http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9527598-B2
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_266d9649b95afb489069afb7f323b820 http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_c721fe8dc4d1b8f924e7e673bd5c2edb http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_485c75421f75c894a689fe273f644263 |
| classificationCPCAdditional | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y10T29-49826 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D2027-262 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D27-20 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D27-02 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D27-26 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D27-20 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D27-26 |
| filingDate | 2010-01-26-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate | 2016-12-27-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_3a2dfff3e753d77425492df0b8756273 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_e95d18d0447d661bafe0766fdf81c486 |
| publicationDate | 2016-12-27-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | US-9527598-B2 |
| titleOfInvention | Aircraft engine mounting system and method of mounting aircraft engines |
| abstract | In an embodiment the invention includes an aircraft engine mounting system ( 20 ) for mounting an aircraft engine to an aircraft. The aircraft engine mounting system preferably includes an airframe structure member having a first engine end ( 28 ) and a distal second engine end ( 30 ), with an aircraft attachment between the first engine end and the distal second engine end, the aircraft attachment for interfacing the airframe structure member with the aircraft, the airframe structure member having an airframe structure member length (YL) from the first engine end to the distal second engine end. The aircraft engine mounting system preferably includes a first engine attachment structure member ( 36 ), the airframe structure member first engine end ( 28 ) contained by the first engine attachment structure member, with the first engine attachment structure member having an outer engine mount member ( 38 ) grounded to the aircraft engine. The aircraft engine mounting system preferably includes a second engine attachment structure member ( 40 ), the airframe structure member second engine end ( 30 ) contained by the second engine attachment structure member, with the second engine attachment structure member having an outer engine mount member ( 42 ) grounded to the aircraft engine. The aircraft engine mounting system preferably includes the first engine attachment structure member ( 36 ) and the second engine attachment structure member ( 40 ) grounded to the aircraft engine with a mounts spacing (MS) between the first engine. |
| isCitedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11697506-B2 |
| priorityDate | 2009-01-26-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 25.