| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_da0cef2e81237af45dd8e8e3bc96b211 |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02T50-60
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2220-76
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2220-329 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C9-42
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C3-107
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C27-12
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C7-262
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D35-02
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C3-10
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C7-36
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C7-275
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H02K7-20
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H02K7-1823
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C7-32
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D35-08 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C7-262 |
| filingDate |
2015-03-26-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate |
2019-04-24-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_fc88fba49c52a25dc3ccfdac53c7deea
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_ba4ac380adb01f28233dc8ec4d16509f
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_beb1464767f397541934a70b703f2b09
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_303259e6af8fab813d32127a0a8d9fa3 |
| publicationDate |
2019-04-24-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
RU-2686236-C2 |
| titleOfInvention |
Assistance device for one of free turbine turbomachines of aircraft comprising at least two free turbine turbomachines |
| abstract |
FIELD: internal combustion engines. n SUBSTANCE: assistance device (100) for free turbine turbomachine (GT1) of an aircraft, comprising at least two free turbine turbomachines (GT1, GT2), the device comprising electric starter machine (D1) for providing prolonged assistance to the gas generator of first turbomachine (GT1) using energy produced by electric generator machine (G2) driven by second turbomachine (GT2), the device additionally comprising at least one electrical storage member (S1) electrically connected to said electric starter machine (D1) to provide short-term assistance to said gas generator. Electric starter machine (D1) is powered by first power converter (SPC1) that allows it to exchange energy with storage member (S1) for short-term assistance, and that transmits to it energy supplied by second power converter (SPC2) for prolonged assistance. n EFFECT: independence from on-board network and easy implementation. n 12 cl, 13 dwg |
| priorityDate |
2014-03-27-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |