| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_473c19bbc792a319a033952b2261a7d0 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D27-26
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D29-06 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F16M13-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D27-26
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D29-06
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F16M1-00 |
| filingDate |
2013-07-24^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate |
2017-02-14^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_4e01b67b43e2f05a20a5cf37f0cb61e2
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_dbd4451571c79c5b953653df9c4cd9db
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_008b70a264a59fc54df6fd8b952923b7
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_e372ea19b94b697c2e58a7d571900f2b |
| publicationDate |
2017-02-14^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
US-9567089-B2 |
| titleOfInvention |
Hybrid hinge and latch beam |
| abstract |
A hybrid beam for support of a nacelle panel of a jet engine is disclosed. The beam is comprised of a first longitudinal composite panel and a second longitudinal composite panel, wherein the first longitudinal composite panel is integrally affixed to the second longitudinal composite panel along a longitudinal edge. The composite panels form a composite beam structure that is substantially open with a cross-section that is generally “L-shaped”. A plurality of hinge stations are affixed to a first side of the first longitudinal composite panel and at least one track guide is disposed on a second side of the first longitudinal composite panel. The track guides receive a head portion of a slider that is fixed to the translating jet engine nacelle panel. Each hinge station further comprises a bushing for defining a center of rotation for the jet engine nacelle panel relative to the beam. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2016281539-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10093429-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11125112-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11780599-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11447260-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10508566-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2022297845-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11396854-B2 |
| priorityDate |
2012-07-24^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |