEATING HELICOPTERS HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS |
Title | AIR INTAKE LIP OF AN AIRCRAFT ENGINE NACELLE, COMPRISING AT LEAST ONE INFRARED EMISSION SOURCE |
URI | https://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20220714&DB=EPODOC&locale=&CC=US&NR=2022219831A1 |
hasFullText | 1 |
inHoldings | 1 |
isFullTextHit | |
isPrint | |
link | http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwfR1dS8MwMIwp6ptOxemUgNIni65r1-5hSJamrrqlI21lT460tiBIN1zFv--lbrqnvSW5cCQX7jO5C0I3ec80bSmlroxT3bStXHeyjtRz5z4xbCfvpqlKFB7z7jA2n6bWtIY-1rkwVZ3Q76o4InBUCvxeVvJ68R_Ecqu3lcu75B2G5g9e1He1lXdsGCofR3MHfTYJ3IBqlPbjUOOiggFzOp02AV9pRxnSqtI-exmovJTFplLxDtHuBPAV5RGqZUUD7dP132sNtDdeXXlDc8V9y2P0SnyBfR6RZ4bBIceBhwnHMEgF8SL8WyMKc0LZaMRuMQ3GE-GHPn_EJMIjRsIIBzDB554ggrkYjqCSpTgMYkHZCbr2WESHOix09keXWRxu7qpziurFvMjOELYzy8qMJEmlckh6ZiLTri3fclBYoKjSpIla2zCdbwdfoAPVVQHOttlC9fLzK7sEzVwmVxVBfwBfNYlk |
link.rule.ids | 230,309,786,891,25594,76903 |
linkProvider | European Patent Office |
linkToHtml | http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwfV3dS8MwEA9jivNNp-LH1IDSJ4uua9fuYUiWpq6uTUc_ZE-WtrYgSDdcxX_fa9x0T3sLd-FILtxdfknugtBtMVBVPUkSud6cyqquFbKR9xK5MB5SRTeKfpbVicIu748j9XmmzRroY50LI-qEfoviiGBRGdh7Jfz14v8QyxRvK5f36TuQ5o9WODSlFTpWlDofRzJHQzb1TI9KlA6jQOK-4IFxGr0uAay0owMoFGDpZVTnpSw2g4p1gHanIK-sDlEjL9uoRdd_r7XRnru68obmyvqWR-iV2D62eUgmDAMgx56FCcdApD6xQvxbIwpzQpnjsDtMPXfq24HNnzAJscNIEGIPOtjc8onPTAxLIHwpDrzIp-wY3VgspGMZBhr_6SWOgs1Z9U5Qs5yX-SnCeq5puZKmWVIDkoGaJllfT94KCFgQqLL0DHW2STrfzr5GrXHoOrFj88kF2q9Z9WFnV-2gZvX5lV9ClK7SK6HcH_EDjE4 |
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=AIR+INTAKE+LIP+OF+AN+AIRCRAFT+ENGINE+NACELLE%2C+COMPRISING+AT+LEAST+ONE+INFRARED+EMISSION+SOURCE&rft.inventor=Gonidec%2C+Patrick&rft.inventor=Rami%2C+Jean-Paul&rft.date=2022-07-14&rft.externalDBID=A1&rft.externalDocID=US2022219831A1 |