| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_e3d8a4d18d94cd8373b4cd85951a1b94 |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2270-09 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K9-70
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C27-022
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K9-24
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C27-06
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D41-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C27-006
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C27-04
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K9-46
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D27-023
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K9-72
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K9-95 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-24
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C27-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-46
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-70
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D27-02
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-95
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-72 |
| filingDate |
2016-10-14-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_e36c26e99190d4656db083816979dc50
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_1225a0c883eb9eff7fcc2a1449239245
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_93af78220bc43fdb87784265cccf6ee5 |
| publicationDate |
2018-11-08-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
US-2018319486-A1 |
| titleOfInvention |
Thrusting rockets for enhancing emergency autorotation |
| abstract |
There is provided, in accordance some embodiment, a method for enhancing autorotation performance of a rotary-wing aircraft in emergency events. The method comprises an action of receiving a request for emergency thrust from a user interface. The method comprises an action of sending a start command to an emergency engine coupled to a rotary-wing aircraft following the request. The method comprises an action of thrusting the rotary-wing aircraft coupled to the emergency engine in a direction substantially of a longitudinal axis of the rotary-wing aircraft, thereby enhancing autorotation performance of the rotary-wing air-craft in an emergency event. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2022144426-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2017015411-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11352900-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-210136-U1 |
| priorityDate |
2015-10-13-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |