| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_a823cc54af48cb3e5431369a321c3616
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_2c0ada4ab18acf7d99df699b2aebef48 |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02T50-40
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02T50-10
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D2033-0226 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D27-26
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D27-20
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C7-02
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C5-02
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C15-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D33-02 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D27-20
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C15-00 |
| filingDate |
2017-11-14-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_d6a55631b0e28c172eadf9d1b36edbef
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_5042cad0421e251f77bcd180c512b742 |
| publicationDate |
2018-05-25-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
CN-108069035-A |
| titleOfInvention |
aircraft |
| abstract |
The invention relates to an aircraft (1) comprising: a fuselage (3) extending along a longitudinal axis (13) between a nose section (15) and a tail section (17); the wing (5) of the fuselage (3); the tail unit (7) mounted to the tail section (17) of the fuselage (3); and the tail unit (7) both mounted to the tail section (17) of the fuselage (3) The first propulsion unit (9) and the second propulsion unit (11) such that the first axis of rotation (19) of the first propulsion unit (9) and the second axis of rotation (21) of the second propulsion unit (11) are at Extends in a vertical center plane (23) passed by the longitudinal axis (13) and the yaw axis (25). The object of the present invention is to provide a centerline mounted twin-engine aircraft allowing simple manufacture, maintenance and retrofitting of the engines, which is realized in that the first propulsion unit (9) and/or the second propulsion unit (11) are arranged in the fuselage (3) EXTERNAL. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-111532426-A |
| priorityDate |
2016-11-14-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |