Aircraft with its fuselage suspended under the wing
First Claim
1. An aircraft comprising:
- a reference system determined by a longitudinal X axis oriented positively toward a front of the aircraft, a vertical Z axis perpendicular to the X axis and oriented positively toward a bottom of the aircraft and a lateral Y axis perpendicular to the plane defined by the X and Z axes and oriented positively toward a right side of the aircraft;
a wing affixed to an upper central part of the fuselage along the longitudinal X axis;
a set of rear airfoils situated behind the wing; and
propulsion engines mounted on the wing,wherein the wing, the set of rear airfoils and the propulsion engines are parts of an aero-propulsive unit, said aero-propulsive unit being a structure independent of the fuselage;
and wherein the aero-propulsive unit is connected to the fuselage by a six degrees of freedom connection system using arms the lengths of which are modified to control a position of the aero-propulsive unit relative to the fuselage along the X, Y and Z axes of the reference system of the aircraft and in rotation about the three axes X, Y and Z, during flight.
2 Assignments
0 Petitions
Accused Products
Abstract
An aircraft includes a reference system including a longitudinal X axis, a vertical Z axis perpendicular to the X axis, and a lateral Y axis perpendicular to the plane defined by the X and Z axes, a fuselage, a wing affixed to an upper central part of the fuselage, a set of rear airfoils situated behind the wing, and propulsion engines mounted on the wing, where the wing, the set of rear airfoils and the propulsion engines are parts of an aero-propulsive unit forming a structure independent of the fuselage, and where the aero-propulsive unit is connected to the fuselage by a six degrees of freedom connection system using arms with lengths modified to control a position of the aero-propulsive unit relative to the fuselage along the X, Y and Z axes and in rotation about the X, Y and Z axes, during flight.
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Citations
17 Claims
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1. An aircraft comprising:
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a reference system determined by a longitudinal X axis oriented positively toward a front of the aircraft, a vertical Z axis perpendicular to the X axis and oriented positively toward a bottom of the aircraft and a lateral Y axis perpendicular to the plane defined by the X and Z axes and oriented positively toward a right side of the aircraft; a wing affixed to an upper central part of the fuselage along the longitudinal X axis; a set of rear airfoils situated behind the wing; and propulsion engines mounted on the wing, wherein the wing, the set of rear airfoils and the propulsion engines are parts of an aero-propulsive unit, said aero-propulsive unit being a structure independent of the fuselage; and wherein the aero-propulsive unit is connected to the fuselage by a six degrees of freedom connection system using arms the lengths of which are modified to control a position of the aero-propulsive unit relative to the fuselage along the X, Y and Z axes of the reference system of the aircraft and in rotation about the three axes X, Y and Z, during flight. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17)
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Specification