The invention discloses aerocraft, the whole weight of the aerocraft can be reduced, the manufacturing cost is low, and the failure rate is lower. The aerocraft comprises a fuselage and an engine, wherein the engine is composed of a duct engine which is installed in the fuselage, an axial lead of the duct engine coincides with that of the fuselage, an airflow inlet of the duct engine is communicated with a confluence cavity which is formed in the fuselage and positioned at the outer side of the airflow inlet of the duct engine, an airflow outlet of the duct engine is communicated with a shunting cavity which is formed in the fuselage and positioned at the outer side of the airflow outlet of the duct engine, at least two air inlet ducts and at least two air outlet ducts are formed in the fuselage, air inlets are formed in the ends, which are far from the duct engine, of the air inlet ducts, air outlets are formed in the ends, which are far from the duct engine, of the air outlet ducts, all of the air inlet ducts are communicated with the confluence cavity, and all of the air outlet ducts are communicated with the shunting cavity.
Aerocraft
2015-05-06
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
COOPERATIVE PATH PLANNING METHOD AND DEVICE FOR AUTOMATIC CONTROL AEROCRAFT AND AEROCRAFT SYSTEM
European Patent Office | 2021
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