| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_4e3c804fb60c8285b549597da004115a |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D2027-026
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02T50-60 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D29-04
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C7-14
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C11-48
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K3-02 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C7-18 |
| filingDate |
2010-01-26^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_cb9bb108536162767c47cc752a4a74a7
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_ebc9a99dc80a31a1c2cd0ee0daedb50f |
| publicationDate |
2011-07-29^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
FR-2955616-A1 |
| titleOfInvention |
COOLING DEVICE FOR AN AIRCRAFT PROPELLER |
| abstract |
The invention relates to a propellant (1) for an aircraft comprising a turbomachine (8) housed in a nacelle (10) and a cooler (45) adapted to be traversed by a hot fluid to be cooled by heat exchange with external cold air audit cooler. The thruster (1) comprises an air stream (13) (1 3b) adapted to conduct pressurized air to an air duct (20) formed between an outer wall (6) and an inner wall (60) of the nacelle (10). The cooler has a volume cooling means (14) positioned in the air duct (20) and a surface cooling means (15), not connected to said volume cooling means, disposed at an outer wall (6, 101) of the aircraft. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10384793-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/FR-3018503-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/WO-2015136210-A1 |
| priorityDate |
2010-01-26^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |