| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_83d05675d70d8a0bc4c39ed076991c55 |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02M37-20
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02T10-12
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02B2275-18
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02B2075-1816
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02B2075-027 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02M37-0017
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02B61-045
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02M37-007
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02M37-0088
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02M31-20
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02M37-0052
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02B75-20 |
| classificationIPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02M37-20
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02B75-18
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02B75-02 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02B75-20
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02M37-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02B29-04
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02B61-04
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02M31-20 |
| filingDate |
1999-04-28-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_e20f4faf2fcd5989c0a37f5276e50bbb
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_c2232c0b0e7235093d7ac93eb3366270
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_61755b0eea3a76ecbfd7f1a12d4c9322 |
| publicationDate |
2000-10-31-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
JP-2000303845-A |
| titleOfInvention |
Propulsion engine |
| abstract |
(57) [Summary] [PROBLEMS] To improve fuel cooling efficiency and to easily secure an arrangement space. An engine in which cylinders are arranged in a vertical direction. A fuel supply system B for supplying fuel to each cylinder is provided. The fuel supply system B is provided with a delivery pipe 46 for distributing fuel to an injector 51 for injecting fuel. The fuel is supplied through the fuel supply passages 42 and 45 by the In a propulsion engine in which a vapor separator 44 is disposed at each of the fuel separators 2 and 45 and excess fuel from a delivery pipe 46 is returned to the vapor separator 44 via a fuel return passage 47, a fuel supply passage and / or a fuel A fuel cooling device C for cooling the fuel in the return passage is provided. |
| priorityDate |
1999-02-18-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |