The present invention relates generally to golf clubs, and in particular to golf clubs with aerodynamic features.
The distance that a golf ball travels when hit by the face of a golf club is determined by the velocity of the club head at the moment of impact with the ball. Drag from the air may reduce the speed of the club head. Some golf clubs use grooves deployed along the top of the club head to decrease resistance and drag. However, the downward curvature of the top surfaces of traditional golf club heads may lead to separation of the airflow along the top, decreasing the efficiency of the upper grooves.
There is a need in the art for a golf club that addresses the shortcomings discussed above.
In one aspect, a golf club head for a driver includes a face portion providing a ball contacting surface, a rearward end portion, and a crown portion including an upward facing surface, where the upward facing surface extends from the ball contacting surface to the rearward end portion. The golf club head also includes a sole portion disposed opposite of the crown portion, where the sole portion includes a downward facing surface, and where the downward facing surface extends from the ball contacting surface to the rearward end portion. The sole portion includes an airfoil portion disposed adjacent the face portion. The ball contacting surface defines a reference axis approximately parallel with the ball contacting surface and oriented in a direction between the crown portion and the sole portion. A lower edge of the face portion has a first position along the reference axis, an upper edge of the face portion has a second position along the reference axis, and the rearward end portion has a third position along the reference axis. The third position is disposed further from the first position than is the second position from the first position.
In another aspect, a golf club head for a driver includes a shaft receiving portion, a face portion providing a ball contacting surface, a rearward end portion, and a crown portion including an upward facing surface, where the upward facing surface extends from the ball contacting surface to the rearward end portion. The golf club head also includes a sole portion disposed opposite of the crown portion, where the sole portion includes a downward facing surface, and where the downward facing surface extends from the ball contacting surface to the rearward end portion. The face portion has a toe portion and a heel portion, where the toe portion is disposed further from the shaft receiving portion than is the heel portion from the shaft receiving portion. The sole portion includes an airfoil portion disposed adjacent the face portion, and the airfoil portion extends at least seventy percent of the distance between the toe portion and the heel portion.
In another aspect, a golf club head for a driver includes a face portion providing a ball contacting surface, a rearward end portion, and a crown portion including an upward facing surface, where the upward facing surface extends from the ball contacting surface to the rearward end portion. The golf club head also includes a sole portion disposed opposite of the crown portion, where the sole portion includes a downward facing surface, and where the downward facing surface extends from the ball contacting surface to the rearward end portion. The sole portion includes an airfoil portion. The airfoil portion includes a raised suction surface disposed adjacent the face portion, a recessed suction surface disposed rearwardly of the raised suction surface, and an elliptic surface connecting the raised suction surface and the recessed suction surface.
Other systems, methods, features, and advantages of the invention will be, or will become, apparent to one of ordinary skill in the art upon examination of the following figures and detailed description. It is intended that all such additional systems, methods, features, and advantages be included within this description and this summary, be within the scope of the invention, and be protected by the following claims.
The invention can be better understood with reference to the following drawings and description. The components in the figures are not necessarily to scale, emphasis instead being placed upon illustrating the principles of the invention. Moreover, in the figures, like reference numerals designate corresponding parts throughout the different views.
Club head 104 may include a club head body portion 105 and shaft receiving portion 106 (also referred to as a hosel), as best seen in
As best seen in
Club head 104 may also include a crown portion 240 that includes an upward facing surface 241. Club head 104 may also include a sole portion 244 that includes a downward facing surface 245. Upward facing surface 241 may extend from an upper edge 224 of face portion 210 up to rearward end portion 216 in an approximately longitudinal direction. Downward facing surface 245 may extend from a lower edge 226 of face portion 210 up to rearward end portion 216 in an approximately longitudinal direction.
Club head 104 may incorporate an airfoil portion 272. As used herein, the term airfoil (or aerofoil) is any structure with curved surfaces that produces an aerodynamic force when moved through a fluid. As used herein, the term “fluid” may refer to any Newtonian Fluid. In other embodiments, airfoils could be used with Non-Newtonian Fluids.
Airfoil portion 272 may be disposed along downward facing surface 245. Furthermore, a leading end of airfoil portion 272 may associated with lower edge 226 of face portion 210. A trailing end of airfoil portion 272 may extend rearwardly (in the longitudinal direction) from the leading end. Thus, airfoil portion 272 may be disposed beneath face portion 210 and may help control the airflow along downward facing surface 245 during a swing, as discussed in further detail below.
