HELICOPTER VIBRATION CONTROL SYSTEM AND ROTATING ASSEMBLY ROTARY FORCES GENERATORS FOR CANCELING VIBRATIONS
A rotary wing aircraft including a vehicle vibration control system. The vehicle vibration control system includes a rotating hub mounted vibration control system, the rotating hub mounted vibration control system mounted to the rotating rotary wing hub with the rotating hub mounted vibration contro...
Saved in:
Main Authors | , |
---|---|
Format | Patent |
Language | English French German |
Published |
04.11.2015
|
Subjects | |
Online Access | Get full text |
Cover
Loading…
Abstract | A rotary wing aircraft including a vehicle vibration control system. The vehicle vibration control system includes a rotating hub mounted vibration control system, the rotating hub mounted vibration control system mounted to the rotating rotary wing hub with the rotating hub mounted vibration control system rotating with the rotating rotary wing hub. The vehicle vibration control system includes a rotary wing aircraft member sensor for outputting rotary wing aircraft member data correlating to the relative rotation of the rotating rotary wing hub member rotating relative to the nonrotating body, at least a first nonrotating body vibration sensor, the at least first nonrotating body vibration sensor outputting at least first nonrotating body vibration sensor data correlating to vibrations, at least a first nonrotating body circular force generator, the at least a first nonrotating body circular force generator fixedly coupled with the nonrotating body, and a distributed force generation data communications network link. |
---|---|
AbstractList | A rotary wing aircraft including a vehicle vibration control system. The vehicle vibration control system includes a rotating hub mounted vibration control system, the rotating hub mounted vibration control system mounted to the rotating rotary wing hub with the rotating hub mounted vibration control system rotating with the rotating rotary wing hub. The vehicle vibration control system includes a rotary wing aircraft member sensor for outputting rotary wing aircraft member data correlating to the relative rotation of the rotating rotary wing hub member rotating relative to the nonrotating body, at least a first nonrotating body vibration sensor, the at least first nonrotating body vibration sensor outputting at least first nonrotating body vibration sensor data correlating to vibrations, at least a first nonrotating body circular force generator, the at least a first nonrotating body circular force generator fixedly coupled with the nonrotating body, and a distributed force generation data communications network link. |
Author | MEYERS, ANDREW, D JOLLY, MARK, R |
Author_xml | – fullname: JOLLY, MARK, R – fullname: MEYERS, ANDREW, D |
BookMark | eNqNjEsKwkAQRGehC3936AsImqj7ydj5QDIdugchqxBk3ChJIN4fRxHXrgpevaqlmvVD7xfqnmNZGKodMlyKhLUryIIh65hKkEYcVqDtGZhc6GwGWgSrpGw-hBtIiQ0KZGgxrInlTcBoa8Jz8H-vslbzW_eY_OabKwUpOpNv_Ti0fhq7q-_9s8U6io-nXXRI9vEfygsVQjht |
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 Physics |
DocumentTitleAlternate | SYSTÈME DE CONTRÔLE DE VIBRATIONS D HÉLICOPTÈRE ET GÉNÉRATEUR DE FORCES ROTATIVES D ENSEMBLE DE ROTATION POUR ANNULER DES VIBRATIONS HUBSCHRAUBERSCHWINGUNGSSTEUERUNGSSYSTEM UND ROTATIONSANORDNUNGSDREHKRAFTERZEUGER ZUR UNTERDRÜCKUNG VON SCHWINGUNGEN |
ExternalDocumentID | EP2356024B1 |
GroupedDBID | EVB |
ID | FETCH-epo_espacenet_EP2356024B13 |
IEDL.DBID | EVB |
IngestDate | Fri Jul 19 16:53:34 EDT 2024 |
IsOpenAccess | true |
IsPeerReviewed | false |
IsScholarly | false |
Language | English French German |
LinkModel | DirectLink |
MergedId | FETCHMERGED-epo_espacenet_EP2356024B13 |
Notes | Application Number: EP20090799799 |
OpenAccessLink | https://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20151104&DB=EPODOC&CC=EP&NR=2356024B1 |
ParticipantIDs | epo_espacenet_EP2356024B1 |
PublicationCentury | 2000 |
PublicationDate | 20151104 |
PublicationDateYYYYMMDD | 2015-11-04 |
PublicationDate_xml | – month: 11 year: 2015 text: 20151104 day: 04 |
PublicationDecade | 2010 |
PublicationYear | 2015 |
RelatedCompanies | LORD CORPORATION |
RelatedCompanies_xml | – name: LORD CORPORATION |
Score | 3.0095701 |
Snippet | A rotary wing aircraft including a vehicle vibration control system. The vehicle vibration control system includes a rotating hub mounted vibration control... |
SourceID | epo |
SourceType | Open Access Repository |
SubjectTerms | AEROPLANES AIRCRAFT AVIATION BLASTING CONTROLLING COSMONAUTICS ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HEATING HELICOPTERS LIGHTING MEANS FOR DAMPING VIBRATION MECHANICAL ENGINEERING PERFORMING OPERATIONS PHYSICS REGULATING SHOCK-ABSORBERS SPRINGS SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TECHNICAL SUBJECTS COVERED BY FORMER USPC TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ARTCOLLECTIONS [XRACs] AND DIGESTS THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS |
Title | HELICOPTER VIBRATION CONTROL SYSTEM AND ROTATING ASSEMBLY ROTARY FORCES GENERATORS FOR CANCELING VIBRATIONS |
URI | https://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20151104&DB=EPODOC&locale=&CC=EP&NR=2356024B1 |
hasFullText | 1 |
inHoldings | 1 |
isFullTextHit | |
isPrint | |
link | http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwfV1Lb8IwDLYQe942tmnspRwmbtUGDTAOaKJpGExtUzUdghOiLwlNKmh02t-fEx7bZbtVTmSljhzbif0Z4D4zM5M2qcpqfIoMOktaxixuJkaaKWRC9LfXYNWu1xq80ddxc1yC-bYWRuOEfmlwRNSoGPW90Of18ucSy9a5lauHaI6kxXM_7Nq1TXSM5kt1s7WtLveFLViNMfyqeUG3YaJpb1ALA6U99KLbShn4yFJFKcvfFqV_Avs-MsuLUyileQWO2LbxWgUO3c17dwUOdIJmvELiRglXZ_A-4M6QCR8dUTIaWutbJsKEFwbCIXIiQ-6SnmeTQIQ45r2QnpTctZyJpgQTgpEf45Ks09ZCEUhFIUz1qXHU_B1XeQ6kz0M2MHD9052sptzf_al5AeV8kaeXQMyYdtI46jzOMgUegzsQtWjWiJI2TWk9q1eh-iebq3_GruFYCV3X5tEbKBcfn-ktGukiutPi_QbyXY2u |
link.rule.ids | 230,309,783,888,25576,76876 |
linkProvider | European Patent Office |
linkToHtml | http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwfV1LTwIxEJ4QfOBNUQM-ezDcNgpbQA7EsN3iovvKbiVwIuyymxCThcga_77T8tCL3pppM-kj05lpZ74BuEv1VKdNKqMaHyONTmctbRo3Z1qSSmRCtLfXYNWO27Le6MuoOSrAfJsLo3BCvxQ4IkpUjPKeq_t6-fOIZarYytV9NEfS4qkvumZt4x2j-pLVbE2jy33P9FiNMWzV3KDb0FG1N6iBjtIeWthtKQx8aMiklOVvjdI_hn0fmWX5CRSSrAwlti28VoZDZ_PfXYYDFaAZr5C4EcLVKbxb3B4wz0dDlAwHxvqViTDPFYFnk3AcCu6QnmuSwBPY5z6TXhhyx7DHihKMCXp-jIdkHbYmvCCUFMJknRpbjt9xDc-A9Llglobzn-z2asL93Ur1cyhmiyypANFj2kniqPMwTSV4DJ5A1KJpI5q1aULrab0K1T_ZXPzTdwslSzj2BOf2eglH8gBUnh69gmL-8Zlco8LOoxu11d_E65Ch |
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=HELICOPTER+VIBRATION+CONTROL+SYSTEM+AND+ROTATING+ASSEMBLY+ROTARY+FORCES+GENERATORS+FOR+CANCELING+VIBRATIONS&rft.inventor=JOLLY%2C+MARK%2C+R&rft.inventor=MEYERS%2C+ANDREW%2C+D&rft.date=2015-11-04&rft.externalDBID=B1&rft.externalDocID=EP2356024B1 |