| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_85064195730733a28dd406335aa8e710 |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2220-80
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2200-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2220-10
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2220-323 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C3-20
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K5-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K7-16
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H02K44-04
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F03H1-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H02K44-00 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K7-16
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K5-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F03H1-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/H02K44-04 |
| filingDate |
2014-03-13-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_4954be66a3d8df1298bbde92ebe1f090 |
| publicationDate |
2016-12-29-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
US-2016377029-A1 |
| titleOfInvention |
Helicon yield plasma electromagnetic ram-scramjet drive rocket ion vector engine |
| abstract |
HYPERDRIVE receives continuous air breathing assistance from compressed atmospheric air through a high speed magnetically core driven turbine accelerator which resolves around a common flow path tunnel. The tunnel runs from the front to the back of the engine. It is assisted by a series of radial geometric ramjet engines that share the common flow path tunnel for hypersonic exhaust but has separate inlet air from a linear aerospike which governs mass flow of air, velocity of inlet air and pressure to the turbine and/or ramjets, as well as the positioning of the shock wave at the inlet to reduce aerodynamic drag. The ramjet is of hybrid engine design where it can also function as a scramjet, thus a ram-scramjet structure for combustion in a radial configuration about the engine (aft of an electrical compressor), where the common flow path tunnel also serves as a compression tunnel to compress air through a the constantly occurring series of compression shocks entering from and around the aerospike. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/DE-202023101056-U1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/DE-102023100265-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/DE-102023102094-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/DE-102023102766-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/DE-202023100401-U1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/DE-102023104158-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/DE-202023100548-U1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/DE-102023105496-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/DE-202023100801-U1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-109322762-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-111120235-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/DE-102022004989-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/DE-102022105464-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/DE-102022112269-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/DE-102022112677-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-114135457-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/WO-2022183920-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/AU-2020201929-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-112109924-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-113044246-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2018328282-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-111997853-A |
| priorityDate |
2013-03-15-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |