Wingtip shield
Wingtip shields are described. In one embodiment, a wingtip shield includes an inner surface facing a high-pressure side of an airfoil. The airfoil is attached to the main body. The wingtip shield also includes an outer surface configured opposite from the inner surface. The wingtip shield is attachable to the airfoil along a peripheral edge of the airfoil from a first point of a leading edge of the airfoil to a second point of a trailing edge of the airfoil. A first span distance from the first point at the leading edge to the main body is less than a second span distance of the second point at the trailing edge to the main body.
1. An aircraft structure, comprising:
an airfoil having a high-pressure side and a low-pressure side, wherein the airfoil is configured for attaching to a main body; and
a wingtip shield having an inner surface and an outer surface opposite from the inner surface, the inner surface configured for facing towards and extending over the high-pressure side of the airfoil such that the inner surface orthogonally projects over the high-pressure side of the airfoil, wherein a space between the inner surface and the high-pressure side of the airfoil is configured for inducing a fluid flow at a leading edge of the airfoil to at least partially enter the space between the inner surface and the high-pressure side of the airfoil, and wherein, when viewed from the high-pressure side of the airfoil, the wingtip shield is shaped as a generally triangular shape having two edges that meet in a point projecting over the high pressure side of the airfoil,
wherein the wingtip shield is attachable to the airfoil along a peripheral edge of the airfoil from a first point of the leading edge of the airfoil to a second point of a trailing edge of the airfoil, and wherein a first space distance from the first point at the leading edge to the main body is less than a second space distance of the second point at the trailing edge to the main body.
2. The aircraft structure of claim 1 , wherein the airfoil is a wing of an aircraft, and the main body is a fuselage of the aircraft.
3. The aircraft structure of claim 1 , wherein the airfoil is a blade of boat propeller and the main body is a shaft of the boat propeller.
4. The aircraft structure of claim 1 , wherein the airfoil is a blade of an aircraft propeller, and the main body is a shaft of the propeller.
5. The aircraft structure of claim 1 , wherein the airfoil is a blade of a helicopter or a gyrocopter, and wherein the main body is a shaft of the helicopter or the gyrocopter.
6. The aircraft structure of claim 1 , wherein the airfoil is a blade of a wind turbine, and the main body is a shaft of the wind turbine.
7. The aircraft structure of claim 1 , wherein the wingtip shield is removably attached to the airfoil.
8. The aircraft structure of claim 1 , wherein the wingtip shield is fixedly attached to the airfoil.
9. The aircraft structure of claim 1 , wherein the wingtip shield is configured for:
accelerating the fluid flow from the leading edge when entering a space between the inner surface of the wingtip shield and the high-pressure side of the airfoil,
changing a direction of the fluid flow when flowing in the space between the inner surface of the wingtip shield and the high-pressure side of the airfoil, and
based on changing the direction of the fluid flow, changing a fluid flow momentum and a forward force directed toward the leading edge of the airfoil, wherein the wingtip shield is configured for absorbing the forward force.