| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_ac3e5cf3529cc355c01f69bf7883cbda |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F23R3-20
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K7-18
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K9-72
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F23R3-24 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-72
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K7-18
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F23R3-20
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F23R3-24 |
| filingDate |
1970-04-21-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate |
1971-12-14-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_42ca1e0afeaa9ee589b39a76c7488756 |
| publicationDate |
1971-12-14-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
US-3626698-A |
| titleOfInvention |
Combustion chamber construction and method of operating a combustion chamber |
| abstract |
A ROCKET TYPE RAM JET ENGINE INCLUDES A CENTRALLY ARRANGED STREAMLINED DISPLACEMENT MEMBER WHICH DEFINES AN ANNULAR INLET FOR COMBUSTION AIR AND WHICH PROVIDES A RESERVOIR FOR A FUEL COMPONENT AND A PRESSURE GAS FOR ATOMIZING THE COMPONENT IN A CATALYST CHAMBER. THE ATOMIZED FUEL COMPONENT IS DIRECTED INTO A DECOMPOSITION GAS CHAMBER WHERE IT IS DECOMPOSED AND A PORTION OF THE DECOMPOSED GAS IS DIRECTED THROUGH THE WALLS OF THE COMBUSTION CHAMBER FOR DISCHARGE THROUGH ONE OR MORE FUEL NOZZLES IN A COUNTERFLOW DIRECTION IN A MAIN COMBUSTION CHAMBER. THE DECOMPOSITION GASES ARE INTRODUCED INTO THE MAIN COMBUSTION CHAMBER AT A LOCATION DOWNSTREAM OF THE DISCHARGE FROM THE DECOMPOSITION GAS CHAMBER. THE COMBUSTION CHAMBER IS OPERATED WITH DECOMPOSITION GASES WHICH ARE OBTAINED FROM HYDRAZINE OR ITS DERIVATIVES BY CATALYTIC DECOMPOSITION. THE FIRST QUANTITY OF THE DECOMPOSITION GAS IS INTRODUCED CENTRALLY INTO THE MAIN COMBUSTION CHAMBER AND A SECOND PARTIAL GAS QUANTITY IS INJECTED BY NOZZLES INTO THE MAIN COMBUSTION CHAMBER DOWNSTREAM OF THE MAIN INTRODUCTION AND COUNTER TO THE FLOW THEREOF. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2015300292-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2689331-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-104295406-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-104295406-B
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-6112512-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-6679048-B1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-4896501-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-110475963-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2013313333-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2017096965-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2009205311-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/EP-3156636-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-108457768-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11555471-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-3791140-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9879636-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-109184953-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/FR-3042228-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-H01244153-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11703225-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9297334-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-8056319-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2009205309-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10794329-B2 |
| priorityDate |
1969-05-24-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |