US3187708A - Propulsion device - Google Patents

Propulsion device Download PDF

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US3187708A
US3187708A US115463A US11546361A US3187708A US 3187708 A US3187708 A US 3187708A US 115463 A US115463 A US 115463A US 11546361 A US11546361 A US 11546361A US 3187708 A US3187708 A US 3187708A
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water
housing
discharge nozzle
impeller
discharge
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US115463A
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Fox Anthony
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PROPULSION RES Inc
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PROPULSION RES Inc
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H11/00Marine propulsion by water jets
    • B63H11/02Marine propulsion by water jets the propulsive medium being ambient water
    • B63H11/10Marine propulsion by water jets the propulsive medium being ambient water having means for deflecting jet or influencing cross-section thereof
    • B63H11/107Direction control of propulsive fluid
    • B63H11/117Pivoted vane

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  • This invention is a propulsion unit for boats that supplants the gear box, propeller and rudder structure of a usual power boat arrangement.
  • the forward and reverse mechanism consists of a balanced deflector damper within the discharge nozzle which permits deflecting the water jet through forward or reverse ports.
  • Water jet propulsion units for boats are not novel in themselves, but many of the units that have been presented to the purchasing public are at least somewhat unsatisfactory in one or more of the following respects. They are frequently excessively long, heavy and expensive. They are often incapable of operating in a trouble free manner under conditions in which silt, sand and other smalll particles of hard materials are suspended in the water in which the craft is operating. The construction of some is such that they are ditlicult or impossible to steer when reversed. Most of these units heretofore offered occupy as much or more space inside the boat as a comparable propeller driving power plant would. Most also require cutting holes in the bottom of the hull, thus weakening the same, and increasing the likelihood of failure as the result of high speed engine operation and the interaction of the hull with water, especially rough water.
  • Yet another object of this invention is to provide a jet propulsion unit for watercraft that can be mounted in close-coupled arrangement with an engine on opposite sides of the boat transom.
  • a further object of this invention is to provide a jet propulsion unit for boats that is substantially trouble free regardless of the conditions under which it is operated.
  • a still further object of this invention is to provide a jet propulsion unit for boats of simplified construction.
  • Yet another object of this invention is to provide a jet propulsion unit for boats having relatively high water capacity but small outside dimensions.
  • a still further object of this invention is to provide a jet propulsion and engine unit for a boat in which the mounting flanges of the propulsion unit and the engine cooperate to align the drive shaft of the engine with the impeller shaft of the propulsion unit.
  • Still another object of this invention is to provide a jet propulsion unit having a discharge nozzle which minimizes friction between water being discharged and the sides of the discharge nozzle.
  • Yet another object of this invention is to provide a mounting structure for both theY engine and the propulsion unit whereby they are entirely supported by a single element of the boat hull.
  • FIGURE 1 is a longitudinal sectional view through the entire unit with broken lines illustrating adjusted positions of parts as well as hidden parts;
  • FIGURE 2 is a bottom view of the device with portions thereof broken away to illustrate construction more fully; broken lines illustrate hidden and adjusted positions of parts; 1
  • FIGURE 3 is a rear elevation of the device in which broken lines illustrate hidden parts
  • FIGURE 4 is a fragmentary side elevation of the device with portions broken away to illustrate the action of the deection damper; broken lines illustrate hidden and adjusted positions of parts;
  • FIGURE 5 is a vertical section taken on the line 5--5 of FIGURE 1; broken lines illustrate hidden portions;
  • FIGURE 6 is a vertical section taken along the line 6 6 of FIGURE l; broken lines illustrating hidden parts;
  • FIGURE 7 is a fragmentary rear elevation with the discharge nozzle removed;
  • FIGURE 8 is a horizontal section taken on the line 8-8 of FIGURE lrwith broken lines illustrating hidden parts
  • FIGURE 9 is a reduced side elevation of the unit and its driving engine secured to the transom of a boat which is shown fragmentarily and in section; broken lines illustrate hidden parts; and
  • FIGURE l0 is a plan View of the engine shown in FIGURE 9 to illustrate the lateral disposition of the braces therefor.
  • the jet unit is seen to have a housing 20 which is divided into two portions designated 20A and ZtiB.
  • housing 20 Within housing 20 are rigid vertical water directing vanos 21 which direct water from intake 22 in a substantially straight path toward impeller 24.
  • the horizontal vanes 25 are curved downward at their outer ends order to divide water coming in through intake 22 approximately evenly between the upper and lower halves of the impeller entrance.
  • the Water directing varies 26 At the rear of impeller 24 are the Water directing varies 26 which take the water impelled by impeller 24 and straighten it for a substantially straight thrust in the direction of the discharge nozzle assembly 27.
  • Irnpeller 24 is rotatably supported within-the housing 2i) on an impeller shaft 23.
  • This shaft is made of any suitable material such as stainless steel having great strength as well as resistance to corrosion by water.
  • the impeller shaft has a shoulder 29 formed thereon against which central cone of impeller 24 abuts to determine the forward position of impeller 24 on shaft 2S.
  • the rear end of shaft 28 is reduced as at 31'so that a'nut 32.
  • Shaft 28 is rotatably supported at the forward or transom end of housing portion 29A by means ,of suit- It will be seenV that the shoulder of the Vhousing'portion 20A against which impeller 24and wear able bearing-s 39 which are protected from water by vmeans Vof a packing nut 4G bearing on and providing a tight seal with the packing gland 41.
  • Grease for bearing port 39 is provided via a suitable grease fitting as seen at 46.
  • FIG. 1 l isseen a fragmentary portion of the engine. It is secured to the transom 4S by means of a suitable mounting plate or flange 49 and bolts such as those disclosed at 50 and 51 extend through both the mounting flange 49 and appropriate flanges in portions of housing 20A as well asy the transom 48 to pull both of the mounting anges of the two portions of the entire structure tightly against transom 48;
  • a 'sealing member or gasket such as that disclosed at 52 is provided between the mounting ilangeof housing 20A and transom 4S.
  • a similar seal or gasket is desirably positioned at 54 between mounting flange 49 of engine 47 and transom 4?.
  • neckpo'rtion 45 is xedly'located with respect to the shaft 28 and the drive shaft 56 is xedlyrlocated with respect to ⁇ collar portion 55.
  • a yielding joint of the type in which cooperating portions on the two shafts interlace and are buffered with yielding, resilient material such as rubber or the like is seen atv 57. While'the two shafts are aligned by the interaction of the neck. and collar structure, there may wellbe some movementof the engine with respect to the water jet unit particularly in rough water or under high output conditions. For this reason a yielding coupling is considered necessary at this point. Since the jet unit and the engine is close-coupled, however, it is not imperative to have a relatively complex universal joint at this ljuncture of the shafts.
  • the engine Y47 will be seen also to be provided with the rigid braces 58 and 59 which extend from the engine block, and are secured thereto with suitable cap lscrews as at 60 and 61, to the transom 48 of the boat and ⁇ secured in any ⁇ suitable manner as by the bolts 62.
  • Additional means for supporting the end of the engine spaced from the -transom 43 may he employed in the form of a bracket 64 which is suitably secured as by the cap screws 65 to engine block 47 and resting en the air supports or shocks 66.' ⁇ These in turn rest on the inside bottom of hull 67.
  • Either of these means for supporting the engine end spaced from the transom may be employed individually or jointly, depending on the nature ofthe hull with which the structure is used and various other factors. As seen in FIG- URE l0 the engine is braced laterally as well as vertically by the supporting struts 53 and 59.
  • shaft 28 at lits rear portion 31 is rotatably supported by the central cone 63 of the vane units 26.
  • portion 20B may be fitted thereon by screwing together the threads shown at 69.
  • a gasket, as at 70, will provide a seal for the two portions 24M-2GB when the threads at 69 have been engaged suiciently to hold the two units together, yet ⁇ gasket will yield enough to permit continued rotation of 29B until the assembly is properly arrangedV as to have the discharge and control arrangement of the unit properly oriented to housingportion 20A.
  • a tail cone piece 72 is press-'fitted into the cone portion 68 to both close off and protect the rear end of shaft 28 and also provide ⁇ a means for applying a grease fitting 74 thereto by means of which grease is applied to the bearing sur-face within cone 68 that supports the rearV end 31 of shaft 28.
  • the fonward end of cone 684 is slightly smaller than the rearend of cone Si) of the impeller. Asseen at 75 the for-ward cone of the impeller over-hangs the cone of vanes 26 s-o that water is directed on the outside of cone 28 principally. Between the two cones is a slight space as at 76 in which there is always maintained a slight pressure. At this point in housing 20B is a port 77 into which an appropriate tube 78 shown in fragment connects and extends to the water jacket of the engine. engine calls for cooling liquid, the pressure area 76 will cause water to flow through port 77 and tube 78 to cool the engine. Water which has been used for cooling is allowed to overflow int-o the water in which the boat is operating, in the usual manner. Other details of this structure are common ⁇ in usage and therefore not shown in detail. Y
  • housing 20B At Vthe rear ⁇ of housing 20B is formed'a socket portion 79 into which the control discharge nozzle 27 is inserted.
  • a tapered ring 80 provides a close it' to the ball portion of discharge Ynozzile 27;
  • The'ring 80 and ball 27Y are simultaneously pushed into the housing 29B. They are a very tight slip fit, -Once these units are properly positioned within the housing 26B, the pin units 81 are inserted which extend throughboth the ring and the nozzle 27;
  • Stub shaft portions 82 serve asthe pivot points for the discharge nozzle 27.
  • VThus discharge nozzle 27 is pivoted about a vertical axis formed by the stub shafts 82 ⁇ sothat it-can swing to the right or left as disclosed by the broken lines in-FIGURE 2. Vanes S3 in nozzle 27 both stilfen the ball .portion of nozzle 27 and aid Iin reducing turbulence of the ⁇ water flowing through the unit.
  • the discharge nozzle is provided with a main discharge port 84 which'enlarges from the smallest portion of the passageway for water as at 85 to the actual exhaust open- Whenever the thermostat of theV ing 86 of the unit. Pivoted within this enlarging discharge portion of nozzle 27 is a deflection plate 87. Yoke structure 88 is journalled in the sides of the nozzle and supports the plate in any of the various positions to which it may be pivoted by means of the yoke 88.
  • the ends of yoke 88 that embrace the deflection plate 87 are only slightly engaged with the plate itself so that the area between the two ends of the yoke that grip the deflection plate is nearly as great as the reduced opening 85 of the discharge nozzle. Because the discharge nozzle flares or enlarges from its most restricted point S5, to the actual point of discharge of the jet from the unit, the walls of the aring portion 84 of the jet do not have any substantial contact with the water being expelled through d-ischarge port 85.
  • Reverse port 89 not only serves to discharge water in a forwardly direction when the power of the unit is used to reverse the boat, it also acts as an air intake when the boat is thrusting forward as would be the case when the deect-ion plate S7 is positioned as shown in FIGURE 1.
  • the jet unit is largely raised out of the water as the boat planes on the bottom 67 of its hull. Air is therefore allowed to enter through port 89 and in doing so it mixes with the water being discharged through discharge port 86 and produces an aeration or bubbling action similar-to bubbling or non-splashing faucets which are common. 'I'his bubbling action also serves to prevent any substantial skin friction or liquidnozzle friction Vafter the water passes the narrow point 85 of the discharge nozzle 27.
  • Yoke 88 may he moved forward and backward by any suitable means ⁇ such as the heavy Bowden wire 90 having the usual casing 9.1.
  • any suitable means such as the heavy Bowden wire 90 having the usual casing 9.1.
  • the Bowden wire 90 extends forward to a suitable control adjacent to the operator of the vehicle, he can, by appropriately positioning his control lever, move plate 87 to the position shown in broken lines in FIGURE 1, in order to deflect at least some of the water being discharged upwardly. This deflection of the water being discharged through the jet tends to thrust the rear of the jet unit down and the nose of the boat up, which is of assistance in getting the boat up into a planing position on top of the water.
  • this same control may be moved to the extreme rearward position as shown in solid lines in that figure, which deects substantially all of the water being discharged through restn'cted area 85 out through the reverse port 89.
  • the entireV thrust of the engine is being applied to move the boat backward through the water.
  • the broken line position shown in FIGURE 4, is one in which water being discharged straight rearwardly and through reverse port 89 is divided.
  • a neutral position may be located at which the rearward thrust and the forward thrust are substantially balanced and this produces no movement of the boat regardless of the power being exerted by the engine.
  • the broken line position in FIGURE 4 is approximately a neutral position. It will be seen, therefore, that the deflection plate 87 may be used to direct all of the thrust of the engine selectively through the discharge port 86 or the Vreverse .port 89 at will.
  • the water being discharged through these ports may be divided proportionately in order to produce very controlled forward and backward motion as when maneuvering up to a dock or the like.
  • the deection plate 87 s entirely contained within nozzle portion 84. For this reason, regardless of the direction in which water is being deflected, it is always being employed usefully and not merely spraying out into the air in a useless or even lso .peller 24 rotates counter-clockwise.
  • yoke 88V is divided into two portion-s and suitably clamped together as by the bolt assembly units 92. For this reason, the yoke may be disassembled and removed from the portion 84 of the discharge nozzle 27 in order to remove the deflection plate 87 for service or repair.
  • the deflection plate is provided with the notches 94 and the ends of the yoke portions are bifurcated so as to embrace the top and bottom ⁇ of the plate.
  • the bifurcated ends of the yoke portions retain the plate on its top and bottom while the engagement of the yoke portion with the notches 94 causes -the plate to be retained in a forward and backward direction with the yoke.
  • Any suitable superstructure housing is used to both protect and lend an attractive appearance to the Bowden cable structure -91.
  • This housing may be any suitable casting, stamping or extrusion that is secured to the outside of the housings 20A and 20B.
  • Suitable means such as the cables 95 which are secured to the pierced ears 96 thatA are at the outer end of the discharge nozzle 277.
  • cables 95 have excellent leverage in pulling the discharge nozzle either to the right or left.
  • Ythe other is automatically released in the commonly understood manner by having them Isecured to a steering wheel drum or other similar mechanism.
  • discharge nozzlef27 pivots about the points 82.
  • Suitable housings such as extrusions 97 are used to encase the'cables 95 on the exterior of housings 20A and 20B.
  • these extrusions are suitably secured to the housings by suitable means such as cap screws 98 and serve in addition to set screws 71 to hold the portions A20A and 20B of housing 20 in proper alignment with the axis of pivoting of dischargeV nozzle 27 in a vertical plane.
  • Cables 95 may be provided at the transom of the boat with any suitable sort of water seal and one suggested -form is an accordion pleated rubber sleeve arrangement that can be tightly secured to both the transom and the cable and yet yield suciently to provide steering. In this manner, water is prevented from gaining access to the interior of the boat, yet the housings 97 are left open at their rear ends in order to achieve drainage whenever water does enter these housings.
  • FIGURE 2 also is shown the grille 99, the purpose of which is to limit the size objects entering intake 22.
  • a grille such as that shown at 99 is used over intake l 22, any object that is small enough to enter the intake 22 lis small enough to be pumped directly through the jet and exhausted through exhaust port 86.
  • housing 93 has sufficient flare at its rear end to permit the Bowden cable 90 to yield laterally in either ⁇ direction as discharge nozzle 27 is turned.
  • impeller 24 will be seen to have vanes in it that are slanted after the manner of a propeller blade as well as being angled radially from a position near the shaft 28 at the entrance to the impeller to an exit portion more widely spaced from the shaft. For this reason impeller 24 not only exerts axial thrust after the manner of a water screw, but also throws the water out its discharge port with considerable force as a centrifugal pump. As shown in FIGURE 5, the im- This dual radial and exial thrust imparted Ito the water being thrown by lmpeller 24 produces an extremely high volume as well as substantial force pump.
  • FIGURE 7 which is a view looking at the vanes Z6 from -the discharge nozzle end thereof, shows that they have rear portions which extend in a straight line with respect to the length of the unit thereby discharging the water in an almost straight stream toward the discharge nozzle 27.
  • a waterjet propulsion unit comprising a housing, an impeller rotatably mounted in said housing, a socket portion in said housing to the rear ofl said impeller, a'discharge nozzle pivotally mounted on a vertical axis in said socket, a discharge port in the rear of said discharge nozzle, a reverse port near said discharge port, and a deflection damper pivotally mounted on a horizontal axis within said discharge nozzle port area Lwhereby Water being discharged through said discharge.
  • nozzle may be deflected through said discharge and reverse ports selectively and proportionately at will, said deection damper including a plate notched at its sides and a split yoke journalled in said discha-rge nozzle and having bifurcated ends engaging A ⁇ the notches in said deflection damper plate.
  • jet propulsion unit comprising a housing, and an impeller secured to said impeller shaft within said housing, a plurality Vof water directingV vanesk inside said housing both in front of and behind said impellera socketA portion in Said housing behind the vanes to the rear of said impeller, a discha-rge nozzle pivotally mounted on a vertical axis in said socket, said discharge nozzle hav-ing aforward converging portion and a rearward diverging portion, a discharge port at therear of said diverging portion, a reverse port near said discharge port, and a deection damper pivotally mounted on a horizontal axis entirely within said diverging portion ofl saidV discharge -nozzle whereby
  • a water jet propulsion unit adapted to be mounted outside a boat transom comprising a housing, an impeller rotatably mounted in said housing, a plurality of xed water directing vanes inside said housing and both in front of and behind said impeller, a socket portionin said housing behind the vanes to the rear of said impeller, a discharge nozzle pivotally mounted on a vertical axis in said socket, said discharge nozzle having a forward converging section and a rearward diverging section, a discharge port atthe rear of said discharge nozzle, a reverse port formed in said discharge nozzle near said discharge port, and a deflection damper pivotally mounted on a horizontal axis entirely within the dive-rging section of said discharge nozzle whereby water being discharged through said discharge nozzle may be deflected propor. tionately and exclusively through said Adischarge andv reverse ports, and means for pivoting said discharge nozzle independently of the action of said deflection damper;
  • a water jet propulsion unit being adapted to be mounted entirelyon the outside of a boat transom comprising a housing, an impeller rotatably mountedV in said housing, a discharge nozzle secured to said housing and including a forward converging section. and a rearward diverging section, a discharge port at the rear of said ⁇ dive-rging section, a reverse port formed in said discharge nozzle near said discharge port, and a deflection damper pivotally mounted intermediate its ends on a horizontal axis entirely within said diverging section of said discharge nozzle ywhereby water being discharged through said discharge nozzle is deflected proportionately, selectively and exclusively through said discharge and .reverse ports.

Description

June 8, 1965 A. Fox l 3,187,708
PRoPULsIoN DEVICE Filed June '7.v 1961 3 Sheets-Sheet 2 `-f ze t INVENTOR. ANTHONY Fox Arran/ver:
Junes, 1965 A, Fox PRoP-.ULsIoN DEVICE Filed June 7, 19511l I 3 Sheets-Sheesh FIG. l0
INV EN TOR.
