The aeroplane includes at least a fuselage, two wings, a rear tail unit including a horizontal tail provided with two tail ends, and at least two engines arranged on the fuselage on either side of a vertical plane of symmetry of the aeroplane. The aeroplane has a longitudinal axis. The engines are mounted so as to be able to be displaced, at least in flight, on the fuselage, substantially parallel to the longitudinal axis, and the tail ends are mounted so as to be able to be pivoted, at least in flight, relative to the horizontal tail. The aeroplane thus has a configuration that changes in flight.
Aeroplane With Configuration Changing In Flight
2019-06-06
Patent
Electronic Resource
English
Engineering Index Backfile | 1928
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