US3004510A

US3004510A - Ship stabilizers

Info

Publication number: US3004510A
Application number: US754876A
Authority: US
Inventors: Nawara Jozef
Original assignee: Individual
Current assignee: Individual
Priority date: 1958-08-13
Filing date: 1958-08-13
Publication date: 1961-10-17
Anticipated expiration: 1978-10-17

Description

Oct. 17, 196.1 NAwARA 3,004,510

SHIP STABILIZERS Filed Aug. 15, 1958 INVENTOIL lgzefflawara United States Patent 3,004,510 I SHIP STABILIZERS Jozef Nawara, Ravenswood Hospital Laboratory, 1931 Wilson Ave., Chicago 49, Ill, FiledAug. 13, 1958, Sen No. 754,876 3 Claims, (Cl. 114G126) The present invention relates to ship stabilizers and has for its main object the provision of shipv stabihzm pl nes, pivotally supportable both adjacent the bow and stern of a ship. for reducing the pitching motion of a shi r Xnother object of the present invention is the provision of substantially. horizontal stabilizing planes, positioned below the water level, one pivotally supported adjacent the bow and another adjacent the stern of a ship, the two planes utilizing the alternate water pressures at: the underffaces, or, upper faces of the two planes as the bow and stem of the ship alternately dip and rise for redueing the pitching motion of the ship and thereby for maintaining theship upon a substantially even keel.

A still further object of the present invention is the provision oi means for limiting angular shifting movement oi the planes upon their pivots.

A still further object of the present invention is to provide means whereby the pressure of water actingupon the stabilizing plane, from below or above, that is during the dip. or rise of a given end of a. ship, would be-capahie-oi angularly shifting the plane upon its pivot for thereby easing thedip or rise motion of theship. and reconditioning oi the planes operation.

Another object of: the present invention is to devise a ship stabilizing plane in such a manner that the resultant force of the water pressure upon the stabilizing. plane added to that of the normal propulsion of the ship. would be generally to a forward direction, thereby reducing any dragof the water upon the plane to a minimum and adding to the elficiency of the ships propulsion.

With the above general objects in view and others that will appear as the invention is better understood, the same consists in the novel construction, combination and arrangement of parts hereinafter more fully described, illustrated in the accompanying drawing and pointed out in the appended claims.

In the drawing forming a part of this application, and in which like designating characters refer to corresponding parts throughout the several views:

FIG. 1 is a top elevational view of a ship illustrating an operative position of the stabilizing planes adjacent the bow and the stem of a ship;

FIG. 2 is a side eievational view of a ship, with the stabilizing planes in an operative position therewith, illustrating in dotted, lines the operation of the planes during the dip of the ships bow;

FIG. 3 is. a fragmentary side elevational view of the mechanism for limiting the angular shifting motion of a stabilizing plane when under the pressureof water, during the dip or rise of either end of the ship;

FIG.- 4 is a top elevational view of the stern of a ship with, a pair of stabilizing planes in an operative position, similar to that of FIG. 1, fiurther-illustrating separate mechanism for each stern plane for limiting angular shifting movement thereof;

FIG. 5 is a diagrammatical view of the bow andstern planes to illustrate the action of the water pressure thereon from faces opposite from those shown in FIG. 2;

FIG. 6 is a graphic illustration of combined force re sulting from the propulsion force of a ship and a water pressure force when acting against the upper face of the plane; and v FIG. 7 is a similar view graphically illustrating the com- 3,004,510 Patented Oct. 17, 1961 2 bined force when the water pressure force upon the plane is from the opposite direction, that is against the lower face of the plane.

Referring to the present drawing in detail there is shown a hip. which includes a hull, 8; bow.- 9, pr w 10 and stem 11. p I

The bow stabilizing p an g n rally ndicated by 12 in FIG, 1, is of generally v-shaped formation and includes forward section 13 and a pair of rearwardly disposed sections 14. Both of saidsectipns 13, and 1.4 are in a spaced relation with bow f the ship. Eaeh side of the stabilizer plane 12, intermediately of the rear ends of the forward section 13 and the front ends of the rearward sections 14, is provided with transverse tubular bearing 15, for reception therewithin of shaft 16, within which-each end of said shaft 16 is rigidly connected. Intermediately, of its. ends shaft 16 is extended'throughprow 10in a transverse relation. It is observed that the rearward. sections 14. of the stabilizer plane '12 have a combined surfaceareacorresponding to about twofthirds. and the forward section 13 to about one-third of the entire area of the stabilizing plane 12, for the purpose which will be later apparent.

