| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_266d9649b95afb489069afb7f323b820
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_3a1fe38d95ee4b535c566ed46f8da03c
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_2740d4d5d428a041ec42a3fe569a339a
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_6549b05050b4e1cf326c5d2a36803110
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_c721fe8dc4d1b8f924e7e673bd5c2edb |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y10T29-49826
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D2041-002 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D41-00 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D27-00 |
| filingDate |
2010-12-17-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate |
2013-04-09-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_bd0e13c7b00f5133935a69f7d701e8d0
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_282716b5b4000ed84392c771563292f3
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_ae517346a3818a0322b504d1dc591440
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_f2b873e33a95f09ec6614e428295d6b9 |
| publicationDate |
2013-04-09-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
US-8413926-B2 |
| titleOfInvention |
Aircraft auxiliary power unit suspension system for isolating an aircraft auxiliary power unit |
| abstract |
The invention provides an aircraft with an auxiliary power unit isolated from the aircraft. An auxiliary power unit suspension system includes at least one suspension linkage. The suspension linkage terminates with a first low stiffness elastomeric rod end. The low stiffness elastomeric rod end has a low spring rate with the aircraft auxiliary power unit suspension system providing the aircraft auxiliary power unit with a suspended auxiliary power unit natural frequency, the suspended auxiliary power unit natural frequency below the aircraft auxiliary power unit operation frequency. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9469412-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2015298815-A1 |
| priorityDate |
2005-04-04-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |