| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_36b24a67692efb417e7c9f3c8dd0273e |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02T50-40 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C1-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B29C53-60
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B29C70-36
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B29C70-08 |
| filingDate |
2012-11-01-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate |
2014-03-20-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_e9c2a56fd3e5595ac0af45eec270950c
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_ba06f3d500b44f21b89b2daed2de0536
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_535984d24cee2d475cf1081c2172bd35
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_50a1160af5635c655e63545ef71556fa
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_5a52bba17769ecf625442946ff0220d8
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_85c434ce6677de92f5d24b3b6a1809f0
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_d4c8ec2543251959720544e09f64a4dc
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_a4068ad64f010a653a6d6f44eeefb752
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_5e747735bf579d92d3fd18b10203c18a
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_0eb77d8c7048cb2579668108b6d83c9b
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_5d8ec1646df4e0d2e74a2650cebcbfd8 |
| publicationDate |
2014-03-20-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
RU-2509649-C1 |
| titleOfInvention |
Method of making aircraft thrust reverser bearing grate sections from polymer composites, mandrel to this end, mould for pouring anti-adhesion elastic material of mandrel separation layer for implementation of said method and sections of aircraft thrust reverser bearing grate |
| abstract |
FIELD: process engineering. n SUBSTANCE: invention relates to aircraft engineering and can be used for production of gas turbine engine elements. Specific features of this invention consist in that lengthwise and crosswise grooves 3 and 4 of mandrel 5 wind on crossing lengthwise and crosswise plies of grooves 7 and blades of grate section 1. Grooves are made in separation layer 13 of anti-adhesion elastic layer to make rows of rods 14 between grooves 3 for ribs 7, said rods being separated in said rows by said grooves 4 reinforced with metal ledges 15. Said ledges 14 are used in the mould for making the anti-adhesion elastic layer to make rows of rods 14 between grooves 3 for ribs 7. After polymerisation, ledges 15 are withdrawn in individual paths to extrude rods 14 of said anti-adhesion material from grate cells to be laid in space released by ledges 15. Section of said grate is secured by front bearing blade to the frame 49 of engine nacelle 50 and by rear blade 52 its is secured to moving cowl 53 of thrust reverser 2. n EFFECT: hi-tech design of thrust reverser, higher reliability. n 8 cl, 12 dwg |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/WO-2018169453-A2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/WO-2018169454-A2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/WO-2018169453-A3
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-110617158-B
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-110617158-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10087842-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-2666889-C1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-2663249-C1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-2569725-C2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/WO-2018169454-A3
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/EP-3597409-A4 |
| priorityDate |
2012-11-01-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |