PROPULSION ASSEMBLY FOR AN AIRCRAFT, COMPRISING A GAS GENERATOR AND TWO OFFSET FANS
According to the invention, the propulsion assembly (10) comprises an air inlet fairing formed upstream of a nacelle (25) connecting the fans, said fairing (15) having, between the fans (12), an air inlet opening (17, 17′) lying substantially perpendicular to the fan plane and on either side of this...
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Main Authors | , , |
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Format | Patent |
Language | English |
Published |
18.05.2017
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Subjects | |
Online Access | Get full text |
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Summary: | According to the invention, the propulsion assembly (10) comprises an air inlet fairing formed upstream of a nacelle (25) connecting the fans, said fairing (15) having, between the fans (12), an air inlet opening (17, 17′) lying substantially perpendicular to the fan plane and on either side of this plane, the propulsion assembly further comprising an air supply device configured so as to supply the gas generator (11) with a part of the incoming air and to take off, from the remaining part of the incoming air, a cooling airflow intended to cool elements of the propulsion assembly and/or a wing supporting the propulsion assembly. |
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Bibliography: | Application Number: US201615346612 |