Propeller blade indentations for improved aerodynamic performance and sound control
First Claim
1. An aerial vehicle comprising:
- a first motor configured to rotate a first propeller such that the first propeller generates a first lifting force;
the first propeller including;
a first hub that is coupled to the first motor so that the first motor can rotate the first propeller;
a first propeller blade extending from the first hub, the first propeller blade including;
a leading edge;
a tip;
a trailing edge;
a surface area of the first propeller blade that extends from the first hub to the tip and between the leading edge and the trailing edge, the surface area of the first propeller blade having an upper side, and a lower side; and
a first plurality of indentations formed in at least a portion of the surface area of the first propeller blade, the first plurality of indentations having a first depth and a first shape, wherein the first plurality of indentations increases a duration in which air passing over the first propeller blade remains attached to the first propeller blade; and
a second motor configured to rotate a second propeller such that the second propeller generates a second lifting force;
the second propeller including;
a second hub that is coupled to the second motor so that the second motor can rotate the second propeller;
a second propeller blade extending from the second hub, the second propeller blade including;
a leading edge;
a tip;
a trailing edge;
a surface area of the second propeller blade that extends from the second hub to the tip and between the leading edge and the trailing edge, the surface area of the second propeller blade having an upper side, and a lower side; and
a second plurality of indentations formed in at least a portion of the surface area of the second propeller blade, the second plurality of indentations having a second depth and a second shape, wherein the second plurality of indentations increases a duration in which air passing over the second propeller blade remains attached to the second propeller blade; and
wherein the first depth of the first plurality of indentations of the first propeller blade is different than the second depth of the second plurality of indentations of the second propeller blade.
1 Assignment
0 Petitions
Accused Products
Abstract
Sounds are generated by an aerial vehicle during operation. For example, the motors and propellers of an aerial vehicle generate sounds during operation. Disclosed are systems, methods, and apparatus for actively adjusting the position of one or more propeller blade treatments of a propeller blade of an aerial vehicle during operation of the aerial vehicle. For example, the propeller blade may have one or more propeller blade treatments that may be adjusted between two or more positions. Based on the position of the propeller blade treatments, the airflow over the propeller is altered, thereby altering the sound generated by the propeller when rotating. By altering the propeller blade treatments on multiple propeller blades of the aerial vehicle, the different sounds generated by the different propeller blades may effectively cancel, reduce, and/or otherwise alter the total sound generated by the aerial vehicle.
62 Citations
20 Claims
-
1. An aerial vehicle comprising:
-
a first motor configured to rotate a first propeller such that the first propeller generates a first lifting force; the first propeller including; a first hub that is coupled to the first motor so that the first motor can rotate the first propeller; a first propeller blade extending from the first hub, the first propeller blade including; a leading edge; a tip; a trailing edge; a surface area of the first propeller blade that extends from the first hub to the tip and between the leading edge and the trailing edge, the surface area of the first propeller blade having an upper side, and a lower side; and a first plurality of indentations formed in at least a portion of the surface area of the first propeller blade, the first plurality of indentations having a first depth and a first shape, wherein the first plurality of indentations increases a duration in which air passing over the first propeller blade remains attached to the first propeller blade; and a second motor configured to rotate a second propeller such that the second propeller generates a second lifting force; the second propeller including; a second hub that is coupled to the second motor so that the second motor can rotate the second propeller; a second propeller blade extending from the second hub, the second propeller blade including; a leading edge; a tip; a trailing edge; a surface area of the second propeller blade that extends from the second hub to the tip and between the leading edge and the trailing edge, the surface area of the second propeller blade having an upper side, and a lower side; and a second plurality of indentations formed in at least a portion of the surface area of the second propeller blade, the second plurality of indentations having a second depth and a second shape, wherein the second plurality of indentations increases a duration in which air passing over the second propeller blade remains attached to the second propeller blade; and wherein the first depth of the first plurality of indentations of the first propeller blade is different than the second depth of the second plurality of indentations of the second propeller blade. - View Dependent Claims (2, 3, 4, 5)
-
-
6. An aerial vehicle, comprising:
-
a frame; a first motor coupled to the frame; a first propeller coupled to and rotatable by the first motor, the first propeller including a first plurality of indentations having a first depth into a surface area of the first propeller; a second motor coupled to the frame; and a second propeller coupled to and rotatable by the second motor, the second propeller including a second plurality of indentations having a second depth into a surface area of the second propeller, wherein the first depth is different than the second depth. - View Dependent Claims (7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20)
-
Specification