CA2088361A1 - Power and propulsion system utilizing fluid - Google Patents
Power and propulsion system utilizing fluidInfo
- Publication number
- CA2088361A1 CA2088361A1 CA002088361A CA2088361A CA2088361A1 CA 2088361 A1 CA2088361 A1 CA 2088361A1 CA 002088361 A CA002088361 A CA 002088361A CA 2088361 A CA2088361 A CA 2088361A CA 2088361 A1 CA2088361 A1 CA 2088361A1
- Authority
- CA
- Canada
- Prior art keywords
- fluid
- pipe
- power
- propulsion
- power generating
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03G—SPRING, WEIGHT, INERTIA OR LIKE MOTORS; MECHANICAL-POWER PRODUCING DEVICES OR MECHANISMS, NOT OTHERWISE PROVIDED FOR OR USING ENERGY SOURCES NOT OTHERWISE PROVIDED FOR
- F03G7/00—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for
- F03G7/10—Alleged perpetua mobilia
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01K—STEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
- F01K25/00—Plants or engines characterised by use of special working fluids, not otherwise provided for; Plants operating in closed cycles and not otherwise provided for
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
A system for generating power, buoyancy or propulsion force comprising power generating means and propulsive means. The power obtained by utilizing the compressibility of a fluid passing through a fluid passage is utilized for buoyancy or propulsive system without being influenced by the outside of the bodies of an airplane or ship. Upon being operated by outside electric power, the power generating means continuously produces electric power even when the supply of the outside power is stopped. That is, the self-generating power may be utilized for obtaining buoyancy or propulsion force. The self-operating power generating means may operate continuously by sucking heat from an outside fluid. The electric energy produces a force exerting in one direction within the airtight room of the propulsion means. With this construction, an airplane, vehicle or ship may be safely operated even in an abnormal phenomenon. Furthermore, heat exchanger means may be served as a cooling system.
Description
W092/2t862 PCTJKR92/00020 . l "
3~
PoWER AND PROPULSIGN SYSTEM UTILIZING FLUID
etailed DescriPtion of the Invention This invention relates to a power and a propulsionsyste~s wherein the power is obtained by utilizing t~e `5 compressive force of fluid passing through a fluid passage and the power is applied to a buoyancy or propulsion sYstem without influencing the exterior of the body of an aeroplane or ship.
A power system which is presently used, to propel ` 10 aeroplane, ship or vehicle, is operated by the high-speed ., .~
rotation of an engine which is operated by an oil fuel. For example~ an aeroplane's bodY is propelled by the rotation of jet engine while the buoyancy of the body is obtained by ~1 the lift utilizing the curved airfoil.
In ~e of a ship or a ~ehicle, their bodies are d propelled bY power transfer means which opera~ed by the rotation of engine.
~ The above-described power generating system results in ;~ the consumption of large amounts of energy. Furthermore, 20 the structure of the typical -~Ystem is comple~, causing a frequent breakdown of the system ~nd a rise in the ~ manufacture cost.
;~ In parti ar, a buoyancy sYstem is required to buoy the aeroplane or ship. helicopter and airship are 25 propelled and buoyed by the rotation and curved configuration of the air~oil which contacts directly the ai-r. The propulsion and buoyancy of the helicopter and ~ WO92/2l862 PCT/KR92/00020 `.. ~. ~i 2~88361- 2 -airship are influenced bY such weather conditions as .
irregular air current or difference of air density, thus ` resulting in the abnormal phenomenon which may cause the -- suspension of the operation of the ship or the aeroplane. or a sudden accident.
.' .
Summarv of the Invention . , .
An object of the present invention $S to provide a ; , power system which produces pcwerful and high-speed turning Y -'~j' force utilizing a small quantity of energy.
;,'- 10 Another object of the present invention is to provide ;, a power system which is simple in construction and effective ;, .~
in operation.
Still another object of the present invention is to i~ ~
,,~ provide a propulsion system wherein fluid flows within an ~`~ 15 airtight room and propulsion force is produoe d in one ~ direction, whereby buoyancy or propulsion may be exhibited ...~
-' independently of the outside air.
~'i The invention will be further descri~ed with reference '~ to the accompanying drawin~s.
.
,' 20 Brief DescriPtion of the Drawin~s . .
r;~ FigC. 1 to 3 are schematic views of the present invention;
Fig. 4 shows a power generating system of the prese~t 'i', invention;
Fig. 5 is a side view of magnification ,means in oper,ation;
WO92~21862 PCT/KR92/00020 .- _ 3 '~8~361 . Fig. 6 is an enlarged ~iew of an essential portion in Fig. ~ in operation;
Fig. 7 is a second embodiment of the power generating system of the present i~vention;
Fig. 8 is an enlarged ~iew of an essential portion in . Fig. 7, in operation;
Fig. 9 is a third embodiment of the power generating of the present in~ention;
: Fig. 10 is an enlarged view of an essential portion in 10 Fig 9;
Fig. 11 is a fourth embodiment of the power generating system of the present invention;
.' Fig. 12 is a fifth embodiment of the power generatin~
system of the present in~ention;
:~ 15 Fig. 13 is a sectional view of a portion of Fig. 12;
Fig. 14 is a sixth embodiment of the pcwer generating .
system of the present invention;
Fig. 1~ is a se~enth embodiment of the power generating system of the present inventioni ~`~6 20 Fig.16 shcws compression means of the power generating system of the present invention;
Fig. 17 is a sectional view of a side of Fig. 17;
Fig. 18 shows second embodiment of the compression ~d~ means of the power generating s~stem of the present 25 invention:
~i~ Fig. 19 an enlarged schema~ic view of a section of -.
~' fluid passing pipe of the power generating system of the . .
' ;
.
~ WO92/21862 PCT/~R92/00020 ~ `~088361 - 4 - ~
present invention;
Fig. 20 is a perspective view of a fluid pass~ge ~- dividing pipe of the pcwer gcnerating system of the present inYention;
Fi~. 21 is a sectional view of a heat exchange system e~bodying the present invention;
Fig. 22 is an enlarged view of a portion of Fig. 21;
Figs.23 t~rough 27 are schematic views of a propulsion system of the present invention;
Figs. 28 through 31 are perspective views of a groove of the propulsion system of the present invention;
Fig. 32-A shows the propulsion system of the present invention in operation;
Fig. 32-B shows the propulsion system of the present 15 invention showing another operation state;
~`,i`
~i~ Fig. 33 is an enlarged view of an essential portion of ,. . .
~ ~ Fig. 32 showing the ope~ation of an airfoil with respect to `:.' ;~ an absorption airfoil;
~ Fig. 34 a perspective view of a rotation body of the ,s 20 propulsion system of the present invention, thr rotating ~, body having 8 cut-away portion;
'., .
Fig. 35 a perspective view of a support member of thr ;! propulsion system of the present invention, the support ~ member ~aving a cut-away portion;
,i Fig. 36 is another em~odiment of the propulsion system of the present invention;
;, Fig. 37 is a perspective view of a main buov~ncy .... .
. :
,:
,~
W092/2t862 PCT/KR92/00020 '~ ;, : - 5 - ~1~ 8 8 ~
system of a spiral pipe of Fig. 36 showing the internal structure of the main buoyancy system;
Fig. 38 shows a construction of a wavy patterned spiral pip~ of fig. 36;
. 5 Fig. 39 shows another construction of the wa~y patterned spiral pipe of Fig. 36; .
Fig. 40 shows still another construction of the wavy patterned spiral pipe of Fi~. 36;
Fig. 41 is an enlarged view of a portion of Fig. 37;
Fig. 42 is an enlarged, perspective view of another ` embodiment of 36;
Fig. 43 is an enlarged, perspective view of sti ll , anot~er embodiment of Fig. 36;
i . Fig. 44 is an enlarged, perspective view of another .~ 15 embodiment of Fig. 36;
~ Fig. 4~ is a perspective view of another embodiment of .' the propulsion sYstem of the ~resent invention, the : propulsion system having a cut-away portion;
.~! Fig. 46 is a perspective view of an essential part of 20 Fig 4~;
, Fig. 47 is a perspective view of another embodiment of i~ the fluid passin~ pipe of the pro~ulsion of the present . ~ .
- invention;
.1 Fig. 48 shows an essential part of Fig. 47 in :~ 25 operatio~;
Fig. 49 is a sectional vie.w of the fluid passage pipe . which i5 ~ooled b~ outside fluid;
' ! :
, ~ W092~2l862 PCT/KR92/00020 2~88361 - 6 ' : Fig. 50 is another operation state of the propulsion system of the present invention;
Fig. ~1 is an enlarged view of a cut-away portion of ~` Fig. ~O:
5Fig. 52 is a perspective view of Fig. 51;
Fig. 53 is a perspective view of the spiral fluid passing pipe in another operation of the propulsion system of the present invention;
~1 Fig. 54 is a sectional view of a portion of Fig. ~3;
.~
10~ig. 5~ is a sectional view of a portion of another groo~e construction of the spiral fluid passing pipe of Fig.
~3;
Fig. 56 is a sectional view of a portion of another embodiment of the propulsion system;
'~ 15Fig. 57 is a perspective view of a portion of Fig. ~6;
,~
Fig. ~8 is a perspective view of Fig.~6 with a portion cutted-away;
Fig. ~9 is a perspective ~iew of Fig. ~4 with a , 1 portion cutted-away;
20Fig. 60 is a sectional view of another operation state , ~.
i of the pr~p~ulsion system;
.,~. .
:i Fig. 61 is a sectional view of another operation state of the propulsion systam;
Detailed DescriPtion of the In~ention ~' 25Referring to the drawings, a pcwer ge~erating system 100 is provided with an electric motor M , compression means :~ :
~ 10 which produces feeding force from one to the other , ''' :
W O 92/21862 PC~r/KR92/00020 - 7 ~ 2~S83~
direction, fluic~ velocity increasing means 130 in which fluid velocity is increased at an input side of the means 130 by t~e character of the construction of the fluid pasisa~e and a turbine 140. A propulsion system 200 is - 5 provided with a driving motor M, a rotation body 210. an absorption airfoil Z21, a support body 220 and an enlclosed compartment 2~0.
~ The dri~ing motor M is dri~en by the electric power ; from the pcwer generating system 100. Airfoils 211 are fixed slanted on the periphery of the rotation kody 210 to move fluid ds~nn~ards. The abso~ption airfoil 221 is pro~ided with se~eral minute grooves 222 and mounted on the - support body 220. The groo~es 222 are slanted in the same ; . .
direction as the airfoil 211 of the rotation body 210 and 'î
are provided in the opposite surface of the airfoil Z11.
~l With the grooves 222, the downward flc~ing direction of the ; fluid moved by the rotation of the airfoil 211 is converted . :~ and the compression of the fluid is fluctuated turblently.
~`! Propulsion means is constituted by the airfoils 211 and the ;,~ 20 absorption airfoils 221 and provi~ed in the enc~losed ,~ compartment 2~0 of which upper and 1ower surfaces are .~ enclosed by the support body 220. The fluid in the enclosed ~ compartment 250 has buoyancy or propulsion produced . ~,;
, ,~ji upwar~ 1 y .
~i 25 The power generating system 103 produces power by ~ means of the fluid velocity increasing means 130 which .~ increases fluid ~elocity of the ~luid filled in the fluid ;
...
- ~, .1 : ~ j ~f ~`~`WO92/21862 PCT/KR92/00020 `2~88361 - 8 --pipe I20 by the character of the fluid passage.
Fig. 4 shows a first embodiment of the power ~`generating system lOO wherein the motor M, cc~,pre~sion mea~s 110, fl~id velocity increasin~ means 130 and turbine 140 are ;5 pro~ided at one side of the fluid pipe 120 in which fluid is filled.
~le electric motor M rota-tes the c~mpression means 110 upon being driven.
`~The campression means llO is a centrifugal pump tyFe in which, as shown in the drawings, rotating wings are :,, mounted radially and have a straight or radial type and `guiding wings 112 for turning the fluid which directs directly and induced to an induction port of the center of the pump, t~ward the circumference, minimize the angle with 15 the rotating direction of the rotating wings. When induced, the fluid has the same direction as the fluid in the turbulent compartment 113 at the outside of the rotating wings. With the ab,ove, arran~eme,nt, the fluid is turned at .~ :
the outside of the guiding wings 112, thus producing `20 centrif~,2~l power by which ~c~,pression effect is increased.
With the above-described cc~nstruction, the fluid ~;filled in the interior of the compression means 110 is .. .
compresse,d at the exit *hereof. Whe~n fed by str,,ng feeding force, the fluid is induced to the lnlet of the fluid `' 25 velocity increasing means 130.
The fluid is fed and turned, ha~ing ~n angle Wit21 re~pect ot the th~ ~enter 132. like the direc*ion shown in : .
. ~, ~, . j,. . .
~ W O 92/21862 PC~r/KR92~00020 .
. _ g _ 2~8&361 Fig. 1~. By the centrifugal force of the turning fluid, the - compression of the fluid at the center 132 is lcwer at the'':`
-small- radius location than at the large-radius location of the center 134. and in proportion to the radius to the critical point. With this construction, the compression of the fluid is higher than at the exit of the ~uiding wing 131. The fluid is emitted to the dischar~e port at the state of increased kinetic energy compared with the inlet and drives the turbine 140 to obtain electric energy.
The power to operate the turbine 140 may be obtained by a single fluid velocity increasing means 130. However, to obtain further stronger power, a number of the fluid ; velocity increasing means 130 (In the drawings, three means are shown) are desired to be connected in series. With this arrangement, gradually increasing force is obtained before electric energy i5 obtained. To ~inimize the decrease of ~i~ the effectiveness cau æ d by the difference of the fluid 3`
-~ velocity among each fluid ~elocity increasing means, the ~' fluid pipe at the exit of each fluid velocity increasing ,~
~i20 means is de5ired to ~e made as a straight pipe which is extendible gradually at the sectional area thelc~f.
. - .:
`~The wing of the turbine 140 sre forced to be rotated by the feed of the fluid to obtain electric energy.
The fluid. after having been compressed bY the fluid '25 velocity increasing means and by the turbine 140, is cooled. The fluid is further cooled ~y the repetitlve induction from the -compression means 110 to the fluid W092/2l862 PCT/KR92/00020 : 2088361 velocity incrteasing means 130, whereby the operation of the " system is stopped. To keep the system being operated, a heat-suction pipe 1~1 and a heat exchanger 1~0 are mounted in the middle of the fluid pipe 120 which constitutes a closed circuit.
.~
The heat exchanger 1~0 supplies the outside air to a radiator 152 by a fan 153 and compensate heat for a heat t~ansmitting pipe which transmits heat to the cooled fluid to maintain the normal temperature. With this ar~angement, the interior of the fluid pipe 120 has adequate temperature ` by the radiating pipe.
Accordingly, the power generating system of the pre ænt invention operates smcothly at the no~mal ~ temperature.
; 15 The fluid velocity increasing means has their inlets ~ - ,i. .
and outlets contacted with one nother and increases the fluid as followings.
As shown in Figs. ~ and 6, when flowing through the ` suction port of the fluid velocity increasing means 130 b the compression means 110, the fluid has the direction of ~ the fluid pas~e out of the center of the centripetal axis i , 132 by the guiding wing 131.
AccordinglY the fluid toward ar~und the centrip~tal axis 132 turns around the centripetal axis, thus producing the centrifugal force. By the centrifugal ~orce, the ccmpression of the fluid is low at a small-radius location.
.~
itl Hbwever, to the critical point the larger the radius is, the ... .
,'~,............. .... ... . .
WO92/21862 PCT~KR92/00020 ~ '.
3 ~ 1 .
higher the c~mpression of fluid is.
In the biginning, the compression of fluid is different at a large-radius location by the centrifugal force. The ~irection of fluid which is turning around the centripetal axis 132 at a high-pressure location does not disturb flowing fluid even thcugh the fluid pressure at the high-pressure location is higher than that at the exit of the guidin~ wing 131. The reason is that the oe ntripetal .force corresponding the centrifugal force is formed in the center part, whereby the velocity component acts as ioint `~forces which joins a straight driving component (cen~rifugal force with suction force tcward the center part), and turns.
Accordingly, the kinetic energy of fluid at the exit is greater than that at the suction port, t~ereby producing the kinetic energy of fluid increased over that of fluid pushed by the compression means 130.
,i'The grade of an oblique angle of the fluid of the exit ... .
` ~of the guiding wing 131 with respect to the center is adjusted by the fluid velocity and compression difference between inlet and exit. It should be noted that, when the `~angle is ad~usted, the fluid, when sucked, iS further slanted towards the direction of th~ center as the fluid velocity is the greater. As shown in Fig. 19, to minimize the decrease of the effect caused by the decrease of the Z5 fluid, the fluid pipe at the exit of the compression means I10 is deslred to be made as a straight pipe which has a gradual 1Y increasing section area.
.!
`~WO92/21862 PCT/KR92/00020 ,~,~,, . ~.
~20~8~61 12 The fluid velocity increased as the abo~e-described way drives the turbine 140, thus rotating the motor and the ;compression means 110. The fluid ha~ing its ener~y re-reduoe d is fed to the exit from the suction port of the 5 fluid velocity increasing means 130 to o~tain strong and fast energy and circulated. At this time, the remaining electric energY in the turbine 140 after driving the motor rotates a generator 141, thereby ~eing utilized to operate other electric appliance used for another purpose.
Fig. 1~ shows another fluid ~elocity increasing means ~",`'.:
~-, 130 comprising a number of fluid velocity increasing means elements connected one another, wherein suction port 134 and exit 135 fluid pipe are of cylindrical shape and the guiding wing which is lccated at the exit and directed in 15 the center , converts the fluid flcwing in the center so that the fluid passes around the centripetal axis and then turned toward the axis directi~n naturally.
~, I
Fig. 7 is a second embcdiment of the fluid velocity ~ increasing means 130. The construction of the power -~ 20 generating system in the seoond embodiment oompriæs the i same elements as that of the first embodiment. Hcwever, the ;~ ~ type of the fluid passage in the mean3 130 is different.
A disk-shaped fluid paS~n~e oonverts the fluid flowing in the centripetal direction to a radial direction For 3; 25 this purpose, the disk-shaped fluid pass e has a curved .~3 surface 133 so that the fluid flows perpendicular to the ~i-~ flowing- in ~direction. A guiding wing 131 is mounted in :''~ i W O 92/21862 PC~r/KR92/00020 _ 13 - 208~61 the middle of the curved surface 133 and has the same diameter of the inlet.
The guiding wing 131 is designed in such a manner that the radially discharging fluid is gradually oonverted with a smooth curvature and discharged toward the periphery at one end of the guiding wing.
` The fluid having been compressed initially flows in the inlet of the fluid velocity increasing means 130 and is turned along the radial fluid pas~ee and then discharged to the oulet of the fluid pipe 120. There fter, the direction ;~' of the fluid flowing straightly at the end of the guiding wing 131 is changed by the direction of the i~ner surface of the fluid pipe 120, thereby centrifugal force and force ,. ;;~ , further compressing outward fluid toward the exit are produced, resultin~ in the difference between the compression of the fluid near the center and the centrifugal force acting on the outward fluid. Consequently, the compression at the inlet of the fluid velocity increasing s 130 becomes ~reater than that at the outlet of the means 130, ~hus resultin~ in su~stantial kinetic energy of the fluid. Accordingly, pcwer is obtained by the remaining kinetic energy of the turbine 140.
Fig. 10 is a third em~odiment of the fluid velocity ~, increasing means 130.
~ 25 A U-turn fluid pas~e is added to the outside of the - ~ f luid pas~e of the secone embodiment. A curved surface 133 is provided at the interior of the center. A plurality ,~':@ . , ~.:J
20883'~`1 of guiding wings 131 are spaced and extends radially . The guiding wings 131 are of a curved shape. Inlets and outlets are connected with on~ another. The inlet has two pas~ges and the outlet has a divided two fluid passages. The fluid 5 flcws in the suction port 134 of the center and the suction port 13~ of the outside, r~spectively.
