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 |
Incoming Links
Total number of triples: 25.