| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_f3a1da6bfa25f2c9b159622afaf2b43c |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29L2031-7172
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B60K2015-03217
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02T50-40
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29K2307-04 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D37-02
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G01F23-263
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D37-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G01F23-268
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D37-06
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G01F23-284
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B60K15-03177
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C3-34
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29C70-885 |
| classificationIPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B29K307-04
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B29L31-00 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G01F23-26
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D37-06
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B29C70-88 |
| filingDate |
2017-06-21^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_c34d40b6dd9f1623a4e263a9de75f9cf |
| publicationDate |
2017-12-28^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
US-2017368769-A1 |
| titleOfInvention |
Method of forming a structural portion of a fuel tank for an aircraft |
| abstract |
The present application relates to a method of forming a structural portion of a fuel tank for an aircraft in which the structural portion is formed from a fibre reinforced polymer and a sensor is integrated in the structural portion. The method includes providing a fibre ply which acts as a structural component, and embroidering an electrically conductive wire in a predetermined pattern on the fibre ply to form the sensor. The fibre ply acts as a sensor substrate. Furthermore, the method includes applying a polymer matrix to the fibre ply so that the fibre ply and electrically conductive wire are covered by the polymer matrix. The present application also relates to a fuel tank for an aircraft, a fuel quantity indicating system, and an aircraft. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2018230631-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/WO-2021186436-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2021184392-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10953624-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11735860-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2017246833-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11559918-B2 |
| priorityDate |
2016-06-22^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |