FLEXIBLE BOW SEAL AIR RIDE BOAT HULL

Abstract: A marine surface vessel with at least one recess (56) that intersects the hull (14) substantially beneath the static waterline thereof, the recess (56) bounded by sidehulls (15, 16), flexible seal member (17) at its forward portion, with bow shaped members at its aft portion (19) and optionally therebetween (18). The flexible seal member (17) is to absorb much of the initial wave impact to improve ride quality. The recess (56) is supplied with pressurized gas to maintain a lift-augmenting gas layer under the hull (14), which is to improve efficiency, speed, load carrying capability and ride quality. Bow shaped members (18, 19) and sidehulls (15, 16) are to provide sure tracking and turning characteristics, proper hull attitude and trim even if the pressurized gas supply is wholly or partially inoperative. In the preferred embodiment, the sidehull keels (22, 23) diverge to allow a smaller seal (17) width forward between the sidehulls (15, 16) to reduce gas leakage forward and provide a smoother ride.

Description: FLEXIBLE BOW SEAL AIR RIDE BOAT HULL Field of the Invention This invention relates to the field of marine surface vessels supported at least in part by gas trapped beneath the hulls, and more particularly to this type of watercraft which retains substantially the above waterline aesthetics of conventional boats except for having a flexible seal in a forward portion thereof. V 2.ET OMPI W 11 I? °J — . — Background of the Invention This invention constitutes a variation upon and re¬ finement of Applicant's earlier invention in the field of this invention, generally entitled "Air Ride Boat Hull". All of these inventions involve the introduction of pres- surized gas in one or more recesses under a boat hull to augment hull lift and thereby improve hull load-carrying capability, efficiency, ride quality and speed. The recess is bounded by one or more flexible seal members at its forward portion, downwardly extending members at its generally bow shaped aft portion and optionally between the forward and aft portions, and by stabilizing, load carrying, catamaran-like side hulls that in the preferred embodiment may have diverging keels. The flexible seal at a forward portion of the vessel in this invention absorbs much of the initial wave impact. The latter feature is intended to contribute substantially to the already exceptional ride qualities of vessels that incorporate Applicant's prior air ride inventions. The combination of these elements is the aforemen- tioned performance advantages over conventional hulls while offering operation, cost, and aesthetic advantages over other pressurized air hull craft. The invention taught herewith handles much like conventional hulls whether the pressurized gas supply is in use or not, costs only slightly more to manufacture and maintain than conventional hulls, and offers generally the same payload space, while maintaining most of the above water aesthetics of conventional hulls. Even though the idea of introducing air or other gases at ambient or higher pressures under boat hulls is not new in basic concept, only a few of the more sophisticated developments have met with any commercial success. However, due to their complex structural requirements and much larger flexible seals than that proposed in the present invention, these inventions generally remain too expensive or imprac- tical for general marine application. The only example of the foregoing that is believed to have any applicability is the Surface Effect Ship (SES) as it is known in the United States. The SES is an outgrowth of the success of the Ground Effect Machine (GEM) as first made workable by Christopher Cockerell over two decades ago in England. The GEM is totally supported by an air cushion and has seals around its full periphery, and as such it is truly amphibious, and has little relationship to this invention. The SES is a marine vehicle with catamaran side hulls connected by a high, wide, cross structure at the top sides and by large flexible seals fore and aft. The SES offers superior ride qualities since the flexible seals yield resiliently to passing waves. However, because of the flex- ibility of the seals, and a generally flat undersurface, the hull cross structure is designed with a high wave clearing undercarriage. As a result, hull stresses can be very high and a highly stressed heavy hull cross structure is neces¬ sary. This is also aggravated by the fact that the SES must be much wider than the conventional hull or the Air Ride hull for stability purposes because of the SES's higher center of gravity (CG) . As a result, even though the SES is very efficient, it compromises much of that advantage to expensive dead structure weight. A one hundred ten foot SES would have an undercarriage clearance of about six to eight feet and requires some forty feet beam for stability. A similar one hundred ten foot vessel made according to the present invention has a chamber depth of only about eighteen inches and a required beam of only some twenty-eight feet. The reason that the present invention requires so much less beam is because its deck load is only five to eight feet ' above the water compared to approximately twelve to fifteen feet for the SES because of the high wave clearing under¬ carriage made necessary by the form of the SES's structure. However, due to its superior ride quality, very high speed capability, and high efficiency, the SES has received at¬ tention for naval and commercial application. The prior art is substantially different from the present invention since they use flap-like or flexible seal members in the aft portion of the vessel, have a deep wave clearing undercarriage which utilizes much valuable hull space, have deep static draft requirements, require very wide beams for stability because of high CG characteristics, have inherently high stress hull structures that are heavy and expensive to manufacture, and cannot readily locate OMPI propellers under the aft flexible seal members due to vertical movement of the seals. Additionally, the flap-like flexible seals are heavy and expensive due to their large size and easy removal of the seals for replacement or ain- tenance by on-board personnel while the SES remains in the water is virtually impossible. As noted above, the present invention is a derivation rom Applican 's other inventive efforts with improved per¬ formance marine surface vessels that are in part supported by a pressurized gas layer structurally trapped and re¬ strained beneath the hull. Prior patent filings of Applicant have centered upon vessels having a more or less convention¬ ally shaped bow of hard structure. Actual test results utilizing forty-two foot and sixty-five foot boats built in this manner show the viability of the forward bow member. These welded aluminum boats have achieved in actual practice substantial efficiency improvements as compared to conven¬ tional hull forms. Based on the test results, it can be said that, in moderate and heavy load carrying applications, conventional hulls will generally require from fifty to one hundred percent more power at planing speeds than a hull with concepts embodied in Applicant's prior inventions in this area. Additionally, the Air Ride invention normally realizes at least a thirty percent speed advantage. These performance advantages are similar to those experienced by the complex and vastly more expensive SES described above. Since the bottom line on any commercial venture is cost, it should be considered that a one hundred ten foot off-shore oil industry crew and supply boat built to a con- ventional design would cost about 1.2 million dollars while a one hundred ten foot SES is in the four million dollar cost range. A one hundred ten foot air ride vessel built according to the present invention would cost thirty percent more than the conventional hull or about 1.6 million dollars. The Air Ride's higher speed and greater payload capability will pay back any of the cost difference between it and the conventional hull normally within the first year of opera¬ tion. The difference between the 4 million dollar cost of a one hundred ten foot SES and the 1.6 million dollar for a one hundred ten foot vessel built according to the present OMP invention is enough to cover fixed operating expenses less depreciation of the present invention for over fifteen years. Summary of the Invention 5 With the foregoing in mind, it is the principal ob¬ ject of the present invention to provide a marine surface vessel with extraordinarily smooth ride qualities and significant load-carrying, efficiency and speed improvements compared to conventional hulls while also maintaining low J_ Q stress and therefore low cost hull structure, shallow draft, flexibility of propulser location, narrower beam, and much more useful hull space when compared to the SES type craft. Another primary object of the invention is to furnish the foregoing objects and advantages while retaining much _5 of the above water aesthetics and handling characteristics of conventional hull forms. One more principal object of the invention is to provide a hull which offers very nearly the same low manu¬ facturing and maintenance cost as conventional hulls while o offering the foregoing advantages. Similarly, a related object of the invention is to offer an inherently strong structure that is more stable when quiescent in comparison to conventional hulls. Another object of the invention is to offer improved 5 efficiency and speed without significantly affecting the dynamic draft or internal hull space of comparably sized con¬ ventional craft. A further object of the invention is to provide means whereby the forward flexible seal member can be easily 0 changed while the vessel is in the water. Another object of the invention is to provide means to pressurize the forward flexible seal member and thereby make it respond faster to wave impact. A related object of the invention is to provide means 5 to regulate the gas pressure supplied to the forward flex¬ ible seal member thereby controlling ride quality. Yet another object of the invention is to provide a hull with diverging catamaran sidehull keels which provides a narrow entry forward with a less wide flexible seal member 0 with resultant better ride qualities and less gas leakage - θR OM forward. _ 6 _ A further object of this invention is to provide an improved hull embodying the foregoing advantages which is not prone to fouling by debris or to damage thereby. One more object of the invention is to offer the pre¬ ceding objects and advantages with changes that do not significantly affect draft of the hull when quiescent, and which will not cripple or seriously hamper use of the vessel if the pressurizing means of the invention are not in use or temporarily rendered inoperative. Other objects and advantages of the present invention will become apparent from the following descriptions and claims and from the accompanying drawings. In accordance with the present invention there is disclosed an improved performance marine surface vessel with at least one recess that intersects the hull substantially beneath the static waterline thereof, the recess bounded by stabilizing, load-carrying, catamaran-like side hulls, flexible seal member at its forward, portion, with downwardly extending generally bow shaped members located at its aft portions and optionally there-between, with the recess being supplied with pressurized gas to maintain a lift-augmenting, restrained pressurized gas layer under the hull that im¬ proves load carrying capability, efficiency and ride quality. The flexible seal member at the front of the vessel absorbs much of the initial wave impact thereby contributing sub¬ stantially to the exceptional ride quality which, along with efficiency and speed, is a major object of the invention. The aft bow members, and optional intermediate bow sections in some cases, may ride in the water like small bow sections thereby improving hull ride and handling characteristics and reducing gas leakage. The bow shaped members along with the catamaran-like side hulls provide gas restraining means, sure tracking and turning characteristics when underway in any type of sea, and proper hull attitude and trim without wallowing at low speeds or yaw, roll or pitch instabilities at high speeds even if the pressurized gas supply is wholly or partially inoperative. The bow shaped members not only act as gas flow re- strictors, but also add substantially to hull structural OMP integrity and seaworthiness. In the design of the more de¬ sirable longer finer hull shapes it is advantageous to locat several bow shaped members athwartships of and interspaced down the length of the recess that impacts with the ir- regular water surface during rough sea operation. This maintains a series of gas chambers down the length of the hull, that may be interconnected and/or individually pressurized, and minimizes water impact with the underside of the rather shallow recess itself. The bow shaped members are downwardly extending and may have any shape such as inverted-V, V, rounded, W, flat or the like, with the inverted-V being a preferred embodiment because of its simplicity of construction, inherently strong structural characteristics, and good ride qualities. The forward flexible seal would normally be fabricated from vinyl coated flexible materials although other seal materials and designs are considered within the scope of the invention. Seal designs can include rigid material por¬ tions joined by flexible materials, combined or overlapping rigid material sections that result in an overall flexing effect, and the like. In its preferred embodiment pres¬ surized gas is impacted onto the back side of the seal to help seal shape recovery while traversing rough seas. This seal is intended to be easily removable for replacement or repair by removing a series of bolts, plates or the like that can be reached by on-board personnel while the boat remains in the water. The use of divergihg keels on the catamaran sidehuils has proven to be very effective and valuable on Air Ride test craft and is the preferred embodiment for this flexible bow seal Air Ride inventive hull also. As an example, on the 42 foot Air Ride test craft the catamaran sidehull keels are some six feet apart at the forward end of the recess and twelve feet apart aft. This means less gas flow leakage forward and narrower or finer entry forward which contribute to the exceptional ride qualities of these craft. The amount of sidehull keel divergence need not be large to pro¬ vide noticeable improvements and twenty percent is considered sufficient while fifty percent divergence offers truly superior performance. f OMPI The catamaran sidehuils employ non-trip chines in their preferred embodiment that aid stability in turns. The 42 foot Air Ride test craft can negotiate a full 180° turn in less than a 200 foot radius while traveling at an estimated 25 ph. Banking characteristics in a turn are similar to a conventional semi-V hull with the outboard chine higher than the inboard chine. The use of non-trip chines on the cata¬ maran sidehuils contributed to these good handling character¬ istics. In the case of the sidehuils, aft seals, and any addi¬ tional bow members disposed proximal the recess it is gener¬ ally considered, for the present invention, that 50 degrees is an upper limit for good planing efficiencies and that 5 degrees is a lower limit that still has reasonable rough water ride qualities. With reference to Page 117, Figure 91 of High Speed Small Craft, Third Edition by Peter DuCane, Temple Press Books Limited, London, 1964, this can be illus¬ trated. That figure titled "Boundary of planing of flat- bottomed planing surfaces" shows that a deadrise angle of 50 degrees has planing efficiencies of 45 percent while, for example, 70 degrees has only 20 percent. Planing efficien¬ cies, as presented in the reference by DuCane, are over 90 percent for the 5 degree surface. Therefore, the range of angles, 5 to 50 degrees, results in good planing lift effi- ciencies, reasonably good to excellent ride qualities, and generally at least partial water contact to reduce gas flow leakage (Note that deadrise angle is the angle that a bottom surface of the hull, as measured in a vertical transverse plane of the hull, forms with a line perpendicular to the vertical centerline plane of the hull) . It is interesting to note that the wide essentially horizontal lower surfaces of the aft seals of SES's and other prior art normally ride above the water surface by some distance, some one and one half feet or so is the design goal for a future 3000 ton Navy SES, which at least partially accounts for the high air flow rate requiransnt of these craf and other partially air supported craft that utilize basically horizontal aft seal surfaces. The angled portions of the aft bow member of the present invention need not span the full width of the bow member as the critical impact areas are normally at or near the water contacting portions. Therefore, with the 5-50 degree angled surface limitation, it can be stated that an aft bow member that is angled over at least 25 percent of the recess width would be acceptable (Note that "average recess width" as herein defined is the width between recess boundary waterlines on boat structure averaged over recess length. If there are any breaks in the recess boundary waterline, such as might be caused by a hole or vent in a sidehull or bow member at the waterline, the waterline is considered to be on a straight line between the waterlines on boat structure either side of said break in the recess boundary waterline) . Since the aft or any additional bow members can be composed of one or more bow members that can be staggered slightly fore and aft, as well as side to side, it is necessary to define a means of measuring the bow mem¬ ber surface angles. These angles are measured in one or more vertical transverse planes of the hull that intersect the bow members and do not overlap each other across any longitudinal vertical plane parallel to the vertical center- line plane of the hull. Therefore, these vertical trans¬ verse planes may be staggered, but their total width shall not exceed the maximum outside width of the bow members. The invention will be better understood upon refer- ence to the drawings and detailed description of the invention which follow in which: Brief Description of the Drawings Figure 1 is a side elevation of a boat hull built according to the present invention showing the catamaran keel, outer chine, and non-trip chine. Figure 2 is a bottom view of a boat hull built with the invention and showing the recess, the catamaran-like load carrying side hulls, diverging side .hull keels, aft and in- termediate inverted-V bow members, flexible seal in the bow, inlet ports, and dynamic calm sea waterline. Figure 3 is a centerline cross section of the hull of Figure 2 showing a gas pressurizing means in relation to the recess, flexible forward seal and flexible seal pressuriza- tion means, aft and intermediate inverted-V bow members, and flexible seal removing means. Figure 4 is a partial cross section taken along the line 4-4 of Figure 2 showing the catamaran keel and outer chine. Figure 5 is a partial cross section taken along the line 5-5 of Figure 2 showing the catamaran keel, non-trip, and outer chine. Figure 6 is a partial cross section taken along the line 6-6 of Figure 2. Figure 7 is a partial front and/or bow elevation of the starboard side of the invention showing the flexible seal and flexible seal removable means, catamaran side hull, outer and non-trip chine. Figure 3 is a partial rear or stern elevation of the starboard side of the invention. Figure 9 is a partial bottom view of several alter¬ native embodiments of the hull of Figure 2 including V-shaped bow members, one with gas passageway and stepped diverging catamaran side hull keels. Figure 10 is a partial cross section taken along the line 10-10 of Figure 9. Figure 11 is a partial cross section taken along the line 11-11 of Figure 9 showing the catamaran side hull keel and V-shaped bow member with integral gas passageway. Figure 12 is a partial cross section taken along the line 12-12 of Figure 9. Detailed Description With reference to each of the aforementioned Figures in turn, and using like numerals to designate similar parts throughout the several views, a preferred embodiment and several alternative embodiments will now be described. Figure 1 discloses a motorboat with the inventive hull 14 in profile view of the port side which illustrates the resemblance to standard hull forms. Some elements of the port load carrying catamaran sidehull 15 includes the port catamaran keel 22, port inner chine 26, port non-trip chine 27, and port outer chine 25. The port hull sheer line 29, transom 28, and dynamic waterline 13 are also shown. Figure 2 discloses a bottom view of the inventive CMP hull 14. The preferred embodiment of a flexible bow seal 17 includes an easily removable attaching arrangement in¬ cluding such items as attaching bolts 41 and plate 42 or other suitable attachment means that can be removed while the boat is waterborne by qn-board personnel. Port 15 and Starboard 16 load-carrying catamaran sidehuils, aft bow shaped member 19, and optional typical secondary bow member 18 define the recess 56. It will be seen from the drawing that the load-carrying catamaran sidehuils begin near or proximal to the bow or forward portion of the hull. Any number of additional bow members such as 18 may be utilized if desired and, further, shapes other than the inverted-V shown are acceptable. -It is also considered within the scope of the present invention to have downwardly extending planing steps (not shown) located on the recess side of sidehuils to add to stability. This could be accomplished by removing a center section of an additional bow member 18 for example. The recess 56 gas supply ports 20 and 21 are shown in a typical arrangement although from one to many ports can be utilized and can be located anywhere in the recess 56. The propulsor underwater gear include drive shafts and sup¬ ports 32 and 35 that project through the gas recess 56. In this version, subcavitating propellers 31 and 34, and rudders 30 and 33 are shown in typical arrangement, although the Air Ride invention can utilize other propeller types, water- jets and the like if desired and location can be any other suitable location such as under the catamaran sidehuils, aft of the transom, or even on deck in the case of air pro- pulsors. Other items in Figure 2 include hull intersect lines 37 and 38, sheer lines 29 and 46, outer chines 25 and 45, inner chines 26 and 43, and non-trip chines 27 and 44. Chines such as the aforementioned are not essential to func- tion of the Air Ride invention and other designs such as rounded bilges are feasible. However, hard chine designs coupled with one or more non-trip chines is the preferred embodiment for most applications. Note that the catamaran sidehull keels 22 and 23 diverge for at least a portion of the length of the recess 56 in the preferred embodiment of this invention in order to provide a relatively narrow entry forward with resulting good ride qualities, reduced air leakage forward and reduced wetted area aft. These cata¬ maran keels can be parallel for either their whole or partial length if desired, and, further, in order to aid sealing at the rear of the recess, can be made to converge aft. Nevertheless, the preferred embodiment is certainly the diverging catamaran sidehull keels as shown. Figure 3 discloses a longitudinal cross section along a hull vertical centerline plane 3-3 of Figure 2. When any gas, such as air, is supplied to the recess 56 through supply ducts or ports such as 20 from any gas supply source or sources at ambient or higher pressures such as from a powered blower 48 in fluid communication therewith, per- formance improvement results. When at higher than ambient pressures, a hull lift-augmenting force is realized that improves hull lifting capabilities, ride quality, and ef¬ ficiency. The gas flow arrows 36 show the general direction of gas flow in the recess 56 during dynamic calm sea opera- tion. The forward flexible seal 17 can be supplied with pressurized gas from a source such as the powered blower 48 through gas ducts 49 with pressure regulated by an optional gas regulating valve 50. This allows variations in firmness of the flexible seal 17 with resultant control of ride quality and flexible seal 17 gas leakage in a seaway. Those features coupled with the preferred embodiment inverted-V downwardly extending bow shaped members 18, 19, result in a cushioned effect to produce an extremely soft ride. Figure 3 also shows a typical prime mover engine 47. The blower 48 can be powered by its own engine, not shown, or belt, hydraulic, or other drive means off of other engines such as the prime mover engine 47. Drive shaft 35 sub- cavitating propeller 34 and rudder 33 can also be seen. Flexible seal 17 intersects the dynamic calm water line 13 in this instance and is attached to the hull using bolt 41 and plate 42. Load-carrying catamaran sidehull 16 is shown extending downwardly from hull 14, which can also be seen clearly in cross-sectional view Figure 4 in referring to the keel 23 of the sidehull 16. Turning now to Figure 4, there is disclosed a partial cross-section taken along the line 4-4 of Figure 2 dis¬ closing sheer line 46, outer chine 45, catamaran sidehull keel 23, and hull line intersect 38. The flexible seal area parallel to each other sidehull inside surfaces are illus¬ trated by a line from 23 to 38. Figure 5 is also a partial cross-section taken along the line 5-5 of Figure 2 and illustrates sheer line 46, outer chine 45, non-trip chine 44, inner chine 43, catamaran sidehull keel 23, and hull intersect line 38. The inside surfaces of sidehuils, as illustrated by a line 23 to 38, are at least in part comprised of angles, when measured in at least one hull vertical transverse plane proximal the re¬ cess, that are between twenty-five and eighty degrees with a line perpendicular to the vertical centerline plane of the hull. Figure 6 is a similar partial cross-section taken at the stern of the boat along the line 6-6 of Figure 2. It also illustrates the location at that point of sheer line 46, outer chine 45, and the trailing edge of catamaran sidehull keel 23. Figure 7 is a partial front elevation, showing the flexible bow seal member 17, attached to inventive hull 14 by bolt 41 and plate 42. It is generally advisable to have the inside surface of the sidehuils adjacent to the flexible seal 17 parallel to each other to prevent interference with seal movement. The outer chine 45 is shown in relation to starboard load-carrying catamaran sidehull 16, non-trip chine 44, and inner chine 43. Also shown is catamaran sidehull keel 23, dynamic water line 13 and sheer line 46. Beneath flexible seal 17 appears aft bow-shaped member 19, drive shaft 35, subcavitating propeller 34, and rudder 33. In Figure 8 a partial rear elevation is shown of the starboard side of the craft showing transom 28, dynamic water line 13, catamaran sidehull keel 23, and the conven¬ tional elements of drive shaft 35, propeller 34, and rudder 33. Figure 9 is a partial bottom view showing several alternative embodiments which may be considered as separate alternatives. Shown is an abbreviated form of aft bow member 19 in proximity to drive shaft 32 and 35, propellers 31 and 34, and rudders 30 and 33 mounted on transom 28. Re¬ cess 56 is defined by aft bow member 19, load-carrying catamaran sidehuils 15 and 16 and forward portions which are not shown in Figure 9. One of the alternative embodiments shown in Figure 9 is a secondary bow member 18 containing a further optional feature, air passageway 57. The floor of the recess 55 surrounds bow member 18, and bow member 18 and aft bow member 19 are shown intersecting the dynamic water line 24. In a manner similar to those disclosed in Figure 2, air inlets are shown forward of the aft bow member 20 and 21, and are duplicated forward of the second¬ ary bow member 18 with inlets 51 and 52. The catamaran sidehuils 15 and 16 may alternatively diverge from the vertical center line plane of the inventive hull for at least a portion of their length. A further alternative__ embodiment shown in Figure 9 is at least one step in the di¬ verging sidehuils as shown at 22. As a result, bow hull intersect lines 37 and 38 are also stepped in the alterna- tive embodiment shown in Figure 10. Of course, sheer lines 29 and 46 and chines 25 and 46 are also shown as in earlier views. Turning now to Figure 10, which is a partial cross- section taken along the line 10-10 of Figure 9, the sheer line 29, chine 25, catamaran sidehull keep 22, hull inter¬ sect line 37 and the floor 55 of recess 56 is shown therein. In Figure 11, which is partial cross-section taken along the line 11-11 of Figure 10, there is again disclosed sheer line 29, chine 25, catamaran sidehull keel 22, hull intersect line 37, the floor 55 of recess 56, the slope of secondary bow 18, and air passageway 57. Finally, turning to Figure 12, which is partial cross-section taken at the very rear of the craft along the line 12-12 of Figure 9, there is disclosed hull sheer line 29, chine 25, catamaran sidehull keel 22, hull intersect line 37, and aft bow section 19. While the invention has been described in connection with a preferred and several alternative embodiments, it will be understood that there is no intention to thereby limit the invention. On the contrary, there is intended to be covered all alternatives, modifications and equivalents as may be included within the spirit and scope of the in¬ vention as defined by the appended claims, which are the sole definition of the invention.

Claims: Claims - 16 - 1. In an improved boat hull that is partially supported by a pressurized gas lifting surface including a recess in an underside of the hull, which recess is sup¬ plied with pressurized gas from at least one powered gas supply source through at least one gas inlet connected to said recess, and having a gas sealing forward flexible member which is supplied with gas from at least one gas in¬ let, the improvement comprising: stabilizing, load-carrying catamaran-like side- hulls beginning at a forward portion of and extending down¬ ward from the hull and having keels extending substantially parallel to each other rearwardly from said forward portion of said hull to a point at which they begin to diverge, said gas sealing forward flexible member extending between and substantially to said point of divergence of said substan¬ tially parallel portions of said side hull keels; and at least one fixed substantially rigid aft gas sealing bow member extending over a major portion of recess width, said bow member including at least one surface in part curvilinear and at least partially comprising at least one inverted-V structure. 2. The hull of claim 1 wherein the catamaran side hull keels diverge by at least one hundred percent (100%) of the distance between them at their forward portions. 3. The hull of claim 1 which further comprises at least one additional bow member proximal to the recess. 4. The hull of claim 2 which further comprises at least one additional bow member proximal to the recess. 5. The hull of claim 3 which further comprises in¬ dividual fluid communication of gas pressurizing means with individual portions of the recess. 6. The hull of claim 3 which further comprises at least one gas passageway in an underside of at least one of the additional bow members thereby allowing gas to flow _ _ between portions of the recess. 7. The hull of claim 1 wherein catamaran sidehull keel divergence is accomplished by at least one outward step in said side hull keel. 8. The hull of claim 1 wherein the gas sealing for¬ ward flexible member is pressurized from a pressurized gas source through a pressure regulating device. 9. The hull of claim 1 which further comprises at least one gas sealing forward flexible member that can be detached while the hull is waterborne. 10. The hull of claim 1 wherein the side hulls have non-trip chines. 11. In an improved boat hull that is partially sup¬ ported by a pressurized gas lifting surface including a recess in an underside of the hull, which recess is supplied with pressurized gas from at least one powered gas supply source through at least one gas inlet connected to said recess, and having a gas sealing forward flexible member which is supplied with gas from at least one gas inlet, the improvement comprising: stabilizing, load-carrying, catamaran-like side- hulls beginning at a forward portion of and extending downward from the hull and having keels extending substan¬ tially parallel to each other rearwardly from said forward portion of said hull to a point at which they begin to di¬ verge, said gas sealing forward flexible member extending between and substantially to said point of divergence of said substantially parallel portions of said side hull keels; and At least one fixed substantially rigid aft gas sealing bow member extending over a major portion of recess width, said bow member including at least one surface in part curvilinear and at least partially comprising at least one V structure. 12. The hull of claim 11 wherein the catamaran side hull keels diverge by at least one hundred percent (100%) of the distance between them at their forward portions. 13. The hull of claim 11 which further comprises at least one additional bow member proximal to the recess. 14. The hull of claim 12 which further comprises at least one additional bow member proximal to the recess. 15. The hull of claim 13 which further comrpises in¬ dividual fluid communication of gas pressurizing means with individual portions of the recess. 16. The hull of claim 13 which further comprises at least one gas passageway in an underside of at least one of the additional bow members thereby allowing gas to flow between portions of the recess. 17. The hull of claim 11 wherein catamaran sidehull keel divergence is accomplished by at least one outward step in said side hull keel.- 18. The hull of claim 11 wherein the gas sealing forward flexible member is pressurized from a pressurized gas source through a pressure regulating device. 19. The hull of claim 11 which further comprises at least one gas sealing forward flexible member that can be detached while the hull is waterborne. 20. The hull of claim 11 wherein the side hulls have non-trip chines. 21. In an improved boat hull containing a vertical centerline plane and that is partially supported by a pres¬ surized gas lifting surface including a recess in an under¬ side of the hull, and having a gas sealing forward flexible member, which recess is supplied with pressurized gas from at least one powered gas supply source through at least one gas inlet in fluid communication with said recess , the im¬ provement comprising: stabilizing, load-carrying catamaran-like side- hulls beginning at a forward portion of and extending downward from the hull and having keels that diverge to enlarge recess width by at least twenty percent (20%) aft of their water contacting portions that are proximal a lowermost portion of said forward flexible seal member, said sidehuils having inside surfaces that are substantially pa- -.*• rallel to each other proximal at least a portion of said for¬ ward flexible seal member, a sum of substantially rigid water contacting elements of said sidehuils on each side of said recess extending substantially from said forward flexible seal member to at least one aft substantially rigid gas sealing bow member, with total width of said aft bow members comprising a major portion of recess width proximal said aft bow members, said aft bow members at least partially com¬ prising angled surfaces that in total, when measured in at least one hull vertical transverse plane where said trans¬ verse planes in total substantially equal a maximum outside width of said aft bow members, comprise at least twenty-five percent (257o) of recess width proximal said aft bow members and said angles of said surfaces, when measured in hull ver¬ tical transverse planes, being between five (5) and fift (50) degrees with a line perpendicular to the vertical center- line plane of the hull. 22. The hull of claim 21 wherein said aft bow member at least partially includes angled surfaces, as seen in a vertical transverse plane of the hull, that comprise a major portion of the width of said aft bow member. 23. The hull of claim 21 wherein surfaces of the aft bow member are at least in part curvilinear. 24o The hull of claim 21 wherein the aft bow member includes at least one substantially inverted-V shaped structure. SUBSTIT ' ° M?I 25. The hull of claim 21 wherein the aft bow member includes at least one substantially V-shaped structure. 26. The hull of claim 21 which further comprises at least one additional substantially rigid bow member disposed both proximal the recess and forward of the aft bow member. 27. The hull of claim 26 wherein said additional bow member at least partially includes angled surfaces that in total, when measured in at least one hull vertical trans¬ verse plane where said transverse planes in total substan- tially equal a maximum outside width of said additional bow member, comprise at least twenty-five percent (25%) of additional bow member width and said angles of said surfaces, when measured in hull vertical transverse planes, being be¬ tween five (5) and fifty (50) degrees with a line perpend- icular to the vertical centerline plane of the hull. 28. The hull of claim 27 wherein said additional bow members angled surfaces comprise a majority of the width of said additional bow members. 29. The hull of claim 26 wherein surfaces of the ad¬ ditional bow member are at least in part curvilinear. 30. The hull of claim 26 wherein the additional bow member includes at least one inverted-V shaped structure. 31. The hull of claim 26 wherein the additional bow member includes at least one V-shaped structure. 32. The hull of claim 26 which further comprises in¬ dividual fluid communication of gas pressurizing means with individual portions of the recess. . 33. The hull of claim 21 wherein said sidehull keels diverge by at least fifty percent (50%) of the distance be¬ tween them at their forwardmost watercontacting portions. 34. The hull of claim 21 wherein said sidehull keels are substantially parallel proximal their forwardmost watercontacting portions. 35. The hull of claim 21 wherein at least one down¬ wardly extending planing step i s disposed proximal the recess side of a sidehull, said steps further extending over only a portion of recess width proximal said steps. 36. The hull of claim 21 wherein the sidehuils have non-trip chines. 37. The hull of claim 21 wherein said sidehuils further at least in part comprise watercontacting planing surfaces whose average angle, when measured in a hull vert¬ ical transverse plane proximal the recess, is between five (5) and fifty (50) degrees with a line perpendicular to the vertical centerline plane of the hull. 38. The hull of claim 21 that has gas sealing struc¬ ture rearward of said aft bow member. 39. The hull of claim 21 wherein the gas sealing for¬ ward flexible member is pressurized from a pressurized gas source through a pressure regulating device. 40. The hull of claim 21 wherein the gas sealing for¬ ward flexible member is held in sealing position on its lower portions by pressurized gas supplied from a powered gas source. 41. The hull of claim 21 which further comprises at least one gas sealing forward flexible member that can be changed by on-board personnel while the hull is waterborne. 42. The hull of claim 21 wherein catamaran sidehull keels diverge in a discontinuous manner to expand a width of the pressurized recess. OMPI 43. In an improved boat hull containing a vertical centerline plane and that is partially supported by a pres¬ surized gas lifting surface including a recess in an under¬ side of the hull, and having a gas sealing forward flexible member, which recess is supplied with pressurized gas from at least one powered gas supply source through at least one gas inlet in fluid communication with said recess, the im¬ provement comprising: stabilizing, load-carrying catamaran-like side- hulls beginning at a forward portion of and extending downward from the hull and having keels that diverge to enlarge recess width by at least twenty percent (20%) aft of their watercontacting portions that are proximal a lower¬ most portion of said forward flexible seal member, at least one aft substantially rigid gas sealing bow member, with total width of said aft bow members comprising a major por¬ tion of recess width proximal said aft bow members, said aft bow members at least partially comprising angled surfaces that in total, when measured in at least one hull vertical transverse plane where said transverse planes in total substantially equal a maximum outside width of said aft bow members, comprises at least twenty-five percent (25%) of recess width proximal said aft bow members and said angles of said surfaces, when measured in hull vertical transverse planes, being between five (5) and fifty (50) degrees with a line perpendicular to the vertical centerline plane of the hull, and at least one additional substantially rigid bow member disposed both forward of the aft bow member and substantially between the sidehuils. 44. The hull of claim 43 wherein said aft bow member at least partially includes angled surfaces, as seen in a vertical transverse plane of the hull, that comprises a major portion of the width of said aft bow member. ' 45. The hull of claim 43 wherein surfaces of the aft bow member are at least in part curvilinear. 46. The hull of claim 43 wherein the aft bow member includes at least one substantially inverted-V shaped structure. _ 23 - 47. The hull of claim 43 wherein the aft bow member includes at least one substantially V-shaped structure. 48. The hull of claim 43 wherein said additional bow member at least partially includes angled surfaces that in total, when measured in at least one hull vertical trans¬ verse plane where said transverse planes in total substan- tially equal a maximum outside width of said additional bow member, comprise at least twenty-five percent (25%) of additional bow member width and said angles of said surfaces, when measured in hull vertical transverse planes, being be¬ tween five (5) and (50) degrees with a line perpendicular to the vertical centerline plane of the hull. 49. The hull of claim 48 wherein said additional bow members angled surfaces comprise a majority of the width of said additional bow members. 50. The hull of claim 43 wherein surfaces of the ad¬ ditional bow member are at least in part curvilinear. 51. The hull of claim 43 wherein the additional bow member includes at least one inverted V-shaped structure. 52. The hull of claim 43 wherein the additional bow member includes at least one V-shaped structure. 53. The hull of claim 43 which further comprises in¬ dividual fluid communication of gas pressurizing means with individual portions of the recess. 54. The hull of claim 43 wherein said sidehull keels diverge by at least fifty percent (50%) of the distance be¬ tween them at their forwardmost watercontacting portions. 55. The hull of claim 43 wherein said sidehull keels are substantially parallel proximal their forwardmost water¬ contacting portions. OMPI O 56. The hull of claim 43 wherein at least one down¬ wardly extending planing step is disposed proximal the recess side of a sidehull, said steps further extending over only a portion of recess width proximal said steps. 57. The hull of claim 43 wherein the sidehuils have non-trip chines. 58. The hull of claim 43 wherein said sidehuils further at least in part comprise watercontacting planing surfaces whose average angle, when measured in a hull vertical transverse plane proximal the recess, is between five (5) and fifty (50) degrees with a line perpendicular to the vertical centerline plane of the hull. 59. The hull of claim 43 that has gas sealing struc¬ ture rearward of said aft bow member. 60. The hull of claim 43 wherein the gas sealing forward flexible member is pressurized from a pressurized gas source through a pressure regulating device. 61. The hull of claim 43 wherein the gas sealing forward flexible member is held in sealing position on its lower portions by pressurized gas supplied from a powered gas source. 62. The hull of claim 43 which further comprises at least one gas sealing forward flexible member that can be changed by on-board personnel while the hull is waterborne. 63. The hull of claim 43 wherein catamaran sidehull keels diverge in a discontinuous manner to expand a width of the pressurized recess. 64. In an improved boat hull containing a vertical centerline plane and that is partially supported by a pres¬ surized gas lifting surface including a recess in an under¬ side of the hull, and having a gas sealing forward flexible member, which recess is supplied with pressurized gas from at least one powered gas- 2s5up-ply source through at least one gas inlet in fluid communication with said recess, the im¬ provement comprising: stabilizing, load-carrying catamaran-like side- hulls beginning at a forward portion of and extending downward from the hull and having keels that diverge to enlarge recess width by at least twenty percent (20%) aft of their watercontacting portions that are proximal a lowermost portion of said forward flexible seal member, at least one aft substantially rigid gas sealing bow member, with total width of said aft bow members comprising a major portion of recess width proximal said aft bow members, said aft bow members at least partially comprising angled sur¬ faces that in total, when measured in at least one hull vertical transverse plane where said transverse planes in total substantially equal a maximum outside width of said aft bow members, comprises at least twenty-five percent (25%) of recess width proximal said aft bow members and said angles of said surfaces, when measured in hull vertical transverse planes, being between five (5) and fift (50) degrees with a line perpendicular to the vertical centerline plane of the hull, and at least one downwardly extending planing step disposed proximal the recess side of a sidehull, said steps further extending over only a portion of recess width prox- imal said steps. 65. The hull of claim 64 wherein said aft bow member at least partially includes angled surfaces, as seen in a vertical transverse plane of the hull, that comprise a major portion of the width of said aft bow member. 66. The hull of claim 64 wherein surfaces of the aft bow member are at least in part curvilinear. 67. The hull of claim 64 wherein the aft bow member includes at least one substantially inverted V-shaped structure. 68. The hull of claim 64 wherein the aft bow member includes at least one substantially V-shaped structure. 69. The hull of claim 64 which further comprises at least one additional substantially rigid bow member disposed both proximal the recess and forward of the aft bow member. 70. The hull of claim 69 wherein said additional bow member at least partially includes angled surfaces that in total, when measured in at least one hull vertical transverse plane where said transverse planes in total substantially equal a maximum outside width of said additional bow member, comprise at least twenty-five percent (25%) of additional bow member width and said angles of said surfaces, when measured in hull vertical transverse planes, being between five (5) and fifty (50) degrees with a line perpendicular to the vertical centerline plane of the hull. 71. The hull of claim 70 wherein said additional bow members angled surfaces comprise a majority of the width of said additional bow members. 72. The hull of claim 69 wherein surfaces of the ad¬ ditional bow member are at least in part curvilinear. 73. The hull of claim 69 wherein the additional bow member includes at least one inverted V-shaped structure. 74. The hull of claim 69 wherein the additional bow member includes at least one V-shaped structure. 75. The hull of claim 69 which further comprises in¬ dividual fluid communication of gas pressurizing means with individual portions of the recess. 76. The hull of claim 64 wherein said sidehull keels diverge by at least fifty percent (50%) of the distance be¬ tween them at their forwardmost watercontacting portions. 77. The hull of claim 64 wherein said sidehull keels are substantially parallel proximal their forwardmost water¬ contacting portions. 78. The hull of claim 64 wherein the sidehuils have non-trip chines. 79. The hull of claim 64 wherein said sidehuils fur¬ ther at least in part comprise watercontacting planing sur¬ faces whose average angle, when measured in a hull vertical transverse plane proximal the recess, is between five (5) and. fifty (50) degrees with a line perpendicular to the vertical centerline plane of the hull. 80. The hull of claim 64 that has gas sealing struc¬ ture rearward of said aft bow member. 81. The hull of claim 64 wherein the gas sealing for¬ ward flexible member is pressurized from a pressurized gas source through a pressure regulating device. 82. The hull of claim 64 wherein the gas sealing for¬ ward flexible member is held in sealing position on its power portions by pressurized gas supplied from a powered gas source. 83. The hull of claim 64 which further comprises at least one gas sealing forward flexible member that can be changed by on-board personnel while the hull is waterborne. 84. The hull of claim 64 wherein catamaran sidehull keels diverge in a discontinuous manner to expand a width of the pressurized recess.

Inventors: BURG DONALD EARL, BURG, DONALD, EARL
Applicants: BURG DONALD EARL, BURG, DONALD, EARL
Application year: 1983
Main classification: B63B1
IPC codes: B63B1