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classificationCPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F16H25-2472
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classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C13-34
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F16H25-24
filingDate 2010-09-06-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_cbd60a45197192c66670516bed2efb1f
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_229657b94eda969a08645b352c5a4c9b
publicationDate 2011-03-09-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber EP-2292513-A1
titleOfInvention Actuator with integrated status monitoring system and method for manufacturing same
abstract The present invention relates in the field of aviation and vehicle technology, in particular in the field of control technology, to an actuator with an integrated condition monitoring system for detecting and monitoring mechanical irregularities of individual components of the actuator and / or for measuring a load distribution thereon. Furthermore, the present invention relates to a method for condition monitoring of the actuator and a method for its production. The actuators according to the invention are used in positioning systems in the field of flight control and vehicle control technology as well as in the field of energy generation.
priorityDate 2009-09-08-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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