patent/GB-1072712-A

Predicate	Object
assignee	http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_13ef102659c1a496330aeae6979abc83
classificationCPCInventive	http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L1-04 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10G69-126
classificationIPCInventive	http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C10L1-04 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C10G69-12
filingDate	1965-01-26-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor	http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_df809a8d4f3564d992505d06975215c1
publicationDate	1967-06-21-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber	GB-1072712-A
titleOfInvention	Improvements relating to fuels for supersonic jet aircraft
abstract	Fuels for supersonic jet aircraft comprise a saturated aliphatic hydrocarbon composition boiling in the range 204-288 DEG C. and having a freezing point of less than -50 DEG C. and a flash point greater than 60 DEG C., and prepared by oligomerizing one or more C2 to C6 olefines to give polymers having carbon numbers in the range C12 to C18 and fully hydrogenating the product. The monomers may be propylene, n-butylene, iso-butylene or short chain olefine mixtures derived from cracking of petroleum.
priorityDate	1964-01-28-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type	http://data.epo.org/linked-data/def/patent/Publication

Predicate	Subject
isDiscussedBy	http://rdf.ncbi.nlm.nih.gov/pubchem/substance/SID425601984 http://rdf.ncbi.nlm.nih.gov/pubchem/substance/SID458393697 http://rdf.ncbi.nlm.nih.gov/pubchem/compound/CID297 http://rdf.ncbi.nlm.nih.gov/pubchem/compound/CID8255 http://rdf.ncbi.nlm.nih.gov/pubchem/substance/SID419559581 http://rdf.ncbi.nlm.nih.gov/pubchem/compound/CID7844 http://rdf.ncbi.nlm.nih.gov/pubchem/substance/SID425675739

Total number of triples: 20.