The present invention relates to an aircraft comprising a fuselage, a lateral support wing (1) and propulsion assembly (100) mounted under the wing, the wing comprising at least two structural spars (11ba, 11bf) extending from the fuselage toward the tip of the wing, one of these (11ba) being upstream and the other (11bf) downstream, and the propulsion assembly comprising a gas generator (106) and at least two offset fans (102, 104) arranged on either side of the axis of the gas generator. The aircraft is characterized in that the offset fans (102, 104) are attached directly to one of the said spars (11ba, 11bf) and the gas generator (106) is attached directly to the two spars. In particular, with the leading edge of the wing forming a given sweep of angle (α) with the axis of the fuselage, the two offset fans (102, 104) are axially offset from one another.
AIRCRAFT WITH MULTIPLE FAN PROPULSION ASSEMBLY FIXED UNDER THE WING
2018-10-04
Patent
Electronic Resource
English
Aircraft with multiple fan propulsion assembly fixed under the wing
European Patent Office | 2021
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