F/G. 9 ANTHONY Fox @www gqrTakNe-YJ United States Patent Office 3,187,708 Patented June 8, 1965 3,187,708 PRPULSION DEVICE Anthony Fox, Minneapolis, Minn., assignor to Propulsion Research, Inc., Minneapolis, Minn., a corporation of Minnesota Filed .lune 7, 1961, Ser. No. 115,463 6 Claims. (Cl. 11S-12) This invention is a propulsion unit for boats that supplants the gear box, propeller and rudder structure of a usual power boat arrangement. It is believed to be novel in the particular construction of the housing in which the impeller and water controlling vanes are arranged in that the outside shell of the unit is very smooth and has a minimum of projections thereon which might engage and snag on objects in the water. This streamlined construction is achieved in part by having portions of the housing that are normally secured together by anges being secured by threads instead. The forward and reverse mechanism consists of a balanced deflector damper within the discharge nozzle which permits deflecting the water jet through forward or reverse ports. Yet another novel point of construction in this jet propulsion unit is the manner of mounting it and the engine which drives it in close-coupled arrangement on opposite sides of the transom of the boat so as to occupy a minimum of space both inside and outside and With the jet unit entirely outside of the boat hull. It is also believed novel in this type of unit to have the pivoting steering arrangement held in by a wear ring that establishes the position of the steering unit with threaded stub shafts serving both to hold the wear ring in the housing and provide the pivots for steering. Also novel is the flared discharge nozzle which minimizes friction between the nozzle and water being discharged.
Water jet propulsion units for boats are not novel in themselves, but many of the units that have been presented to the purchasing public are at least somewhat unsatisfactory in one or more of the following respects. They are frequently excessively long, heavy and expensive. They are often incapable of operating in a trouble free manner under conditions in which silt, sand and other smalll particles of hard materials are suspended in the water in which the craft is operating. The construction of some is such that they are ditlicult or impossible to steer when reversed. Most of these units heretofore offered occupy as much or more space inside the boat as a comparable propeller driving power plant would. Most also require cutting holes in the bottom of the hull, thus weakening the same, and increasing the likelihood of failure as the result of high speed engine operation and the interaction of the hull with water, especially rough water.
Accordingly, it is the principal object of this invention to provide an improved jet propulsion unit for watercraft.
Yet another object of this invention is to provide a jet propulsion unit for watercraft that can be mounted in close-coupled arrangement with an engine on opposite sides of the boat transom.
A further object of this invention is to provide a jet propulsion unit for boats that is substantially trouble free regardless of the conditions under which it is operated.
A still further object of this invention is to provide a jet propulsion unit for boats of simplified construction.
Yet another object of this invention is to provide a jet propulsion unit for boats having relatively high water capacity but small outside dimensions.
A still further object of this invention is to provide a jet propulsion and engine unit for a boat in which the mounting flanges of the propulsion unit and the engine cooperate to align the drive shaft of the engine with the impeller shaft of the propulsion unit.
It is another object of this invention to provide a jet propulsion unit for boats in which such materials as sand, grit, silt and the like will either be carried through the unit harmlessly or any elements which conceivably could be fouled by such materials may be quickly and easily cleared thereof.
Still another object of this invention is to provide a jet propulsion unit having a discharge nozzle which minimizes friction between water being discharged and the sides of the discharge nozzle.
Yet another object of this invention is to provide a mounting structure for both theY engine and the propulsion unit whereby they are entirely supported by a single element of the boat hull.
Other and further objects of the invention are those inherent and apparent in the apparatus as described, pictured and claimed.
To the accomplishment of the foregoing and related ends, this invention then comprises the features hereinafter fully described and particularly pointed out'in the claims, the following description setting forth in detail certain illustrative embodiments of the invention, these being indicative, however, of but a few of the various ways in which the principles of the invention may be employed.
The invention will be described with reference to the drawings in which corresponding numerals refer to the same parts and in which:
FIGURE 1 is a longitudinal sectional view through the entire unit with broken lines illustrating adjusted positions of parts as well as hidden parts;
FIGURE 2 is a bottom view of the device with portions thereof broken away to illustrate construction more fully; broken lines illustrate hidden and adjusted positions of parts; 1
FIGURE 3 is a rear elevation of the device in which broken lines illustrate hidden parts;
FIGURE 4 is a fragmentary side elevation of the device with portions broken away to illustrate the action of the deection damper; broken lines illustrate hidden and adjusted positions of parts;
FIGURE 5 is a vertical section taken on the line 5--5 of FIGURE 1; broken lines illustrate hidden portions;
FIGURE 6 is a vertical section taken along the line 6 6 of FIGURE l; broken lines illustrating hidden parts; FIGURE 7 is a fragmentary rear elevation with the discharge nozzle removed;
' FIGURE 8 is a horizontal section taken on the line 8-8 of FIGURE lrwith broken lines illustrating hidden parts;
FIGURE 9 is a reduced side elevation of the unit and its driving engine secured to the transom of a boat which is shown fragmentarily and in section; broken lines illustrate hidden parts; and
FIGURE l0 is a plan View of the engine shown in FIGURE 9 to illustrate the lateral disposition of the braces therefor.
Referring to the drawings and particularly to FIG- URE l, the jet unit is seen to have a housing 20 which is divided into two portions designated 20A and ZtiB. Within housing 20 are rigid vertical water directing vanos 21 which direct water from intake 22 in a substantially straight path toward impeller 24. The horizontal vanes 25 are curved downward at their outer ends order to divide water coming in through intake 22 approximately evenly between the upper and lower halves of the impeller entrance. At the rear of impeller 24 are the Water directing varies 26 which take the water impelled by impeller 24 and straighten it for a substantially straight thrust in the direction of the discharge nozzle assembly 27. Irnpeller 24 is rotatably supported within-the housing 2i) on an impeller shaft 23. This shaft is made of any suitable material such as stainless steel having great strength as well as resistance to corrosion by water. The impeller shaft has a shoulder 29 formed thereon against which central cone of impeller 24 abuts to determine the forward position of impeller 24 on shaft 2S. The rear end of shaft 28 is reduced as at 31'so that a'nut 32. may be slid over it before the portion 26B of the housing is positioned and theV nut tightened on the threads 34 to hold impeller from rearward motion on shaft 28.`V Impeller 24 is secured against rotation will respect to the shaft 2S by suitable means such as the key 3S.` While the housing 2t) is made from a strong lightweight alloy of aluminum and magnesium or other suitable material, a wear ring 36 is pressed into the housing at the point where the forward end of the impeller cornes closest to it. Wear ring 36 vmay be of any suitable material and a suggested one that has been found practical is what is known as Creamery metal, it being an alloy of nickel and brass which is reasonably hard and at the same time corrosion resistant.
-ring 36 abut, as at 37, is such that the opening for water to pass into the interior of the impeller 24 is slightly smaller than the opening of the impeller itself. For this reason, any material being carried with the water will not get` between the impeller and the wear ring 36 but 'instead Will be carried with the flow of water through the impeller and outthe rear of the unit. It will also be seen 'as at 38 that there is clearance between kthe impeller and the housing members 26A and 29B to allow any materials which do get into this area to be carried on rearward by theflow of water.`
Shaft 28 is rotatably supported at the forward or transom end of housing portion 29A by means ,of suit- It will be seenV that the shoulder of the Vhousing'portion 20A against which impeller 24and wear able bearing-s 39 which are protected from water by vmeans Vof a packing nut 4G bearing on and providing a tight seal with the packing gland 41. A ring, as shown at 42, suitably secured by cap screws 44, holds the bearing inthe neck portion of housing portion 20A. Grease for bearing port 39 is provided via a suitable grease fitting as seen at 46.
At 47 in FIGURE l isseen a fragmentary portion of the engine. It is secured to the transom 4S by means of a suitable mounting plate or flange 49 and bolts such as those disclosed at 50 and 51 extend through both the mounting flange 49 and appropriate flanges in portions of housing 20A as well asy the transom 48 to pull both of the mounting anges of the two portions of the entire structure tightly against transom 48; A 'sealing member or gasket such as that disclosed at 52 is provided between the mounting ilangeof housing 20A and transom 4S. A similar seal or gasket is desirably positioned at 54 between mounting flange 49 of engine 47 and transom 4?. Within mounting flange 49 is formed the ring 55 which iits snugly neck portion 45 of housing portion 20A'. Neckpo'rtion 45 is xedly'located with respect to the shaft 28 and the drive shaft 56 is xedlyrlocated with respect to `collar portion 55.' These fixed shaft, collar and neck relations correspond so that the entrance of neck portion 45, including .the plate 42, into the collar 55, causes the shaft 2S to align with the shaft 56.
A yielding joint of the type in which cooperating portions on the two shafts interlace and are buffered with yielding, resilient material such as rubber or the like is seen atv 57. While'the two shafts are aligned by the interaction of the neck. and collar structure, there may wellbe some movementof the engine with respect to the water jet unit particularly in rough water or under high output conditions. For this reason a yielding coupling is considered necessary at this point. Since the jet unit and the engine is close-coupled, however, it is not imperative to have a relatively complex universal joint at this ljuncture of the shafts.
Referring to FIGURES 9 and l0, the engine Y47 will be seen also to be provided with the rigid braces 58 and 59 which extend from the engine block, and are secured thereto with suitable cap lscrews as at 60 and 61, to the transom 48 of the boat and` secured in any` suitable manner as by the bolts 62. Additional means for supporting the end of the engine spaced from the -transom 43 may he employed in the form of a bracket 64 which is suitably secured as by the cap screws 65 to engine block 47 and resting en the air supports or shocks 66.'` These in turn rest on the inside bottom of hull 67. Either of these means for supporting the engine end spaced from the transom may be employed individually or jointly, depending on the nature ofthe hull with which the structure is used and various other factors. As seen in FIG- URE l0 the engine is braced laterally as well as vertically by the supporting struts 53 and 59.
Referring again to FIGURE 1, shaft 28 at lits rear portion 31 is rotatably supported by the central cone 63 of the vane units 26. Once the shaft 2i; and impeller 24 are secured in the housing portion 20A, portion 20B may be fitted thereon by screwing together the threads shown at 69. A gasket, as at 70, will provide a seal for the two portions 24M-2GB when the threads at 69 have been engaged suiciently to hold the two units together, yet` gasket will yield enough to permit continued rotation of 29B until the assembly is properly arrangedV as to have the discharge and control arrangement of the unit properly oriented to housingportion 20A. When the two housing portions 20A-2GB are correctly aligned, one or more set screws 7d are inserted and tightened to positively hold the two housing portions` in proper alignment. A tail cone piece 72 is press-'fitted into the cone portion 68 to both close off and protect the rear end of shaft 28 and also provide `a means for applying a grease fitting 74 thereto by means of which grease is applied to the bearing sur-face within cone 68 that supports the rearV end 31 of shaft 28.`
A-t this point it is to be noted that the fonward end of cone 684 is slightly smaller than the rearend of cone Si) of the impeller. Asseen at 75 the for-ward cone of the impeller over-hangs the cone of vanes 26 s-o that water is directed on the outside of cone 28 principally. Between the two cones is a slight space as at 76 in which there is always maintained a slight pressure. At this point in housing 20B is a port 77 into which an appropriate tube 78 shown in fragment connects and extends to the water jacket of the engine. engine calls for cooling liquid, the pressure area 76 will cause water to flow through port 77 and tube 78 to cool the engine. Water which has been used for cooling is allowed to overflow int-o the water in which the boat is operating, in the usual manner. Other details of this structure are common `in usage and therefore not shown in detail. Y
At Vthe rear` of housing 20B is formed'a socket portion 79 into which the control discharge nozzle 27 is inserted. A tapered ring 80 provides a close it' to the ball portion of discharge Ynozzile 27; The'ring 80 and ball 27Y are simultaneously pushed into the housing 29B. They are a very tight slip fit, -Once these units are properly positioned within the housing 26B, the pin units 81 are inserted which extend throughboth the ring and the nozzle 27; Stub shaft portions 82 serve asthe pivot points for the discharge nozzle 27. VThus discharge nozzle 27 is pivoted about a vertical axis formed by the stub shafts 82` sothat it-can swing to the right or left as disclosed by the broken lines in-FIGURE 2. Vanes S3 in nozzle 27 both stilfen the ball .portion of nozzle 27 and aid Iin reducing turbulence of the `water flowing through the unit.
The discharge nozzle is provided with a main discharge port 84 which'enlarges from the smallest portion of the passageway for water as at 85 to the actual exhaust open- Whenever the thermostat of theV ing 86 of the unit. Pivoted within this enlarging discharge portion of nozzle 27 is a deflection plate 87. Yoke structure 88 is journalled in the sides of the nozzle and supports the plate in any of the various positions to which it may be pivoted by means of the yoke 88. As shown in FIGUTRES 1 and 2, as well as in FIGURE 8, the ends of yoke 88 that embrace the deflection plate 87 are only slightly engaged with the plate itself so that the area between the two ends of the yoke that grip the deflection plate is nearly as great as the reduced opening 85 of the discharge nozzle. Because the discharge nozzle flares or enlarges from its most restricted point S5, to the actual point of discharge of the jet from the unit, the walls of the aring portion 84 of the jet do not have any substantial contact with the water being expelled through d-ischarge port 85.
At the bottom of .the discharge portion S4 is the reverse port 89. Reverse port 89 not only serves to discharge water in a forwardly direction when the power of the unit is used to reverse the boat, it also acts as an air intake when the boat is thrusting forward as would be the case when the deect-ion plate S7 is positioned as shown in FIGURE 1. At this time the jet unit is largely raised out of the water as the boat planes on the bottom 67 of its hull. Air is therefore allowed to enter through port 89 and in doing so it mixes with the water being discharged through discharge port 86 and produces an aeration or bubbling action similar-to bubbling or non-splashing faucets which are common. 'I'his bubbling action also serves to prevent any substantial skin friction or liquidnozzle friction Vafter the water passes the narrow point 85 of the discharge nozzle 27.
Yoke 88 may he moved forward and backward by any suitable means `such as the heavy Bowden wire 90 having the usual casing 9.1. When the plate 87 is positioned as shown in FIGURE l, all o'f the power of the jet is directed straight rearward for the greatest forward thrust. As the Bowden wire 90 extends forward to a suitable control adjacent to the operator of the vehicle, he can, by appropriately positioning his control lever, move plate 87 to the position shown in broken lines in FIGURE 1, in order to deflect at least some of the water being discharged upwardly. This deflection of the water being discharged through the jet tends to thrust the rear of the jet unit down and the nose of the boat up, which is of assistance in getting the boat up into a planing position on top of the water. As shown in FIGURE 4, this same control may be moved to the extreme rearward position as shown in solid lines in that figure, which deects substantially all of the water being discharged through restn'cted area 85 out through the reverse port 89. In this position of plate 37, the entireV thrust of the engine is being applied to move the boat backward through the water.
The broken line position, shown in FIGURE 4, is one in which water being discharged straight rearwardly and through reverse port 89 is divided. By this dividing of the thrust from the jet, a neutral position may be located at which the rearward thrust and the forward thrust are substantially balanced and this produces no movement of the boat regardless of the power being exerted by the engine. The broken line position in FIGURE 4 is approximately a neutral position. It will be seen, therefore, that the deflection plate 87 may be used to direct all of the thrust of the engine selectively through the discharge port 86 or the Vreverse .port 89 at will. Furthermore, the water being discharged through these ports may be divided proportionately in order to produce very controlled forward and backward motion as when maneuvering up to a dock or the like.
As shown in FIGURES 1, 4 and 8, the deection plate 87 s entirely contained within nozzle portion 84. For this reason, regardless of the direction in which water is being deflected, it is always being employed usefully and not merely spraying out into the air in a useless or even lso .peller 24 rotates counter-clockwise.
annoying manner as to throw water on the' occupants of the craft being ypowered by the jet unit.
As shown in FIGURE 3, yoke 88V is divided into two portion-s and suitably clamped together as by the bolt assembly units 92. For this reason, the yoke may be disassembled and removed from the portion 84 of the discharge nozzle 27 in order to remove the deflection plate 87 for service or repair. As shown in FIGURE 8, the deflection plate is provided with the notches 94 and the ends of the yoke portions are bifurcated so as to embrace the top and bottom `of the plate. Thus the bifurcated ends of the yoke portions retain the plate on its top and bottom while the engagement of the yoke portion with the notches 94 causes -the plate to be retained in a forward and backward direction with the yoke. This structure has been found extremely trouble free, and if trouble should develop, the disassembly of the yoke by removing the bolts 92 makes it possible to repair any difficulty quickly and easily. Any suitable superstructure housing, as shown at 93, is used to both protect and lend an attractive appearance to the Bowden cable structure -91. This housing may be any suitable casting, stamping or extrusion that is secured to the outside of the housings 20A and 20B.
As shown in FIGURE 2, steering is controlled by suitable means such as the cables 95 which are secured to the pierced ears 96 thatA are at the outer end of the discharge nozzle 277. For this reason cables 95 have excellent leverage in pulling the discharge nozzle either to the right or left. When one cable is pulled, Ythe other is automatically released in the commonly understood manner by having them Isecured to a steering wheel drum or other similar mechanism. When one of the cables is tightened and the other loosened, discharge nozzlef27 pivots about the points 82. Suitable housings such as extrusions 97 are used to encase the'cables 95 on the exterior of housings 20A and 20B. As shown in FIGURE 9, these extrusions are suitably secured to the housings by suitable means such as cap screws 98 and serve in addition to set screws 71 to hold the portions A20A and 20B of housing 20 in proper alignment with the axis of pivoting of dischargeV nozzle 27 in a vertical plane. Cables 95 may be provided at the transom of the boat with any suitable sort of water seal and one suggested -form is an accordion pleated rubber sleeve arrangement that can be tightly secured to both the transom and the cable and yet yield suciently to provide steering. In this manner, water is prevented from gaining access to the interior of the boat, yet the housings 97 are left open at their rear ends in order to achieve drainage whenever water does enter these housings.
l In FIGURE 2 also is shown the grille 99, the purpose of which is to limit the size objects entering intake 22. When a grille such as that shown at 99 is used over intake l 22, any object that is small enough to enter the intake 22 lis small enough to be pumped directly through the jet and exhausted through exhaust port 86. As seen in FIG- URE 3, housing 93 has sufficient flare at its rear end to permit the Bowden cable 90 to yield laterally in either` direction as discharge nozzle 27 is turned.
Referring to FIGURE 5, impeller 24 will be seen to have vanes in it that are slanted after the manner of a propeller blade as well as being angled radially from a position near the shaft 28 at the entrance to the impeller to an exit portion more widely spaced from the shaft. For this reason impeller 24 not only exerts axial thrust after the manner of a water screw, but also throws the water out its discharge port with considerable force as a centrifugal pump. As shown in FIGURE 5, the im- This dual radial and exial thrust imparted Ito the water being thrown by lmpeller 24 produces an extremely high volume as well as substantial force pump. By comparing FIGURES 6 and 7, vanes 26 will be seen to slant at their ends nearest to impeller 24 in the opposite direction to the direction of slant of the impeller blade. In this manner the water that is given some rotating or torque action,.as the result of the rotary action of the impeller, tends to have its rotary motion' counteracted and straightened Vout. FIGURE 7, which is a view looking at the vanes Z6 from -the discharge nozzle end thereof, shows that they have rear portions which extend in a straight line with respect to the length of the unit thereby discharging the water in an almost straight stream toward the discharge nozzle 27. As a result of the interaction of the impeller and vanes 2e, very little of the torque action of the unit is'felt in the operation of the boat itself.
