Aircraft with reduced environmental impact
View Patent ↗An aircraft includes a fuselage and at least one engine provided with at least one propeller and mounted at a rear part of the fuselage, on the back thereof, with the at least one engine having an axis substantially parallel to the longitudinal axis of the fuselage, where the at least one engine is mounted on the rear part of the fuselage so that the propeller lies forward of the tails, and provided at the rear part of the fuselage, symmetrically with respect to the fuselage, are removable noise masking surfaces configured to occupy either a deployed position in which the removable noise masking surfaces project laterally with respect to the rear part of the fuselage and are positioned plumb with the propeller, or a retracted position in which the removable noise masking surfaces are incorporated into the rear part of the fuselage.
1. An aircraft with reduced environmental impact comprising:
a fuselage, which has a longitudinal axis and a rear part which carries a horizontal tail and at least one vertical tail, and
at least one engine provided with at least one propeller and mounted at said rear part of the fuselage, on the back thereof, having an axis substantially parallel to said longitudinal axis of the fuselage,
wherein:
said engine is mounted on said rear part of the fuselage so that said propeller lies forward of said tails; and
provided at said rear part of the fuselage, symmetrically with respect to said fuselage, are removable noise masking surfaces configured to occupy:
a deployed position in which the removable noise masking surfaces project laterally with respect to said rear part of the fuselage and are positioned plumb with said propeller; and
a retracted position in which the removable noise masking surfaces are incorporated into said rear part of the fuselage.
2. The aircraft as claimed in claim 1 , wherein said propeller is positioned at the rear of said engine and is able to exert thrust on said aircraft.
3. The aircraft as claimed in claim 1 , wherein said propeller has no peripheral cowling.
4. The aircraft as claimed in claim 1 , wherein said engine comprises two contra-rotating coaxial propellers, said removable masking surfaces being, in the deployed position, positioned plumb with said two coaxial propellers.
5. The aircraft as claimed in claim 1 , wherein said removable noise masking surfaces are planar.
6. The aircraft as claimed in claim 5 , wherein said planar removable noise masking surfaces are able to move in terms of sliding in respective planes of said planar removable noise masking surfaces and wherein, in the retracted position, said planar removable noise masking surfaces are housed inside said rear part of the fuselage.
7. The aircraft as claimed in claim 1 , wherein said removable noise masking surfaces are curved.
8. The aircraft as claimed in claim 7 , wherein said curved removable noise masking surfaces are able to move in terms of rotation and wherein, in the retracted position, said curved removable noise masking surfaces are pressed against said rear part of the fuselage.
9. The aircraft as claimed in claim 8 , wherein, in the deployed position, said curved removable noise masking surfaces are positioned in such a way that concave sides of said curved removable noise masking surfaces face toward said propeller.