http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2020200097-A1
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_fd4735dbc2bd2bb60a1673344a4a95c1 |
| classificationCPCAdditional | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2250-38 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2260-40311 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02T50-60 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K3-06 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K3-02 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C7-057 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C9-18 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K1-06 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C9-18 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C7-057 |
| filingDate | 2019-05-28^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_627ee4194fa5b93e09349e3a09d6deff http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_fab80d14e1746dc5bbdd224ac4555127 |
| publicationDate | 2020-06-25^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | US-2020200097-A1 |
| titleOfInvention | Turbofan gas turbine engine with bypass duct |
| abstract | A gas turbine engine for an aircraft including: an engine core; a fan located upstream of engine core, fan including a plurality of fan blades; a nacelle surrounding the gas turbine engine, nacelle including an inner surface at least partly defining a bypass duct; and a bypass duct outlet guide vane extending radially across bypass duct between the engine core's outer surface and the nacelle's inner surface. An outer wall axis is defined joining a radially outer tip of a trailing edge of the bypass duct outlet guide vane and a rearmost tip of the inner surface of the nacelle, wherein the outer wall axis lies in a longitudinal plane containing the centreline of gas turbine engine, an outer bypass duct wall angle is defined as the angle between outer wall axis and centreline, and the outer bypass duct wall angle is in a range between −15 to 1 degrees. |
| isCitedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10844721-B2 |
| priorityDate | 2018-12-21^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
| Predicate | Subject |
|---|---|
| isDiscussedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/substance/SID419545405 http://rdf.ncbi.nlm.nih.gov/pubchem/compound/CID91778 |
Showing number of triples: 1 to 23 of 23.