It is apparent that manymoditications and variations of this invention as hereinbefore vset forth may be made without departing from the spirit andrscope thereof. The
lspecific embodiments described are given by way of vex ample only and the inventionwis limited only by the terms of the appended claims. What is claimed is:
1. `A waterjet propulsion unit comprising a housing, an impeller rotatably mounted in said housing, a socket portion in said housing to the rear ofl said impeller, a'discharge nozzle pivotally mounted on a vertical axis in said socket, a discharge port in the rear of said discharge nozzle, a reverse port near said discharge port, and a deflection damper pivotally mounted on a horizontal axis within said discharge nozzle port area Lwhereby Water being discharged through said discharge. .nozzle may be deflected through said discharge and reverse ports selectively and proportionately at will, said deection damper including a plate notched at its sides and a split yoke journalled in said discha-rge nozzle and having bifurcated ends engaging A`the notches in said deflection damper plate. y
2. Thercombination of claim 1 ingwhichthe narrowest part of said discharge nozzle is in front of said split yoke and the ends of the split yoke when engaged with said plateare spaced a distance equal to the inside di# ameter of the smallest partV of said discharge nozzle.
3. In combination with a boat transom, an engine havling a crank shaft, a mounting flange on saidV engine, a Iwater jet propulsion unit having an impeller shaft, mounting means cooperating with the mounting flange ofV said engine and being adapted to support said water jet propulsion unitV entirely outside said transom, said water; jet propulsion unit comprising a housing, and an impeller secured to said impeller shaft within said housing, a plurality Vof water directingV vanesk inside said housing both in front of and behind said impellera socketA portion in Said housing behind the vanes to the rear of said impeller, a discha-rge nozzle pivotally mounted on a vertical axis in said socket, said discharge nozzle hav-ing aforward converging portion and a rearward diverging portion, a discharge port at therear of said diverging portion, a reverse port near said discharge port, and a deection damper pivotally mounted on a horizontal axis entirely within said diverging portion ofl saidV discharge -nozzle whereby water discharged through said dischargel nozzle may be deflected throughrsaid discharge and reverse ports selectively and proportionately at will, means for pivoting saidvdisharge nozzle independently of the action of said dellection damper, and means in addition to said mounting flange for supporting the portion of said engine spaced from said transom. n
4.V The combination of claim 3 in which the mounting flange of said engine has a collar formed therein and said mounting means includes a neck formed thereon that slidably sits snugly Within said collar of said mounting flange of said engine.
5. A water jet propulsion unit adapted to be mounted outside a boat transom comprising a housing, an impeller rotatably mounted in said housing, a plurality of xed water directing vanes inside said housing and both in front of and behind said impeller, a socket portionin said housing behind the vanes to the rear of said impeller, a discharge nozzle pivotally mounted on a vertical axis in said socket, said discharge nozzle having a forward converging section and a rearward diverging section, a discharge port atthe rear of said discharge nozzle, a reverse port formed in said discharge nozzle near said discharge port, and a deflection damper pivotally mounted on a horizontal axis entirely within the dive-rging section of said discharge nozzle whereby water being discharged through said discharge nozzle may be deflected propor. tionately and exclusively through said Adischarge andv reverse ports, and means for pivoting said discharge nozzle independently of the action of said deflection damper;
6. A water jet propulsion unit being adapted to be mounted entirelyon the outside of a boat transom comprising a housing, an impeller rotatably mountedV in said housing, a discharge nozzle secured to said housing and including a forward converging section. and a rearward diverging section, a discharge port at the rear of said `dive-rging section, a reverse port formed in said discharge nozzle near said discharge port, and a deflection damper pivotally mounted intermediate its ends on a horizontal axis entirely within said diverging section of said discharge nozzle ywhereby water being discharged through said discharge nozzle is deflected proportionately, selectively and exclusively through said discharge and .reverse ports.
ReferencesCited by the Examiner Y UNITED. STATES PATENTS 343,769 6/86 Levi 277--100 1,554,591` 9/25 Oliver 103-90 t 1,765,789 V6/30V Ditchburn 11S-4l 2,024,274 12/35 Campini 115-14 2,446,942 8748 McFarland 11S-34 2,681,029 6/54 Canazzi 115-41 2,702,516 2/55 Tinker 115-16 3,007,305 1,1/61 Hamilton 115-14 3,083,679 4/ 63 Conover 115-34 MILTON BUCHLER, Primary Examiner.
ANDREW H. FARRELL, Examiner.

Claims (1)

1. A WATER JET PROPULSION UNIT COMPRISING A HOUSING, AN IMPELLER ROTATABLY MOUNTED IN SAID HOUSING, A SOCKET PORTION IN SAID HOUSING TO THE REAR OF SAID IMPELLER, A DISCHARGE NOZZLE PIVOTALLY MOUNTED ON A VERTICAL AXIS IN SAID SOCKET, A DISCHARGE PORT IN THE REAR OF SAID DISCHARGE NOZZLE, A REVERSE PORT NEAR SAID DISCHARGE PORT, AND A DEFLECTION DAMPER PIVOTALLY MOUNTED ON A HORIZONTAL AXIS WITHIN SAID DISCHARGE NOZZLE PORT AREA WHEREBY WATER BEING DISCHARGED THROUGH SAID DISCHARGE NOZZLE MAY BE DEFLECTED THROUGH SAID DISCHARGE AND REVERSE PORTS SELECTIVELY AND PROPORTIONATELY AT WILL, SAID DEFLECTION DAMPER INCLUDING A PLATE NOTCHED AT ITS SIDES AND A SPLIT YOKE JOURNALED IN SAID DISCHARGE NOZZLE AND HAVING BIFURCATED ENDS ENGAGING THE NOTCHES IN SAID DEFLECTION DAMPER PLATE.
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US3338169A (en) * 1965-10-19 1967-08-29 Thurlow R Kinney Reversible jet pump
US3347203A (en) * 1965-12-30 1967-10-17 Carter K Starry Boat propulsion means
US3735782A (en) * 1968-02-15 1973-05-29 Voith Gmbh J M Suction bend for centrifugal pumps
US3823897A (en) * 1972-05-30 1974-07-16 O Bloomquist Vertical take-off and landing aircraft
US3824946A (en) * 1972-08-30 1974-07-23 D Macardy Water jet propulsion unit
US3942464A (en) * 1973-07-13 1976-03-09 Schoell Harry L Water jet propelling apparatus for boats
US3943876A (en) * 1973-12-06 1976-03-16 Kiekhaefer Aeromarine Motors, Inc. Water jet boat drive
US3946556A (en) * 1974-10-25 1976-03-30 Rockwell International Corporation Integrated nozzle and steering mechanism for waterjets
FR2390329A1 (en) * 1977-05-12 1978-12-08 Kawasaki Heavy Ind Ltd WATER EJECTION PROPELLER
DE2947366A1 (en) * 1978-11-29 1980-06-12 Castoldi Spa BLAST DRIVE FOR SHIPS AND SUCTION DEVICE THEREFOR
US4541808A (en) * 1980-12-18 1985-09-17 Kawasaki Jukogyo Kabushiki Kaisha Water jet propulsion system
US5049096A (en) * 1989-12-27 1991-09-17 Henn Jimmy D Vaned diverter nozzle for jet boats
US5108257A (en) * 1989-05-26 1992-04-28 Pacific Machinery & Engineering Co., Ltd. Impeller for turbo pump for water jet propulsion machinery, and turbo pump including same impeller
US5123867A (en) * 1990-05-10 1992-06-23 Stefan Broinowski Marine jet propulsion unit
WO1993009024A1 (en) * 1991-11-04 1993-05-13 Mccall, Timothy, J. Personal watercraft gullet
WO1994025342A1 (en) * 1993-04-30 1994-11-10 Robert Arthur Blakemore Shroud for the drive shaft of a watercraft
US5370562A (en) * 1992-06-19 1994-12-06 Sanshin Kogyo Kabushiki Kaisha Water injection propulsion device
US20030049978A1 (en) * 2001-08-20 2003-03-13 Patrice Dusablon Watercraft having a jet propulsion system that generates improved thrust
US20060056956A1 (en) * 2004-09-10 2006-03-16 Tomohiro Fuse Water jet propeller
US20060234569A1 (en) * 2005-04-18 2006-10-19 Yeun-Junn Lin Powerboat
US20090061704A1 (en) * 2007-08-27 2009-03-05 Yuting Rui Weed Cutter for a Craft Propelled by a Water Jet
US20090325431A1 (en) * 2008-04-29 2009-12-31 Bombardier Recreational Products Inc. Method of indicating a deceleration of a watercraft
US20160031540A1 (en) * 2013-03-15 2016-02-04 Stefan Broinowski Marine ducted propeller jet propulsion system
US10597129B1 (en) 2013-03-15 2020-03-24 Stefan Broinowski Marine ducted propeller mass flux propulsion system

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US3338169A (en) * 1965-10-19 1967-08-29 Thurlow R Kinney Reversible jet pump
US3347203A (en) * 1965-12-30 1967-10-17 Carter K Starry Boat propulsion means
US3735782A (en) * 1968-02-15 1973-05-29 Voith Gmbh J M Suction bend for centrifugal pumps
US3823897A (en) * 1972-05-30 1974-07-16 O Bloomquist Vertical take-off and landing aircraft
US3824946A (en) * 1972-08-30 1974-07-23 D Macardy Water jet propulsion unit
US3942464A (en) * 1973-07-13 1976-03-09 Schoell Harry L Water jet propelling apparatus for boats
US3943876A (en) * 1973-12-06 1976-03-16 Kiekhaefer Aeromarine Motors, Inc. Water jet boat drive
US3946556A (en) * 1974-10-25 1976-03-30 Rockwell International Corporation Integrated nozzle and steering mechanism for waterjets
FR2390329A1 (en) * 1977-05-12 1978-12-08 Kawasaki Heavy Ind Ltd WATER EJECTION PROPELLER
DE2947366A1 (en) * 1978-11-29 1980-06-12 Castoldi Spa BLAST DRIVE FOR SHIPS AND SUCTION DEVICE THEREFOR
JPS562291A (en) * 1978-11-29 1981-01-10 Kasutorudei Spa S0C Suction apparatus for boat jet propeller
US4325699A (en) * 1978-11-29 1982-04-20 Societa' Castoldi S.P.A. Suction device for jet propulsion units for a watercraft and jet propulsion units comprising the same
US4541808A (en) * 1980-12-18 1985-09-17 Kawasaki Jukogyo Kabushiki Kaisha Water jet propulsion system
US5108257A (en) * 1989-05-26 1992-04-28 Pacific Machinery & Engineering Co., Ltd. Impeller for turbo pump for water jet propulsion machinery, and turbo pump including same impeller
US5049096A (en) * 1989-12-27 1991-09-17 Henn Jimmy D Vaned diverter nozzle for jet boats
US5123867A (en) * 1990-05-10 1992-06-23 Stefan Broinowski Marine jet propulsion unit
US6027383A (en) * 1990-05-10 2000-02-22 Broinowski; Stefan Marine ducted propeller jet propulsion unit
WO1993009024A1 (en) * 1991-11-04 1993-05-13 Mccall, Timothy, J. Personal watercraft gullet
US5236379A (en) * 1991-11-04 1993-08-17 Norman D. Harris Personal watercraft gullet
US5370562A (en) * 1992-06-19 1994-12-06 Sanshin Kogyo Kabushiki Kaisha Water injection propulsion device
WO1994025342A1 (en) * 1993-04-30 1994-11-10 Robert Arthur Blakemore Shroud for the drive shaft of a watercraft
US20030049978A1 (en) * 2001-08-20 2003-03-13 Patrice Dusablon Watercraft having a jet propulsion system that generates improved thrust
US7524220B2 (en) * 2004-09-10 2009-04-28 Honda Motor Co., Ltd. Water jet propeller
US20060056956A1 (en) * 2004-09-10 2006-03-16 Tomohiro Fuse Water jet propeller
US20060234569A1 (en) * 2005-04-18 2006-10-19 Yeun-Junn Lin Powerboat
US20090061704A1 (en) * 2007-08-27 2009-03-05 Yuting Rui Weed Cutter for a Craft Propelled by a Water Jet
US7950974B2 (en) * 2007-08-27 2011-05-31 Surfango, Inc. Weed cutter for a craft propelled by a water jet
US20090325431A1 (en) * 2008-04-29 2009-12-31 Bombardier Recreational Products Inc. Method of indicating a deceleration of a watercraft
US7901259B2 (en) * 2008-04-29 2011-03-08 Bombardier Recreational Products Inc. Method of indicating a deceleration of a watercraft
US20160031540A1 (en) * 2013-03-15 2016-02-04 Stefan Broinowski Marine ducted propeller jet propulsion system
CN105339259A (en) * 2013-03-15 2016-02-17 S·布洛诺斯基 Marine ducted propeller jet propulsion system
US10597129B1 (en) 2013-03-15 2020-03-24 Stefan Broinowski Marine ducted propeller mass flux propulsion system
CN111776184A (en) * 2013-03-15 2020-10-16 S·布洛诺斯基 Marine duct propeller jet propulsion system

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