http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RO-129076-A0

Outgoing Links

Predicate Object
assignee http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_7c5cfd50711def04ed51cbceb4a15527
classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D27-26
filingDate 2013-08-09-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_5bb4173574b75ce18caabc644e81b084
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_75e23fbd12b2bd9a6eccb47246b1a73b
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_a72f0211bddfaed9ac571f7b9d558da1
publicationDate 2013-12-30-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber RO-129076-A0
titleOfInvention SUPPORT ENGINE TURBOPROPULSOR
abstract The invention relates to a turboprop motor support for aircrafts with engines installed under the wing. According to the invention, the motor support consists essentially of a front frame (1), a frame (2) and a rear frame (3), the frame (1) being of welded construction, the frame (2) (3) is welded construction, and attaches to the front frame (1) and the frame (2) fabricated by means of a fork (13), and by wing, by means of the fastening-adjustment subassembly, consisting of an inner threaded bush (6) and a threaded rod (8).
priorityDate 2013-08-09-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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