Abstract:
An airfoil wing system for releasing air from an airfoil wing for an inflatable airfoil is provided. The airfoil wing is secured to the inflatable airfoil. The airfoil wing system comprises at least two wing panels connected together and an opening formed between the two wing panels wherein the opening automatically moves from a closed position to an open position to release air from beneath the airfoil wing thereby allowing takedown of the inflatable airfoil.

Description:
[0001]    The present application is a continuation-in-part of pending U.S. patent application Ser. No. 12/462,085, filed on Jul. 29, 2009, entitled “High Wind Release Vent for Inflatable Airfoils, which is a continuation-in-part of pending U.S. patent application Ser. No. 12/386,232, filed on Apr. 15, 2009, entitled “Adjustable Wing Line Apparatus for Inflatable Airfoils”. 
     
    
     BACKGROUND OF THE INVENTION 
       [0002]    1. Field of the Invention 
         [0003]    This invention relates generally to an airfoil wing system for inflatable airfoils and, more particularly, the invention relates to an airfoil wing system for inflatable airfoils assisting in a controlled flight of the inflatable airfoil and allowing venting an airfoil wing during high wind conditions during flight. 
         [0004]    2. Description of the Prior Art 
         [0005]    There are numerous inflatable devices for providing location information; however, these devices are cumbersome, are not simple to operate, will not fly under windy conditions, are driven to the ground in high wind conditions, have no maneuverability, and are dangerous to bring back to the ground in a controlled manner. MacFadden, U.S. Pat. No. 3,395,877, claims a aerodynamically stable site marker balloon capable of being tethered under adverse flight condition. However, although MacFadden may fly where the spherical balloon will not, MacFadden will not fly and in fact will be driven to the ground in high wind conditions. 
         [0006]    Schnee, U.S. Pat. No. 4,768,739, requires at least a light wind and has significant drawbacks in high winds as it would drag the individual. It claims the kite use as a sail. The Schnee device would be totally unusable in winds having velocity exceeding 20 miles per hour whereas the within invention will fly with wind velocity up to 80 miles per hour. Bringing the Schnee device to the ground during heavy winds can be a difficult if, if not impossible, task. 
         [0007]    Accordingly, there exists a need for an airfoil wing system for an inflatable airfoil allowing release of air from an airfoil flight to stabilize the inflatable airfoil during flight. Additionally, a need exists for an airfoil wing system for an inflatable airfoil wherein the openings in the airfoil wing automatically release air from within the airfoil wing to maximize flight and stability of the inflatable airfoil. Furthermore, there exists a need for an airfoil wing system for an inflatable airfoil wherein the airfoil wing is a para wing comprised of multiple wing panels allowing further control over the flight of the inflatable airfoil. 
       SUMMARY 
       [0008]    The present invention is an airfoil wing system for releasing air from an airfoil wing for an inflatable airfoil provided. The airfoil wing is secured to the inflatable airfoil. The airfoil wing system comprises at least two wing panels connected together and an opening formed between the two wing panels wherein the opening automatically moves from a closed position to an open position to release air from beneath the airfoil wing thereby allowing takedown of the inflatable airfoil. 
         [0009]    In addition, the present invention includes an airfoil wing system for releasing air from an airfoil wing for an inflatable airfoil. The airfoil wing is secured to the inflatable airfoil. The airfoil wing system comprises a plurality of wing panels divided into a plurality of vertical columns and a plurality of horizontal rows with each adjacent wing panel connected to each other adjacent wing panel and a plurality of openings with each opening formed between two adjacent wing panels and extending along the entire length of the connection between the wing panels wherein each opening automatically moves from a closed position to an open position to release air from beneath the airfoil wing thereby allowing takedown of the inflatable airfoil. 
         [0010]    The present invention further includes a method for releasing air from an airfoil wing for an inflatable airfoil. The airfoil wing is secured to the inflatable airfoil. The method comprises providing a plurality of wing panels, dividing the wing panels into a plurality of vertical columns and a plurality of horizontal rows, connecting each adjacent wing panel to each other adjacent wing panel, forming a plurality of openings, forming each opening between two adjacent wing panels, extending each opening along the entire length of the connection between the wing panels, moving each opening from a closed position to an open position, and releasing air from beneath the airfoil wing. 
     
    
     
       BRIEF DESCRIPTION OF THE DRAWINGS 
         [0011]      FIG. 1  is a perspective view illustrating an airfoil wing system, constructed in accordance with the present invention, for inflatable airfoils with openings formed in an airfoil wing allowing release of air from the airfoil wing to stabilize the inflatable airfoil during flight; 
           [0012]      FIG. 2  is a perspective view illustrating the airfoil wing of the airfoil wing system, constructed in accordance with the present invention, for inflatable airfoils with the airflow contacting the wing and at least some of the airflow being directed though the openings in the airfoil wing; 
           [0013]      FIG. 3  is a rear view illustrating the airfoil wing of the airfoil wing system, constructed in accordance with the present invention, for inflatable airfoils with openings in the wing and harness line securement points; 
           [0014]      FIG. 4  is a bottom plan view illustrating airfoil wing attachment location on the inflatable airfoil of the airfoil wing system, constructed in accordance with the present invention; and 
           [0015]      FIG. 5  is a top plan view illustrating the inflatable airfoil of the airfoil wing system, constructed in accordance with the present invention, with the placement of the harness lines indicated thereon. 
       
    
    
     DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS 
       [0016]    As illustrated in  FIGS. 1 and 2 , the present invention is an airfoil wing system, indicated generally at  10 , for an inflatable airfoil  12  allowing release of air from an airfoil wing  14  to stabilize the inflatable airfoil  12  during flight. Used in conjunction with the adjustable wing line apparatus described in U.S. patent application Ser. No. 12/386,232, incorporated by reference, or without the adjustable wing line apparatus  14 , the airfoil wing system  10  provides stability of the inflatable airfoil  12  in all flight conditions, especially during high wind conditions. In addition, the airfoil wing system  10  of the present invention allows air to escape from beneath the airfoil wing  14  thereby allowing the user to safely bring the inflatable airfoil  12  down to the ground even in high wind conditions. It should be noted that references to the ground and lines extending to the ground can be attached to devices that are located on or above the ground itself. 
         [0017]    The airfoil wing  14  of the airfoil wing system  10  of the present invention has at least two wing panels in a vertical column and/or a horizontal row. Preferably, the airfoil wing  14  has a plurality of wing panels divided into a plurality of vertical columns and a plurality of horizontal rows. Furthermore, the airfoil wing  14 , in a preferred embodiment as best illustrated in  FIG. 3 , has eighteen (18) wing panels divided into eight (8) columns  1 - 8  and three (3) rows a-c although having more or less wing panels divided into more or less columns and/or more or less rows is within the scope of the present invention. 
         [0018]    The first column  1  of the airfoil wing  14  of the airfoil wing system  10  of the present invention has a single left end wing panel  1   a.  In a preferred embodiment, the single left end wing panel  1   a  has a substantially triangular shape although constructing the single left end wing panel  1   a  with a different shape is within the scope of the present invention. 
         [0019]    The second column  2  of the airfoil wing  14  of the airfoil wing system  10  of the present invention has three wing panels  2   a,    2   b,    2   c  with the wing panel  2   a  connected to the wing panel  2   b  and the wing panel  2   b  connected to the wing panel  2   c.  The single left end wing panel  1   a  is connected to the wing panel  2   a  creating a first row a. In a preferred embodiment, each of the wing panels  2   a,    2   b,    2   c  has a substantially rectangular shape although constructing the wing panels  2   a,    2   b,    2   c  with different shapes is within the scope of the present invention. 
         [0020]    The third column  3  of the airfoil wing  14  of the airfoil wing system  10  of the present invention has two wing panels  3   a,    3   b,    3   c  with the wing panel  3   a  connected to the wing panel  3   b  and the wing panel  3   b  connected to the wing panel  3   c.  The wing panel  3   a  is connected to the wing panel  2   a  in the first row a, the wing panel  3   b  is connected to the wing panel  2   b  creating a second row b, and the wing panel  3   c  is connected to the wing panel  2   c  creating a third row c. In a preferred embodiment, each of the wing panels  3   a,    3   b  has a substantially rectangular shape and the wing panel  3   c  has a triangular shape although constructing the wing panels  3   a,    3   b,    3   c  with different shapes is within the scope of the present invention. 
         [0021]    The fourth column  4  of the airfoil wing  14  of the airfoil wing system  10  of the present invention has two wing panels  4   a,    4   b  with the wing panel  4   a  connected to the wing panel  4   b.  The wing panel  4   a  is connected to the wing panel  3   a  in the first row a and the wing panel  4   b  is connected to the wing panel  3   b  in the second row b. In a preferred embodiment, each of the wing panels  4   a,    4   b  has a substantially rectangular shape although constructing the wing panels  4   a,    4   b  with different shapes is within the scope of the present invention. 
         [0022]    The fifth column  5  of the airfoil wing  14  of the airfoil wing system  10  of the present invention has two wing panels  5   a,    5   b  with the wing panel  5   a  connected to the wing panel  5   b.  The wing panel  5   a  is connected to the wing panel  4   a  in the first row a and the wing panel  5   b  is connected to the wing panel  4   b  in the second row b. In a preferred embodiment, each of the wing panels  5   a,    5   b  has a substantially rectangular shape although constructing the wing panels  5   a,    5   b  with different shapes is within the scope of the present invention. 
         [0023]    The sixth column  6  of the airfoil wing  14  of the airfoil wing system  10  of the present invention has two wing panels  6   a,    6   b,    6   c  with the wing panel  6   a  connected to the wing panel  6   b  and the wing panel  6   b  connected to the wing panel  6   c.  The wing panel  6   a  is connected to the wing panel  5   a  in the first row a and the wing panel  6   b  is connected to the wing panel  5   b  in the second row b. In a preferred embodiment, each of the wing panels  6   a,    6   b  has a substantially rectangular shape and the wing panel  6   c  has a substantially triangular shape although constructing the wing panels  6   a,    6   b,    6   c  with different shapes is within the scope of the present invention. 
         [0024]    The seventh column  7  of the airfoil wing  14  of the airfoil wing system  10  of the present invention has three wing panels  7   a,    7   b,    7   c  with the wing panel  7   a  connected to the wing panel  7   b  and the wing panel  7   b  connected to the wing panel  7   c.  The wing panel  7   a  is connected to the wing panel  6   a  in the first row a, the wing panel  7   b  is connected to the wing panel  6   b  in the second row b, and the wing panel  7   c  is connected to the wing panel  6   c  in the third row c. In a preferred embodiment, each of the wing panels  7   a,    7   b,    7   c,  has a substantially rectangular shape although constructing the wing panels  7   a,    7   b,    7   c  with different shapes is within the scope of the present invention. 
         [0025]    The eighth column  8  of the airfoil wing  14  of the airfoil wing system  10  of the present invention has a single right end wing panel  8   a.  The single right end wing panel  8   a  is connected to the wing panel  7   a  in the first row a. In a preferred embodiment, the single right end wing panel  8   a  has a substantially triangular shape although constructing the single right end wing panel  8   a  with a different shape is within the scope of the present invention. 
         [0026]    In an embodiment of the airfoil wing system  10  of the present invention, the wing panels are secured together along the entire length of the connection between two adjacent wing panels. The securement of the adjacent wing panels can be accomplished by sewing, welding, adhesive, or other securement means. Between at least one pair of adjacent wing panels, there is an opening  16 . The opening  16  can be any length, but is preferably the entire length of the connection between the adjacent wing panels. As best illustrated in  FIG. 2 , the opening  16  between at least one pair of adjacent wing panels allows air to escape from beneath the airfoil wing  14  for better controlling the flight and take down of the inflatable airfoil. Typically, each opening  16  is formed by the absence of any sewing or other securement means along the connection between the two adjacent wing panels. It should be noted that the number of openings  16  can vary depending on the wind conditions, height of flight, and desires of the user. 
         [0027]    In a preferred embodiment of the airfoil wing system  10  of the present invention, there are six openings  16  formed in the airfoil wing  14 . The first opening  16   i  is formed in the second column  2  between the wing panel  2   b  and the wing panel  2   c.  The second opening  16   ii  is formed in the first row a between the wing panel  2   a  and the wing panel  3   a.  The third opening  16   iii  is formed in the third column  3  between the wing panel  3   a  and the wing panel  3   b.  The fourth opening  16   iv  is formed in the fourth column  4  between the wing panel  4   a  and the wing panel  4   b.  The fifth opening  16   v  is formed in the first row a between the wing panel  6   a  and the wing panel  7   a.  The sixth opening  16   vi  is formed in the seventh column  7  between the wing panel  7   b  and the wing panel  7   c.  It should be noted that the openings  16  described and illustrated herein have been determined by the inventor to provide optimum control of the inflatable airfoil. Once again, however, it is within the scope of the present invention for the airfoil wing  14  to have more than six openings  16  or less than six openings  16  with the openings  16  positioned between other adjacent wing panels. 
         [0028]    The airfoil wing  14  of the airfoil wing system  10  of the present invention has a connecting edge  18  and is secured to the inflatable airfoil  12  along the connecting edge  18 . The connecting edge  18  is formed by the connection of wing panels  1   a,    2   a,    3   a,    4   a,    5   a,    6   a,    7   a,    8   a.  The connecting edge  18  can be secured to the inflatable airfoil  12  using an adhesive material or other means, depending on the desires of the manufacturer or user. In addition, preferably, the connecting edge  18  has reinforcement tape providing additional strength to the connecting edge  18 . Preferably, the tape extends beyond the connecting edge  18 . It should be noted that each of the multiple columns  1 - 8  extend from the connecting edge  18 . 
         [0029]    In addition, the airfoil wing  14  of the airfoil wing system  10  of the present invention has a tailing edge  20  formed by the last wing panels  2   c,    3   c,    4   b,    5   b,    6   c,    7   c  in each of the columns  2 - 7 . Along the tailing edge  20  there are a plurality of harness line securement points  22 . As best illustrated in  FIGS. 4 and 5 , the harness line securement points  22  allow securement of the harness lines  24  for tethering the inflatable airfoil  12 . It should be noted that the securement of harness lines  24  as illustrated are merely one manner and other manners of securement are within the scope of the present invention. 
         [0030]    The airfoil wing  14  of the airfoil wing system  10  of the present invention allows automatic release of air from the airfoil wing  14  to stabilize the inflatable airfoil  12  during flight and assist the user in bringing the inflatable airfoil  12  to the ground. During no wind or light wind conditions, the openings  16  will remain in a closed or substantially closed position. As wind velocities increase, the openings  16  automatically open with the amount of opening depending on the wind velocity. During high wind conditions, the openings  16  will open to their maximum extent. In sum, the airfoil wing system  10  assists the user in maintaining control of the inflatable airfoil  12  during flight and allows the user to bring the inflatable airfoil  12  to the ground in a safe and efficient manner. 
         [0031]    The foregoing exemplary descriptions and the illustrative preferred embodiments of the present invention have been explained in the drawings and described in detail, with varying modifications and alternative embodiments being taught. While the invention has been so shown, described and illustrated, it should be understood by those skilled in the art that equivalent changes in form and detail may be made therein without departing from the true spirit and scope of the invention, and that the scope of the present invention is to be limited only to the claims except as precluded by the prior art. Moreover, the invention as disclosed herein, may be suitably practiced in the absence of the specific elements which are disclosed herein.