A rear end section for an aircraft, having a fuselage, a v-tail, and a thruster assembly including at least one propulsion device installed to ingest and consume air forming a fuselage boundary layer, a control surface attached at the rearmost section of the rear end, and a casing covering at least part of the propulsion device such that an air inlet and an air outlet are defined between the casing and the propulsion device. The air inlet is configured to permit passage of the fuselage boundary layer towards the propulsion device. The air outlet is configured to direct the airflow exhausted from the propulsion device into the control surface, to divert the airflow and provide vectoring thrust for the aircraft.
REAR END SECTION FOR AN AIRCRAFT
04.11.2021
Patent
Elektronische Ressource
Englisch
Frame assembly for rear section of aircraft and rear section of aircraft
Europäisches Patentamt | 2020
|METHOD FOR MANUFACTURING A REAR SECTION OF AN AIRCRAFT AND AIRCRAFT REAR SECTION
Europäisches Patentamt | 2019
|Method for manufacturing a rear section of an aircraft and aircraft rear section
Europäisches Patentamt | 2022
|