The stem stabilizing :plane .is made of a pair oft sections, indicated by 17 in FIG. 1, each, by. its inner edge, in. a spaced relation with the sides. of stern 11 ofthe ship. Eachof said sections. 17 includes forward end 18: and a. rearwardly disposed end 19. lntermediately ofiends 18 and 19 each section 17 isprpyided with a tubular bearing 20, for reception therewithin; of; the ends of shaft 21, whe e na d haf s lihsw n e m di eean l p r ion. t aidslatt-1-irrit ted.- th ough em. 11 nn nans ersere a ionaa atbetqt ar r dw t on 18 e ch, l ne 17. is, b t e i di n as the re rwardly dispo ed en portion 1 9;ot each plane 17 s-abwt; two h r oi he n ea ea-o e chp ne 1.

stabili i g- Planes 12; and17-17 are positioned upon the shin upon a ommonihor z a -pla in a lo g tudinal e a ouw t he sh p, an e owthe tenlevel .2, asis seen in 2.

t s also n tedt at th uter d es. of planes 1. and 17-17 do not extend-outwardly; andbeyondthevertical plane coincidental with the side of hull 8, asis seen in I n ord r t ai pla sm y t ntst e i wharf or dock-23, whentheshipis brought thereto for loa ng ors nloading.

Mounted uponeaeh shait 16;and z1= at its center point, within prow 1,0 and-sternll' respectively, and in,a transverse relation therewith, isbar 24, ina longitudinal relation with theship. Centrally each of said bars 24 may be provided with an annular bearing 25 for accommodating therewithin-each shaft 16 and;2 1, whereineach shaft is keyed or otherwise rigidly afiixed. Supportedvertically-within prow lqand-sternl i asthecase maybe, s. apa po ts t e ps nda whi h dra e path of theends ei her-24, so that one or the other end of ch of'said bars 24, ay l erna ely come ii-c ntac with the end of one or the other of; saidmosts 26, for thereby limiting he ang ar: hit ng. mo ement of-t st b hzmeplanes 2. and 1.7-.+17'. when nder the alternate. water pressure at the upperlor lowenfacesthereof,

all as indicated in FIG, 3-.-

In the modified construction; illustrated-in'FlG; 4 each www.17- of; h t rn-stab zinszplanet s pro d h a separateshaft-zlf. the i ner-end of which rigidly connects with bar 24f, the. angularshifting movement of wh ch is limi d by e, end'sot a p ir o posts. 26'- hu the modi e constructionshownin FIG. 4 cont mplates the water pressure to act independently uponeach of said stabilizing Plane s ctions 17.

Re erring nowtohe. pe at on oi thes bil zer. ho

particularly in FIGS. 2 and 5, it due to the pitching action of the ship brought about by the turbulence of water such as waves, and if it be assumed that the ship bow 9 dips in the direction indicated by an arrow 27 in FIG. 2, then the pressure of water on the lower face of the stabilizing in FIG. 2, with the rear ends 14 of the stabilizing plane elevated and with section 13 of the stabilizing plane in a lowered position, due to the fact that sections 14 of the stabilizing plane are larger in area than the area of the forward section 13.

The dipping of bow 9 influences the ship to make an angular shifting movement about its transverse axis, urging stern 11 to shift upwardly in the direction pointed by arrow 28in FIG. 2. The rising of stem 11 is impeded by the water pressure upon the upper face of the stern stabilizing planes 1717, as is indicated by arrows in FIG. 2 pointing from above and against the upper faces of said stabilizing planes 17-17. As the stern rises, the stabilizing planes 17 will ultimately assume the position indicated by dotted lines in FIG. 2.

That last referred to position of the stabilizing planes 17-17 will be an angularly shifted position with rearwardly disposed ends 19 of the stabilizing planes disposed downwardly and with the forwardly disposed 'ends'18 of the stabilizing planes disposed upwardly. position will result from the greater pressure of water at ends 19 than the water pressure upon the forwardly dispo sedends 18 due to the fact that the reanwardends 19fof the stabilizing planes are larger in 'areathan the area of'the forwardly disposed ends 18.

FIG. shows the reverse action planes when under water pressures atthe time when stern 11 of the ship'dips, as indicated by arrow 29 and the bow of the ship rises, as indicated by arrow 30' in FIG. 5. When the-stern dips the pressureupon stabilizing of the two stabilizing planes 17-17-is from below, thereby alternately bringing the stabilizing planes'17-17 to the position indicated by dotted lines in FIG. 5, with portions 19 disposed upwardly and forward ends 18 disposed downwardly. 'Ihe dipping of the stern due to the pitching of the ship causes the ship to angularly shift about its transverse axis, thereby inducing rising of the bow upwardly in the direction pointed by arrow 30. This in turn brings about an increased pressure of water on the upper face of the stabilizing plane 12, and as the rise of the bow-continues said stabilizing plane will eventually assume an gular position, indicated by dotted lines in FIGJS, with sections 14 disposed in a downward direction and section 13 disposed in an upward direction, due to the area relationship between the two sections, as hereinabove pointed out.

