BOUNDARY LAYER SUCTION DESIGN BY USING A CORE OF A WINGTIP VORTEX FOR A LIFT-GENERATING BODY

Abstract

A boundary layer suction design uses a wingtip vortex core for a lift-generating body with optimized aerodynamic performances. Holes or slots (6), connected to a core or center of a wingtip vortex of the lift generating body via a plenum (9) and pipe (7) with its outlet (8) sticking out from a surface (1) experiencing low pressure, sucked a part of the boundary layer to delay flow transition or separation. Thus, with a more stable boundary layer, the lift is increased while the drag is reduced.

Claims

1. An apparatus with a boundary layer suction design by using a core of a wingtip vortex for a lift-generating body, the apparatus comprising: a lift-generating body with a tip (5) and one surface (2) experiencing a higher pressure than another surface (1); a leading edge (3) and a trailing edge (4); a hole or slot (6) placed on one of the surfaces of the lift-generating body; a plenum (9) embedded in the lift-generating body; characterize by a pipe or channel (7) protruding from a surface of the lift-generating body near the tip (5) and the trailing edge (4) with an outlet (8) extended into the core of the wingtip vortex.

2. The boundary layer suction design by using a core of a wingtip vortex for a lift-generating body according to claim 1, wherein multiple holes or slots (11) are placed on the surface of the lift-generating body and are all connected to the core of a wingtip vortex via multiple plena (10).

3. The boundary layer suction design by using a core of a wingtip vortex for a lift-generating body according to claim 1, wherein a plenum (9) or multiple plena (10) are connected to a core of a wingtip vortex via multiple pipes or channels (12).

Description

BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWINGS

[0009] Having described the invention in general terms, reference will be made to the accompanying drawings, which are not necessarily drawn to scale, and wherein:

[0010] FIG. 1 shows a perspective view of a lift-generating body;

[0011] FIG. 2 shows a perspective view of the lift-generating body with the embedded plenum;

[0012] FIG. 3 shows a perspective view of the lift-generating body with multiple plena;

[0013] FIG. 4 shows a perspective view of the lift-generating body.

DETAILED DESCRIPTION OF THE INVENTION

[0014] The present invention will be described more exhaustively hereinafter with reference to the accompanying drawings, in which some, but not all the embodiments of the invention are shown. Indeed, the invention may be embodied in many different forms and should not be construed as limited to the embodiments set forth herein; rather, the embodiments are provided so that the disclosure will satisfy applicable legal requirements. Like numbers refer to like elements throughout.

[0015] Lift is an aerodynamic force created by the relative motion between a body and a fluid. The body has a leading edge 3 and a trailing edge 4. The imaginary line that directly connects the leading edge 3 to the trailing edge 4 is called the chord. One surface called intrados 2 experiences a higher pressure than another surface on the body called extrados 1. This pressure gradient increases when the body's angle of attack, which is the angle between the direction of motion and the chord, augments until it reaches the critical angle of attack. At the tip of the body 5, a low-pressure area starts to develop within a vortex. That vortex will create an area of low pressure, which is strongest at its center called the core. The core will move onto the upper surface 1 and achieve minimum pressure from the surface 1 and the trailing edge 4 near the tip 5. A pipe or channel 7, protruding from the upper surface 1 near the tip 5 and connected to a plenum 9, extends into the wingtip vortex core. The pipe or channel's outlet 8 present into the wingtip vortex creates a low-pressure area inside the plenum 9 embedded in the lift-generating body. Any hole or slot 6 on the surface and connected to the plenum 9 will be an area of low-pressure. When the pressure in the plenum 9 is lower than the pressure on the extrados 1 at a location where a hole or slot 6 is present, part of the boundary layer on the surface 1 will be sucked into the plenum 9 and expelled at the outlet 8.

[0016] When the angle of attack varies in a manner such that there is an inversion of the pressure gradient, meaning that 1 becomes the intrados and 2 the extrados, part of the boundary layer is still sucked into the plenum 9. If there is a sufficient pressure gradient, the design presented herein will still work. However, the boundary layer on an intrados is more stable than the boundary layer on an extrados. Thus, it is more pertinent to apply the suction on the boundary layer located on the extrados for significant gains in lift and substantial reduction of drag. Furthermore, there is a natural corrective effect of the pressure inside the plenum while varying the angle of attack. When the angle of attack increases, the pressure inside the plenum 9 decreases because the vortex core at the outlet 8 gets stronger.

[0017] The lift-generating body tip 5 can be rounded or curved to increase the wingtip vortex core's strength.

[0018] In specific cases, the pressure inside the plenum 9 may be regulated for optimal performance at different speeds. For such circumstances, a valve system is added to the plenum 9.

[0019] The present invention applies to a wing, or rotor blade, or winglets. Many systems like compressor blades, turbines, aircraft wings, wind turbines, or pumps are made of lift-generating bodies. This invention can enhance any device acting on a fluid.