Although the exemplary embodiment depicts an airfoil portion that extends through substantially the entire width of a club head, in other embodiments an airfoil portion could have a different width that still helps to maintain laminar airflow along the majority of sole portion 244. In some embodiments, an airfoil portion could extend through a width approximately in the range between 60%-100% of the width of the club head. In other embodiments, an airfoil portion could extend at least 70% of the width of the club head. In the exemplary embodiment, airfoil portion 272 extends at least 90% of the width of the club head.
As seen in
With respect to reference axis 302, lower edge 226 of face portion 210 has a first position 310, upper edge 224 has a second position 312 and rearward end portion 216 has a third position 314. Moreover, as seen in FIG. 3, third position 314 is disposed further from first position 310 than second position 312 is from first position 310. That is, with respect to reference axis 302, rearward end portion 216 is “higher” than upper edge 224 of face portion 210. In still other embodiments, upward facing surface 241 could be approximately flat, so that rearward end portion 216 and upper edge 224 have substantially similar positions with respect to reference axis 302. As discussed in further detail below, by shaping the upward facing surface so that the rearward end portion is higher than the face portion, and/or at a similar height with respect to a suitable reference axis, airflow passing over the crown side of the club head may not separate from the club head. By contrast, in configurations where the rearward end portion of a club head is lower than the upper edge of the face portion, airflow may have a tendency to separate from the crown side of the club during a swing.
As seen in
An airfoil may include provisions for keeping airflow “stuck” on the suction surface and allowing air to be redirected through a large angle. In some embodiments, an airfoil can include a leading airfoil portion that is shaped to control the flow of air along a suction surface.
Referring back to
In some embodiments, an airfoil portion could include an elliptic surface. An elliptic surface may be used to connect the raised and lowered suctions surfaces of an airfoil. In the embodiment of
The embodiments could make use of any of the airfoil properties, including airfoil shapes, which are disclosed in Suk et al., U.S. Patent Publication Number 2019/0202503, currently U.S. patent application Ser. No. 15/969,347, filed May 2, 2018, and titled “Airfoils and Machines Incorporating Airfoils,” the entirety of which is herein incorporated by reference.
The more severe slope of downward facing surface 245 requires the use of airfoil portion 272 to maintain laminar flow along the bottom of the club head. Specifically, a second airflow path 404 initially passes across raised suction surface 350 of airfoil portion 272. Next, the second airflow path 404 is directed across elliptic surface 354 to recessed suction surface 352. As the air flows along the trailing end of airfoil portion 272 it will be turned up (that is, towards rearward end portion 216) to keep it from separating from downward facing surface 245.
As seen in the enlarged view within
The embodiments utilize specifically curved arc portions adjacent step-down region 410 to help actively control the turbulent eddies or vortices that develop at step-down region 410. Specifically, the combined shapes of raised suction surface 350, elliptic surface 354 and recessed suction surface 352 combine to actively redirect the fluid flow with use of the Coandă effect toward reattachment to the airfoil upper surface. The Coandă effect refers to the tendency of a jet of fluid emerging from an orifice to follow an adjacent flat or curved surface and to entrain fluid from the surroundings so that a region of lower pressure develops. Vortex 420 (and/or turbulent eddies) at step-down region 410 creates a pressure difference between raised suction surface 350 and recessed suction surface 352. The active fluid flowing across these surfaces creates air curtain 422 (via the Coandă effect) that helps hold vortex 420 in place and keeps it attached to downward facing surface 245. Air curtain 422 thus provides a stabilizing force to keep vortex 420 in place, which further serves to prevent the boundary layer from delaminating from airfoil portion 272.
Referring to
While various embodiments of the invention have been described, the description is intended to be exemplary, rather than limiting, and it will be apparent to those of ordinary skill in the art that many more embodiments and implementations are possible that are within the scope of the invention. Any element of any embodiment may be substituted for another element of any other embodiment or added to another embodiment except where specifically excluded. Accordingly, the invention is not to be restricted except in light of the attached claims and their equivalents. Also, various modifications and changes may be made within the scope of the attached claims.
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