http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-6554224-B2

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assignee http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_887e125008cf84c53554d9e68cf7f02b
classificationCPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K1-72
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K1-766
classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K1-72
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K1-76
filingDate 2001-08-31^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 2003-04-29^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_1aee37c284c4cb9932c60848db89ef7f
publicationDate 2003-04-29^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber US-6554224-B2
titleOfInvention Out-of-plane thrust reverser sleeve lock
abstract A thrust reverser system for a jet engine has a thrust reverser sleeve lock, preferably for each thrust reverser sleeve, that provides at least one of the redundant anti-deployment mechanisms of the thrust reverser. The thrust reverser sleeve lock has a lock pin that engages a lock pin hole in a slider of the thrust reverser when the thrust reverser sleeve is in a stowed position and the thrust reverser sleeve lock is in a lock position to prevent the thrust reverser sleeve from deploying. The thrust reverser sleeve lock is located out of a plane in which other anti-deployment mechanisms of the thrust reverser are located.
isCitedBy http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-8109467-B2
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http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-8201390-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2009151320-A1
priorityDate 2001-08-31^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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