| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_0952a993ee98c37a5569427f57b85836 |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D2041-005
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F17C2205-0134
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H01M2250-20
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F17C2203-067
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D2211-00 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F17C1-06
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D37-02
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64G1-423
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D37-04
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D37-30
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H01M8-04201
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H01M8-0656 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D37-30
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64G1-42
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D37-04
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/H01M8-04082
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/H01M8-0656 |
| filingDate |
2019-11-14^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_0b7ff4b3ce9772047cb1643384ab8e32
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_c6ffbf7616d9be921db160c79756bd1f
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_a595d8b07259fb74988ade4a5c88b79f |
| publicationDate |
2020-05-28^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
US-2020165012-A1 |
| titleOfInvention |
Device for carrying fuel in an aircraft and spacecraft |
| abstract |
Disclosed is a device for carrying fuel in aircraft and spacecraft. The device includes a carrier element having a longitudinal axis, and a fuel tank with a side wall and a chamber at least partially delimited by the side wall. The tank is arranged in the carrier element. The chamber and the side wall extend in a direction along the longitudinal axis. The side wall has a pressure-receiving component that converts a pressure from the chamber on the side wall into a contraction force acting on the side wall along the longitudinal axis. The contraction force compensates for an expansion force, resulting from the pressure from the chamber and acting on the side wall along the longitudinal axis. This provides an improved device for carrying fuel in aircraft and spacecraft, wherein the aircraft and spacecraft has constant flight mechanical properties because of the device. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11565607-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11434014-B2 |
| priorityDate |
2018-11-27^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |