| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_2cb8aeea0794aeefbffe9687de100851 |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2260-20
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2240-35
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2260-98
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2260-213
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02T50-60
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2240-14 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D25-14
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C7-22
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D25-24
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D9-065
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D25-12
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C7-224
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C7-14 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F01D25-14
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F01D25-24
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C7-224
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C7-14 |
| filingDate |
2020-06-10^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_54e4cf68778000daf54cc16b714364ed |
| publicationDate |
2020-12-17^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
WO-2020249599-A1 |
| titleOfInvention |
Gas turbine engine and heat management system for cooling oil in an oil system of a gas turbine engine |
| abstract |
The invention regards a gas turbine engine for an aircraft that comprises a nacelle, a fan, an engine core, a bypass duct extending between the engine core and the nacelle and guiding a bypass airflow through the bypass duct, and at least one non-structural strut (4) extending in the radial direction within the bypass duct, wherein the non-structural strut (4) comprises an outside wall (40) acting as a heat exchanger, and wherein the outside wall (40) includes first transport means (53) configured to transport in the outside wall (40) at least one fluid (60) to be cooled. It is provided that the non-structural strut (4) further comprises second transport means (54) configured to transport a fluid (80) to be heated, wherein the first transport means and the second transport means are configured such that the fluid (80) to be heated is heated by the at least one fluid (60) to be cooled and the at least one fluid (80) to be cooled (60) is cooled both by the bypass airflow (B) and the fluid (80) to be heated. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/WO-2023030867-A1 |
| priorityDate |
2019-06-14^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |