| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_c72d118f5664072de841f9c5c34b9d99 |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02T50-60
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2250-611
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2260-607 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C7-05
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K3-06 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K3-06
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K3-075
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C3-13 |
| filingDate |
2017-12-18-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_ca23d052c30f67cfdeed36832407c76a
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_242154bbdd85c3309f58e00eba7216f4 |
| publicationDate |
2018-07-12-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
WO-2018128791-A1 |
| titleOfInvention |
Protected core inlet |
| abstract |
A gas turbine engine defines a radial direction and an axial centerline. The gas turbine engine includes a core turbine engine that defines a core inlet. The core inlet is oriented with respect to the axial centerline and positioned along the radial direction such that the area available to capture foreign object debris is minimized. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/EP-4101646-A1 |
| priorityDate |
2017-01-05-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |