Hybrid axial/cross-flow fan multi-rotor aerial vehicle
First Claim
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1. A hybrid axial/cross-flow fan multi-rotor aerial vehicle comprising:
- an airfoil shaped wing body having a center of mass, a payload space located at the center of mass of the airfoil shaped wing body and a trailing edge;
at least three axial fans spaced around the center of mass of the wing body;
at least one cross-flow fan propulsor located behind the center of mass and the axial fans and embedded within the trailing edge of the wing body; and
a control system allowing transition from hover to forward flight by increasing power transmitted to the cross-flow fan propulsor and decreasing power transmitted to the axial fans;
wherein the axial fans only produce vertical thrust and the cross-flow fan propulsor produces only horizontal thrust.
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Abstract
A hybrid axial/cross-flow fan aerial vehicle includes both axial and cross-flow fan propulsion for efficient hover and forward flight performance. The axial fans provide primarily vertical thrust, while the cross-flow fan provides horizontal, as well as vertical, thrust. The vehicle takes off vertically, is capable of hover, and can fly forward by vectoring the thrust of the cross-flow fan system. This approach provides large internal cargo capacity and high forward flight speeds.
31 Citations
11 Claims
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1. A hybrid axial/cross-flow fan multi-rotor aerial vehicle comprising:
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an airfoil shaped wing body having a center of mass, a payload space located at the center of mass of the airfoil shaped wing body and a trailing edge; at least three axial fans spaced around the center of mass of the wing body; at least one cross-flow fan propulsor located behind the center of mass and the axial fans and embedded within the trailing edge of the wing body; and a control system allowing transition from hover to forward flight by increasing power transmitted to the cross-flow fan propulsor and decreasing power transmitted to the axial fans; wherein the axial fans only produce vertical thrust and the cross-flow fan propulsor produces only horizontal thrust. - View Dependent Claims (2)
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3. A hybrid axial/cross-flow fan multi-rotor aerial vehicle comprising:
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an airfoil shaped wing body having a center of mass, a payload space located at the center of mass of the airfoil shaped wing body and a trailing edge; and at least six axial fans spaced around the center of mass of the wing body; at least one cross-flow fan propulsor located behind the center of mass and the axial fans and embedded within the trailing edge of the wing body; and a control system allowing transition from hover to forward flight by increasing power transmitted to the cross-flow fan propulsor and decreasing power transmitted to the axial fans; wherein half of the axial fans rotate in the clockwise direction and half of the axial fans rotate in the counter-clockwise direction; wherein the axial fans only produce vertical thrust and the cross-flow fan propulsor produces only horizontal thrust. - View Dependent Claims (4)
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5. A hybrid axial/cross-flow fan multi-rotor aerial vehicle comprising:
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an airfoil shaped wing body having a center of mass, a payload space located at the center of mass of the airfoil shaped wing body and a trailing edge; at least three axial fans spaced around the center of mass of the wing body; at least one cross-flow fan propulsor located behind the center of mass and the axial fans and embedded within the trailing edge of the wing body; and a control system allowing transition from hover to forward flight by increasing power transmitted to the cross-flow fan propulsor and decreasing power transmitted to the axial fans; wherein, in forward flight, the cross-flow fan propulsor produces horizontal thrust and the axial fans provide roll, pitch, and yaw control through differential rotor speed. - View Dependent Claims (6)
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7. A hybrid axial/cross-flow fan multi-rotor aerial vehicle comprising:
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an airfoil shaped wing body having a center of mass, a payload space located at the center of mass of the airfoil shaped wing body and a trailing edge; and at least six axial fans spaced around the center of mass of the wing body; at least one cross-flow fan propulsor located behind the center of mass and the axial fans and embedded within the trailing edge of the wing body; and a control system allowing transition from hover to forward flight by increasing power transmitted to the cross-flow fan propulsor and decreasing power transmitted to the axial fans; wherein half of the axial fans rotate in the clockwise direction and half of the axial fans rotate in the counter-clockwise direction; wherein, in forward flight, the cross-flow fan propulsor produces horizontal thrust and the axial fans provide roll, pitch, and yaw control through differential rotor speed. - View Dependent Claims (8)
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9. A hybrid axial/cross-flow fan multi-rotor aerial vehicle comprising:
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an airfoil shaped wing body having a center of mass, a payload space located at the center of mass of the airfoil shaped wing body and a trailing edge; at least three axial fans spaced around the center of mass of the wing body; at least one cross-flow fan propulsor located behind the center of mass and the axial fans and embedded within the trailing edge of the wing body; and a control system allowing transition from hover to forward flight by increasing power transmitted to the cross-flow fan propulsor and decreasing power transmitted to the axial fans; wherein the axial fans produce primarily vertical thrust and the cross-flow fan propulsor produces primarily horizontal thrust. - View Dependent Claims (10, 11)
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Specification