| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_2cb8aeea0794aeefbffe9687de100851 |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2220-323
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02T50-60
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2260-4031 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D41-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D27-26
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C7-32
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D27-20 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D27-26
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D27-20
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C7-32 |
| filingDate |
2021-06-29^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_9e5472ef15cc39330894981c48d3ae88
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_8ae79e9ee929dc74c30cda971f341287
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_184735ee7e4e3d9e33f68c26adaf1c35
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_6dab1b0bd24dc907e985e4e151e766eb |
| publicationDate |
2021-12-30^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
US-2021404387-A1 |
| titleOfInvention |
Gas turbine engine and aircraft with a gas turbine engine |
| abstract |
A gas turbine engine including an engine core and including a bypass channel of an aircraft is described. The bypass channel radially surrounds the engine core at least in part. At least one core shaft extending in the axial direction is provided, which shaft is operatively connected, by means of a drive train, to a core accessory gearbox arranged between the engine core and the bypass channel, and to an aircraft accessory gearbox. The aircraft accessory gearbox is arranged radially outside the bypass channel. The drive train extends substantially in the radial direction between the core shaft and the aircraft accessory gearbox. The drive train has an angle drive between a radial shaft and the core shaft. Furthermore, the drive train comprises another angle drive between the radial shaft and the core accessory gearbox and an additional angle drive between the radial shaft and the aircraft accessory gearbox. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11572838-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2023119477-A1 |
| priorityDate |
2020-06-30^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |