A PARASAILING ASSEMBLY AND SYSTEM FOR LAUNCHING THE SAME

- Field of the Invention

This invention is directed to an apparatus associated with parasailing including means to sup¬ port a rider or parasailer in a rider support incor¬ porating a float structure and otherwise designed to _Q allow the rider to be oriented in a substantially seated or partially reclined position when suspended from the ascending parachute. A launching assembly aids in both the launching and retrieval of the rider and parachute from the tow craft. 5

Description of the Prior Art

The sport of parasailing is relatively new but has greatly increased in popularity in approximately the last five years. Accordingly, as pointed out in ₀ my United States Patent 3,987,746 persons indulging in this sport have relatively few equipment innova¬ tions which render the sport more enjoyable and safer.

As a result of the lack of development of the 5 general apparatus associated with the sport, parti¬ cipants frequently have used equipment designed for other generally similar sports such as water skiing, sky diving, hang gliding, etc. wherein such sports are associated with the necessity of launching and _Q retrieving a person.

Perhaps one of the most prevelant problems in the sport of parasailing is the lack of proper safety features. This lack of proper equipment, especially equipment designed for the safety as well as comfort 5 of the rider or parasailer has resulted in a great deal of unwarranted serious injuries and even death to the participant which, admittedly, under certain

circumstances entails a certain amout of risk. Of particular risk to the rider is standard harness used to support the participant from the parachute while parasailing. While these prior art harness struc¬ tures are generally capable of providing adequate support, they have in the past provided serious safety hazards and actually caused death of the participant- Death was the result of the inability of the participant to remove himself from the harness when landing in the water such as during boat failure and relatively moderate to rough sea conditions. In addition to the safety feature of needed equipment in this sport, it is also well recognized that a great deal of time and effort are required in order to ready the person or "rider" as well as his parasailing equipment for launching. Accordingly, there is a well recognized need for an improvement in the equipment associated with the sport of parasail¬ ing both from a safety standpoint, such as the rider support on which the occupant is suspended from the parachute, and also, in the launching equipment utilized for launching and retrieving of the para¬ chute from a launching platform on a marine tow craft.

Summary of the Invention

The present invention is directed towards a parasailing assembly and more particularly, a rider support connected to an ascending parachute speci¬ fically designed and structured to retain and support a rider, substantially in a seated or partially reclined position while being suspended.

In addition, the subject invention is further directed to the system of launching and retrieving of the parachute and attached rider in a safe and effi- cient manner using mechanical apparatus which greatly reduces the preparation time associated with launch¬ ing and/or retrieval.

More particularly, the parasailing apparatus of the present invention comprises a rider support incorporating a float assembly preferably having two float structures disposed in spaced apart parallel relation to one another and extending along the length of the rider support. The disposition and dimension of such float structure are such as to enable the support of at least a large male adult on a the surface of the water over which the tow boat travels. While the sport itself does not contemplate ₀ the rider support or secured rider to land in the water, in certain emergency situations, such a land¬ ing may inadvertently occur. In such an event, the rider would be kept safe and be maintained in a floating posture on the surface of the water, instead ₅ of risking drowning when using prior art harness structures.

The subject rider support further includes a seat structure connected to and/or disposed between the aforementioned float structures wherein the seat o structure is designed and configured to allow the rider or occupant to maintain a seated orientation or at least a partially reclined orientation well within the interior of the rider support, thereby adding to the comfort of the rider during the time of support ₅ and suspension from the air supported parachute.

This of course differs from prior art or conventional apparatus associated with the supporting of the rider in depending fashion from the suspended parachute. Typically, such prior art devices include the con- _Q nection of the harness about the upper torso of the rider thereby causing him to be truly suspended with his feet or lower body portion "dangling" from the ascending parachute. The above prior art device therefore not only adds to the discomfort of the 5 occupant or rider but makes retrieval somewhat dif¬ ficult and in certain situations unsafe.

Another feature of the present invention is the

inclusion of a launching system and associated appara¬ tus to effect and render more efficient and less time consuming the launching procedure as well as the retrieval procedure associated with the parasailing sport. Such launching facility includes the use of a telescopically structured boom extending outwardly along its own central longitudinal axis for the purpose of extending the length outwardly from its foundation or support platform on the tow craft itself. In addition, the boom structure is provided so as to be telescopically retracted wherein both the extension and retraction facilitates extension, inflation and support, retraction, respectively of the parachute during the launching and retrieval steps respectively. The invention accordingly comprises the features of construction, combination of elements, and arrange¬ ment of parts which will be exemplified in the con¬ struction hereinafter set forth, and the scope of the invention will be indicated in the claims.

Brief Description of the Drawings

For a fuller understanding of the nature of the present invention, reference should be had to the following detailed description taken in connection with the accompanying drawings in which:

Figure 1 is a side view in partial cutaway of the marine craft, rider support portion of the para¬ sailing assembly and launching apparatus associated with the system for launching and retrieval of the prasailing apparatus.

Figure 2 is a side view showing the parachute portion of the parasailing assembly in a contained and partially inflated position through activation of the lauching apparatus associated therewith. Figure 3 is a side view of a rider support being occupied by a rider and the parachute in its inflated position.

Figure 4 is a side view showing positioning of the lauching apparatus in a position ready for release of its connection to the parachute portion of the parasailing assembly.

Figure 5 is a side view of the parasailing assembly in a position immediately after launching. Figure 6 is a side view of the marine craft and the connected parasailing assembly, being towed and immediately ready for retrieval.

Figure 7 is a side view of the parasailing ₀ assembly mounted on the launching platform of the tow craft and occupants of the rider support are being changed.

Figure 8 is a side view of the launching appara¬ tus engaging the riser lines of the parachute so as ₅ to maintain its inflation or suspension in the air while the rider support is mounted on the launching pad ^" and the occupant or ride has disembarked there¬ from.

Figure 9 is a side view showing the apparatus in o its retained positioned relative to the parachute for attending to the collapse thereof and storage.

Figure 10 is a side view of the subject tow craft with the launching apparatus in its stored position and the rider support and parachute also _c being stored on the craft.

Figure 11 is a detail view in partial section showing structural details of the launching apparatus and the rider support wherein a rider or occupant is represented in phantom lines. ₀ Figure 12 is an end view along line 12-12 of Figure 11.

Figure 13 is a perspective view of the rider support with certain components of the seat structure represented in phantom lines. Figure 14 is a εectonal view along line 14-14 of Figure 13.

Like reference numerals refer to like parts

throughout the several views of the drawings.

Detailed Description of the Preferred Embodiment

With regard to Figures 1 through 14, the present invention is directed towards a parasailing assembly c of the type mounted from a marine tow craft generally indicated as 10. A launching apparatus generally indicated as 12 is mounted on the boat 10 and is associated with the launching system for both launch¬ ing and retrieval of the parasailing assembly. More

₁₀ specifically, the subject parasailing assembly in¬ cludes a rider support generally indicated as 14 used to maintain a rider or occupant 16 in a seated or at least partially reclined position while suspended from ascending parachute 18. In typical fashion

, ₅ associated with the sport of parasailing, an ascend¬ ing parachute generally indicated as 18 is inflated or suspended by the wind or alternately the rapid forward motion of the tow craft 10 causing the occup¬ ant and the rider support structure 14 to be "lifted"

20 from a launching or support platform 20 of the marine craft as the tow line 22 is played out in accordance with the directional allow 23 (see Fig. 5). Also in accordance with conventional structural apparatus associated with the sport of parasailing, the rider

25 support generally indicated as 14 is removably con¬ nected in depending relation from a plurality of shroud lines 24 which are secured in a depending fashion to the inflated or suspended sheet portion 26 of the ascending parachute. The term "inflated" as

₃₀ used herein relative to the inflation or suspension of the sheet portion 26 of the parachute does not in fact mean that the parachute necessarily contains inflatable portions but rather, that the sheet is expanded and suspended by on-rushing wind.

₃₅ For purposes of clarity, the structural details of the present invention will be described parti¬ cularly with regard to Figures 11 through 14 prior to

the step-by-step operation of lauching and retrieval of the subject parasailing assembly as depicted successively in Figures 1 through 10. With regard to Figures 11 through 14, a rider structure generally indicated as 14 comprises a float assembly including two, spaced apart float structures generally indi¬ cates as 30 and 32 disposed in substantially parallel relation to one another on opposite sides of and extending along the length of the rider support 14. With regard to Figure 14, each of the float struc¬ tures include a pair of float elements 34 extending along the length of and at least partially incasing a rigid, relatively high strength material foundation 36 disposed at least partially on the interior of the float elements 34. Each of the float elements there¬ fore are arranged on and partially define exterior sides of each of the float structures 30 and 32 as shown in Figure 14. The foundation 36 is provided for reinforement and may be made from a metallic or even hight strength plastic material. Connection of the float elements 34 to one another occurs through apertures 37 (see Fig. 11) represented in phantom lines wherein adhesive interconnects the float elem¬ ents 34.

The rider support further includes additional brace means generally indicated as 38 and including two brace members 39 and 40 having opposite ends 39' and 40' secured to a cross brace 42 extending adja¬ cent to the leading portion of the rider support 14 with a similar structure provided at the following end of each brace member 39 an 40. Further, each of the members 39 and 40 extend from their respective opposite ends upwardly in a convergent fashion to a point above a seat structure 44 in which an occupant 16 is positioned. In addition, each of the brace elements 39 and 40 include an adjustment flange 45 having a plurality of apertures 47 secured therein in spaced apart relation to one another and extending

along the length of the respective flanges. The adjustment flanges are provided for adjustable inter¬ connection with a connecting means generally indi¬ cated as 48 wherein oppositely disposed, intercon¬ nected and spaced apart portions 50 is designed to be secured to a plurality of the shroud lines 24. Depend¬ ent upon the wind conditions, including strength, direction, etc., the individual attachments 52 can be secured to different ones of the apertures 47 other than that shown in Figure 11. This varies the pitch or angle of connection of the parachute to the rider support 14 thereby taking into consideration wind conditions.

With regard to the seat structure, at least two seat braces 53 and 55 extend transversely across the width of the rider support 14 and are connected either to the foundation and/or the respective float structures 30 and 32. A sling or cradle type struc¬ ture, which may be made of a flexible yet high strength canvas or like material 52 is strung between the spaced apart and parallel seat braces 53 and 55 and extends "deeply" into the interior of the rider support 14 and between float structures 30 and 32, so as to effectively "cradle" the lower or seat portion of the occupant 16. As emphasized in Figure 11, the "deep seating" or placement of the rider 16 into the interior of the rider support 14 makes it extremely difficult or impossible for the rider to become inadvertently dislodged from the rider support 14 or fall therefrom. However, in the event that the rider support with the rider aboard lands in water, the rider can readily remove himself from the rider support. Alternately, the rider may choose to remain within the rider support 14 since the float struc¬ tures 30 and 32 are specifically structured and dimensioned to maintain the rider free from excessive contact with the water. Cushion members 59 may be disposed in surrounding relation to the respective

seat braces 53 and 55 wherein one cushion member is disposed in underlying and cushioning relation to the leg or knee portion of the occupant 16 wherein the other is disposed in underlying and cushioning and supporting relation to the back portion of the occu- pant 16.

Turning now particularly to Figures 11 and 12, the launching assembly 12 includes a boom having a main portion 60 and telescopically disposed outwadly extendable secondary portions 62, 63, and 64. This boom structure is fixedly secured to a housing and base 65 in which a winch and motor assembly 66 may be mounted for activation of the tow line 22. A pair of feeder pulleys 69 may be provided to regulate outward and inward travel of the tow line 22 as clearly shown. In addition, the outward and inward travel of the respective boom portions is controlled by mechani¬ cal or hydraulic means of conventional design which is not shown for purposes of clarity. The boom structure or launching assembly 12 further includes a cable and pulley arrangement wherein one end of a first cable 70 as at 72 is secured in a substantially fixed position to an upper brace portion of the boom 60 as at 60'. A first, second and third pulley structure include first and third pulleys 72 and 74 movable with respective boom portions 62 and 64 and a second fixedly positioned pulley 73 serving as a guide for the first cable segment 70 and second cable segment 76. For purposes of retention, the first cable member 70 may be made of an extendable or expandable, somewhat elastic material to provide elongation in that the one end 72 is anchored and is ^• not movable per se relative to the outward extension of the remaining boom members 62, 63 and 64. Accord¬ ingly, a constant tension is placed on the second cable seglemtn 76 and, more importantly, a releasable connector 78 is allowed to pass upwardly and out¬ wardly of the boo ^* _n housing 79. Reinforcing structure

80 is structured, dimesioned and configured to perman¬ ently arrange the launching assembly 12 including the boom structure at an angular orientation and there¬ fore in cooperative relation to the launching plat¬ form 20, rider support 14 and parachute structure- Turning to Figures 1 through 10, a step-by-step launching and retrieval procedure would include in Figure 1 the boom assembly 12, being disposed in at least partially outward position wherein the pulley and cable assembly is connectable to a riser line or o lead line of the shroud lines 24 as at 24' . This is accomplished due to the releasable connection facil¬ ity 78 connected to the riser lines 24' on each side of the parachute sheet 26. With regard to Figure 2, a further outward extension of the launching assembly 5 12 or boom structure raises the sheet portion of the parachute 26 to a position where wind or air caused by natural conditions or the forward motion of the boat 10 can serve to fill and expand the parachute 18 as generally represented in Figure 3. At this point, o the occupant 16 is already in the rider support 14 ready for launching.

With reference to Figures 3, 4 and 5, it should be noted that in Figure 3 the launching assembly or boom structure 12 is in its fully outwardly extended 5 position so as to maintain the ascending parachute 18 fully inflated even though the rider support 14 and occupant 16 have not left the launching or support platform 20. However, when ready for launching, the boom assembly is retracted to a certain level such 0 that releasable connector 78 may be manually opened so as to release the riser lines 24 ^! of the shroud lines 24. This in turn totally disengages the para¬ chute from the launching assembly 12 except of course for the existence of the tow line 22. As the tow 5 line 22 is played out (see Fig. 5), the parachute again ascends due to its suspension of the passing air as indicated by directional arrow 81.

Upon retrieving of the rider support 14 and occupant 16, the tow line 22 is retracted as in¬ dicated by directional arrow 83 to a point where the rider support 14 is in a substantially hovering position above the launching platform 20. Further

- pulling in of the tow line 22 causes the rider sup¬ port 14 to land or be positioned immediately above the support platform 20. With reference to Figure 7, the rider support 14 is maintained on the lauching pad 20 so that participants 16 and 16' may change

20 places such as occupant 16 leaving the rider support 14 and participant 16' beginning to enter the rider support 14. It should further be noticed that a plurality of participants in addition to the driver may be carried by the tow craft 10 during the para- 5 sailing operation so as to eliminate the need to return to shore to pick up a new occupant or parti¬ cipant. Accordingly, utilizing the rider support 14 of the present invention, there is little time wasted in changing occupants since there is no need for any o removal or attachment of complicated harness devices secured directly to the body of the participant.

If it is desired to maintain the parachute 18 in its inflated condition as shown in Figure 8, for example when a new rider is to enter the rider sup- 5 port 14, the lauching assembly 12 including the boom is again fully extended so as to maintain the ascend¬ ing parachute 18 so fully extended. However, if it is desired to collapse the parachute 18, the launch¬ ing assembly 12 including the boom components are 0 again retracted to a stored position thereby causing a total collapse of the sheet portion 26 of the parachute 18 for its storage and maintenance in a stored positon as shown in Figure 10. Again, it should be emphasized that the removable coupling 78 5 is manually operated and the boom assembly must accordingly be raised and lowered such that a crew member can effectively attach and/or release the

coupling 78 to the riser lines 24' as set forth above.

Additional structural features include a con¬ nector 88 mounted on a leading portion of rider support 14 adjacent a foot rest 90.

It is therefore to be understood that the follow¬ ing claims are intended to cover all of the generic and specific features of the invention herein descri¬ bed, and all statements of the scope of the invention which as a matter of language might be said to fall therebetween.

Now that the invention has been described,