From what has been said it is apparent that the action of the stabilizing planes 12 and 1717 is in an alternate fashion. When a greater degree of pressure at one face of the stabilizing plane at one end of the ship takes place, the greater degree of pressure will beengendered at the opposite face of the stabilizing plane at the opposite end of the ship, and vic'eversal The extent of the angular shifting movement of the stabilizing planes induced by the alternate pressure of water at one or the opposite face of each stabilizing plane due to the pitching motion of the ship must necessarily be limited as otherwise the operation of the stabilizing planes would be ineflicient. Hence the mechanism, best shown in FIG. 3, for limiting the angular shifting movement of each stabilizing plane to one or the opposite direction, brought about by the ends of bars 24 alternately coming in contact with the adjacent upper end of one or the other post 26, as is indicated by dotted lines in FIG. 3. The degree of the angular shifting movement of the stabilin'ng planes may be regulated by either shifting posts 26 to or away from bars 24 or shifting said the stabilizing planes gently due to the fact that the said water pressure has to overcome the normal pressure acting upon the opposite faces of the stabilizing planes. Thus, the action of the stabilizing planes is not abrupt but is cushioned, thereby permitting gradual easing of the ship during its pitching movement.

Although the present invention was primarily designed for the purpose of imparting a degree of stability to the ship by minimizing the extent of the ships pitching movement, the stabilizing planes will 'at the same time act upon the ship in a transverse direction for minimizing the rolling action of the ship due to the action of waves thereon.

FIGS. 6 and 7 graphically illustrate that the combined forces represented by arrows R, resulting from the force of water pressures upon the stabilizing planes, as represented by vector A, and the force of ship propulsion to move the ship forwardly, as represented by vector B, which latter force is in a continuing planar relation with the stabilizing planes, are to a forward direction and substantially parallel to the ships motion.

It is further observed that planes 12 and 1717 could be adapted for use in connection with submersible vessels such as submarines. In connection with such vessels a simple mechanism could be devised to lock the planes in their predetermined angular position in either direction for facilitating diving or surfacing of the vessel.

The stem stabilizing plane 17-17 is preferably made in two separate plates, and not of a homogeneous construction as stabilizing plane 12, for the purpose of effecting space 31 between the ends of sections 19, adjacent their inner edges, for accommodating therewithin a rudder (not shown).

It is to be understood however that the bow stabilizing plane 12 need not be made of a single homogeneous plate, but may be slit at its apex, thereby effecting a pair of stabilizing planes 12, each disposed laterally of the bow 9. The separate planes 12 may be supported upon a single shaft 16, having a single rocking limiting bar 24, as m seen in FIG. 1, or separate shafts, corresponding to shafts 21', shown in FIG. 4, may be employed, with separate bar 24' employed with each separate shaft to limit its rocking movement in either direction.

It is further noted that if the upper end of the rudder does not extend past said planes 17 in an upward direction, then the rearwardly disposed portions 19 of said planes. 17 may be interconnected, thereby eliminating space 31.

From what has been said, it is to be understood that stabilizing planes 12 and 17-17 may be made of homogeneous plates, surrounding, in a spaced relation, the bow and the stern of a ship, respectively, or optionally said planes may be slit upon the vertical plane coincidental with the ships keel to define a pair of laterally disposed planes with relation to the ships bow and stem, respectively. It is therefore to be understood that the reference in this description to the bow and stern stabilizing planes shall include the homogeneously formed stabilizing planes as well as planes formed in two lateral sections.

The increased degree of water pressure resulting from dips and rises of the ships ends upon the respective faces of stabilizing planes 12 and 17-17, as indicated by arrows in FIGS. 2 and 5, not only overcomes the normal water pressure acting upon the planes at the opposite faces thereof, but is also capable of permitting angular shifting movement of the leading ends of said planes in the direction counter to the said increased degree of water pressure. This last result is due to the fact that the rearmost ends of said planes have a greater area than the area of the leading ends thereof. The end result of the action of the increased degree of water pressure upon the stabilizing planes is that the angular shifting movement of the planes, to assume their ultimate angularly shifted positions, indicated by dotted lines in FIGS. 2 and 5, is not abrupt, sudden or jerky, but is gradual, even and smooth, thereby cushioning the dips and rises of the ships ends, while at the same time retarding, diminishing or impeding the extent of the dips and rises of the ships ends.

While there are described herein preferred embodiments of the present invention, it is nevertheless to be understood that minor changes may be made therein without departing from the spirit and scope of the invention as claimed.

What I claim as new is:

1. In a ship having a bow, including a prow, and a stern, a stabilizer comprising a substantially V-shaped planar member in embracing, spaced relation with the bow, a shaft extended through the prow in a transverse relation, the side portions of said planar member being rigidly afiixed to the ends of said. shaft, the rearward end portion of said planar member past said shaft having greater area than the forward end portion of said planar member, a second planar member having portions extending in spaced relation with the sides of the stern, a shaft extended through the stern in a transverse relation, the side portions of said second planar member being rigidly afiixed to the ends of said last named shaft, the rearward end portion of said second planar member past said last named shaft having greater area than the forward end portion thereof, both said planar members being disposed upon a common horizontal plane in a longitudinal relation with the ship and below the Water level, said planar members being capable of angular shifting movement in a vertical direction due to the water pressures thereon resulting from the wave induced motions of the ship, the two shafts being capable of rocking motion imparted thereto by the angular shifting movement of the respective planar members, and means supported within the ship for limiting the rocking motion of said shafts for thereby limiting the angular shifting movement of said planar members in either direction.

2. In a ship having a bow, including a prow, and a stern, a unitary stabilizer having a first portion extending along a side of the bow and forwardly therefrom, a second portion extending along the other side of the bow and forwardly therefrom, said portions defining a V-shaped recess for receiving the bow of the ship therein, a shaft extended through the prow in a transverse relation, said portions adjacent their forward ends being ri idly affixed to the ends of said shaft, the area of said portions rearwardly of said shaft being greater than the area thereof forwardly of said shaft, a second stabilizer comprising a pair of plane sections in a spaced relation with the sides of the stern and extending rearwardly therefrom, a shaft extended through the stern in a transverse relation, said plane sections adjacent their forward ends being rigidly affixed to the ends of said last named shaft, the end portions of said plane sections rearwardly of said last named shaft having greater area than the end portions thereof forwardly of said last named shaft, both pairs of stabilizers being disposed upon a substantially common horizontal plane in a longitudinal relation with the ship and below the water level, the pairs of said stabilizers being capable of alternate angular shifting movement in a vertical direction induced by the alternate increase of water pressure upon one or the opposite faces of each pair of said stabilizers resulting from the alternate dips and rises of the ends of the ship, the two shafts being capable of rocking motion induced by the angular shifting movement of the respective pairs of said stabilizers, and means supported within the ship for limiting the rocking motion of said shafts for thereby limiting the angular shifting movement of each stabilizer in either direction.

3. in a ship having a bow, including a prow, and a. stern, a unitary stabilizer comprising a pair of plane sections in a spaced relation with the sides of the bow and defining a substantially V-shaped recess for receiving the bow therein, a shaft extended through the prow in a transverse relation, said plane sections adjacent their forward ends being rigidly afiixed to the ends of said shaft, the end portions of said plane sections rearwardly of said shaft having greater area than the end portions thereof forwardly of said shaft, a pair of plane sections in a spaced relation with the sides of the stern, a shaft extended through the stern in a transverse relation, said latter plane sections adjacent their forward ends being rigidly affixed to the ends of said last named shaft, the end portions of said last named plane sections rearwardly of said last named shaft having greater area than the end portions thereof forwardly of said last named shaft, both pairs of said plane sections being disposed upon a substantially common horizontal plane in a longitudinal relation with the ship and below the water level, the pairs of said plane sections being capable of alternate angular shifting movement in a vertical direction induced by the alternate increase of water pressure upon one or the opposite faces of each pair of said plane sec tions resulting from the alternate dips and rises of the ends of the ship, the two shafts being capable of rocking motion induced by the angular shifting movement of the respective pairs of said plane sections, a pair of transverse bars each rigidly connected intermediately of its ends with each of said shafts, and a pair of posts supported within the ship in an alined relation with each of said bars, normally the ends of said posts being in a spaced relation with the ends of each of said bars, during the rocking motion of said shafts one or the opposite end of each of said bars being adapted to come in contact with the end of one or the other of said posts for limiting the angular shifting movement of each pair of said plane sections in either direction.

References Cited in the file of this patent UNITED STATES PATENTS 22,097 Vrooman Nov. 16, 1858 1,038,507 Crocco et a1. Sept. 10, 1912 2,223,562 Giliberty Dec. 3, 1940 2,346,337 Stub Apr. 11, 1944 2,520,804 Hollar Aug. 29, 1950 FOREIGN PATENTS 429,170 Great Britain May 22, 1935 326,058 Switzerland Jan. 15, 1958