With the tw~ suction ports. the fluid turns from the outside of the cylindrical formation to the circumference, and then makes a U-turn. The oneside of the fluid pip~ 120 10 enclosing the guiding wing has small diameter and the other j~ end has large diameter. With this structure, the diameter ~i increases gradually from the inlet to the outlet, resultir~
.~ :
- in the outlet having a maximul diameter.
Accordingly, the fluid having b~en sucked in the guiding wing 131 flows in the center and then turns toward circumference. Thereafter, the compression at the outside ' increases by the centrifueal force. The velocity component ... .
of the fluid spreads toward the center of the fluid pipe ~-i 120. The velocity component spreaded taward the center is ,~` 20 utilized to turn the fluid at the outlet of the guiding wing ~` 131. Consequently, the fluid at the outlet increases bY the ~'~ centripetal and centrifl~e~l force.
X Fig. 11 shows a third embodiment of the fluid velocity ;~ increasing means 130. The suction port 137 at the outside 5~ 25 is used as a pas~ee through which the fluid is fed by the compressian means 110. The suction por~ 138 of the center is open to the outside. In the suction port- 130 is sucked 'l WO92/21862 PfCT/KR9Y/00020 ~i - 15 - ~ ~8~361 outside fluid ot~er than the fluid flowing in within the ;~ pipe. With this construction, the fluid at the center turns ~ by the influence of the fluid flowing in the inlet 134 and .
the outlet. Whfen the pressure at the center d~creases fy the centriffugal force, the outside fluid is sucked. The same a~.ount of the outside fluid as the amount of the fluid which is sucked in to the center from a portion of the fluid :' pipe of the circulating passage, is discharged. A portion of the circulating inner fluid is discharged and sucked.
`~ 10 With this costructure, the velocity increasing means has . .
~ ` both a closed and an open pf~sage.
. .
y Fig. 12 is a fourth embodiment of the fluid velf~city incr~asing means. As the most different construction, a ladder-shaped fluid pipe is additionally provided. The 15 ladder-~haped pipfe i-~ wcfund spirally and has a gradually .'`."f ~
decreased curved radius. With the ladder-shaped fluid pipe.
the pressure of the fluid passing through the spiral pip~ is ,~
lfowf at center having a small curved radius, and the pressure ~ f ~ of the fluid flowlng near an outside wall 161 is high. As .;
t,'j' 20 the curved radius of the outer waIl of the spiral pipe "f dec~eases ff~radually, the adjacently flf~wing fluid pr~vifdes biased forc~ tow2rd the center with a portion of the ouside fluid, b~ a collision with an outer surf~ce of the spiral pipe.
WiW~ the ~iased force, the centripetal force is strengthened. The strengthened centriFeta1 fo~ce increases ''i ' -~, the velocity of th~ fluid. As the length of the inner wal-l .,~
~. : , . - , .
, 20~3~1 - 16 or center axis and the outer wall 161 of the spiral pipe gradually lengthened, the biased force tcward the flowing direction of the fluid is strengthened and the velocity of the fluid further increases since greater biased force is formed around t}le center axis.
As shcwn in Fig. 12, when the spirally e~tending center axis at the outlet is thicker than other portion, only the hi~-pressure fluid at the outside is discharged, thus obtaining stronger kinetic energy.
10 It is desired that the spiral pipe 160 be gradually, upwardly lengthened at the outer wall 161 and inner wall ~ .
and an interior angle between the bottom face of the fluid pipe and the outer wall be uniform.
;~ With the le~gtll of the outer wall 161 which is ~.
` 1~ maintained toward the oulet, same effect may be obtained e~en the sectional area of the fluid passage decreases gradually toward the outlet. As shown in fig. 14, the fiuid pipe may have a square shape in-its cross-section.
J Fig. 13 is a cross-section of the spiral pipe 120 20 having a cut-away portion. The spiral pip~ 120 is wound upwardly, spirally.
x Figs. 16 and 17 shc~s the compression means of the . ~ . ',f~
power generating system. The compression means i5 provided ~, with a fluid pipe having the same construction as the velocity increasing means. At the outside of the guidin ~ wing 112 of the fluid pip~ is provided a plurality of '" :'~, ';
~ ~radial~y extending straight and short rotatable wings 111.
'~.; ' ~
;1 W092/2t862 PCT/KR92/00020 ~ .
- 17 - 2~8~61 ; Wlth this arrangement. the sngle when the fluid at the outlet is turned and sucked conforms with the rotation direction. The construction of the rotatable wing is j - similar to that of the radial-winged centrlfugal fluid duct.
However, the rotatable wing is short and narr~w upper and lower ends. The effect of the compression system further increases since the direction of the fluid sucked in the rotatable wing conforms with the direction of the rotatable wing. Further, the pressure at the outlet increases by the centrifugal force of the turning fluid.
Fig. 18 shcws another embodiment of the compressicn means wherein the suction port 139 is provided at the both sides of the axial direction.
Fig. 10 shows a fluid p~se~ee dividing pipe whioh is lS provided at a location at which the section of the fluid passage of the suction port decreases of the fluid velocitY
~ increasing means of the pcwer generating system. The fluid ~ ,;,! p2ssage dividing pipe is provided with a plurality of coaxial cylindrical fluid pipes of which leading end is , 20 thick and rear end is thin. With the coaxial cylindrical pipes, the fluid from a large-sectioned location of the . . .
fluid pipe is sucked uniformly over the~ who~e s~ction of the b!~',i fluid pipe. The section of the fluid pipe between the fluid dividing pipes i5 greatly decreased at the leading end. To the rear end, the fluid pipe has a uniform section or a section of small reduction rate. It is noted that the pipe has any configuration at its section, such as square or oval . ~ .
~ ~3 j ~
: W O 92t21862 PC~r/KR92/00020 20883~I 18 shape. The heat exchange system 150 exchanges the fluid of ordinarY temperature with the inner f 1 Uid by means of heat and supply heat to the inner fluid. The heat exchange system compri æ s a fan 153, a r diator 152 which is 5 connected to a heat sucking pipe 1~1 and a compressor. With ~, .
the heat exchange system, the over heat of the f luid circulatin~ the interior of the fluid pipe is prevented.
-~ resulting in the smooth operation.
Fig. 21 shows the heat exchange system 270 to 10 compensate heat for the interior of the system by absorbing the heat of the nor~al temperature of the outside of the `~ system. With the heat exchange system 270, the freezing of ,, .~
~ the moisture in the air by the absorption of the heat of the r, ,.~ I .
' air, is pre~ented.
In detail, the freezing of the heat exchange system . .
270 is prevented by the follcwing repetitive process. that , is, a water-soluble antifreezing solution flows in the interior of the radiatGr and then is raiæ d along a guiding pipe to the circulating system consisted of a pump.
~ .
~ 20 When the antifreezing solution beoomes lcw in its f .~ concentration the æolution passes through the fluid pipe in ~ a d~y ta~ which is provided with curve(~ radiating pins and } Y then is heated by a heater Z77 under the fluid pipe, whereby the air in the upper space of the dry tank is 25 discharged ~ a vacuum pump 279, resulting in the interior . -,i "~ of the dry tank 276 being made vacuous. Consequently, the solution is returned to a moisture-evaporated ordinary .. ... .
~ ','1 ' ` ~, 9 - ~08~361 solution, thus permitting a repetitive use of the antifreezing solution.
The heat exchange system 270 heat cool air of the interior of the propulsion system 200. With this ~ 5 construction, the heat exchange system 270 supply heat to - the outside ~eat sucking pipe 272 by means of a fan 271 which is located at one end of the radiator 273 w~lile-cooling some obiects by the cool air from t~e heat suction pipe 272. As described above, the heat exchange system 270 10 may be utilized as a cool system such as air conditioner or . . .
~ a refrigerator.
.. , : -`Fig. 1 shows the fluid velocity increasing means of the power generating system 100 wherein the press~re of the ~ fluid increases by the centripetal force. Fig. 2 and 3 show :~15 spiral piped fluid pascAge of the fluid velocity increasing ;3 ~;~system and the po~er generating system utilizing centrifugal force, respectiti~ely.
In the propulsion system 200 the pressure is produoe d to one side according to the flowing direction of the fluid ;~20 and the pressure is absorbed in the other direotion. The . ,.. ~ .
i~difference between the produced and absorbed pressure results in producing b~yancy or propulsion.
Fi~. 32 is a *irst embodi~ent of the enclosed propulsion system 200, wherein the dri~ing motor M is 25 rotated by electric energy obtained fro~ the pawer generating sYStem 100. thus rotating the rotatable body of cylindrical shape which is open at its upper and lower ends.
,~ '' ~, !-;
:, .,' WO92/21862 PCT/KR~2/00020 2~ 88 3 6 1 - 20 The rotatable W 210 has slanted, multi-stepped, ccoperable wings 211 on the periphery thereof. Each of the wings 211 is wide and should be mounted in such a manner that the angie between rotation direction and the wing is small.
The suppo~t W 220 consists of upper and lcw~ir surfaces 223, 224 and side surfaces to tightly close the ,;: rotatable body 210 and wings 211. The support W 220 has wings on the inner face fixed thereto which are crisscross with and have the isame slanted direction as the wings 211 of the rotatable body 210.
-; As shown in fig. 13, the wing 221 has minute grooves 222 in the upper face thereof to increase the area on which, when the fluid containing air or liquid flows dbwn~rdly~
5 the fluid acts, and to decrease the downwardly acting :` pressure by the turbulent fluid in the minute groo~es 222.
"
Accordingly, the wings 211 rotated by the driving ~- motor feeds downwardly the fluid filled in the support W
;~ 220. Furthermore, the ~uoyanCY to lift the wings 211 :
:1 20 together with the rotata~le body 210. In summary, The ~y ' phenomenon arises at every location at which thei wings 211 ~ and the crisscross absorption wing 221 rotate fast. The .~ bu~YancY force obtained at this time is united to be served as strong propulsion force or buoyancy.
Th~ fluid moves downwardly by the rotation of the ,5X, wings 211. The support body 220 has absorption grooves 225 ;~
~i ~ in the -lower sur*ace 224 theireof having the same "~
. .~, .
.
,i , - ~ . ..... , . -- -, . ; - - - - . . . . . .. .. . ..
' . ' ', ,;: ' ` ' ' ` ' ' ".': -' ''. : ' ' ' '. ` . ` '': - ' ' - :- ' ' ' ' .`.: :
.~ . .
~ . i configuration and construction as the minute gr~oves 222 in the wings 211~ With this arrangement, the upwardly pressure by the fluid acts strongly further than the downwardly pressure, thus obtaining more stronger buoyancy.
Th~? distal absorption wing 221' and other absorption wings 221 are mounted at different angle so that the fluid flows in the center in slightly deflected dir~ction. With-this arran~ement, additional effect of the increase of the pressure of t~e upwardlY f luid frvm the center, is obtained by the same theory as in the fir~t embodiment of the fluid increasing means of the p~wer generating system to produce the centrifugal force of thie fluid flowing toward the center to adjust the direction of the fluid flowing through the center. In addition, the diameter of the bearing-supporting location at the upp~r portion is larger than the center, therebv on]~ high-pressure fluid havirg large turning radius is disc}~rged and turned at the upper portion. As the upper and lo~er width of th~ fluid passage of the :?
~ ; uppermost part of the upper being narro~, the pressure at . ~
~^~i 20 th~? upper surface is higher than that at the lcwer surface, thus increasing the buoyarcy further.
With the difference of the pressure acting on the upper part and the lower part by the m?ovement of the fluid, ~ buoyancy or propulsion force from the airti~ht interior to i 25 one direction is obtained. The buoyancy or propulsion force ' ,?
is used for ships or air~lanes.
~ 1n case the ab~v~-described systems of the sa~ ~ number ....
",: . - ~. . : : . , W O 92/21862 PC~r/KR92/00020 20 8~3 6 ~ ~ 22 are mounted at both sides of and spaced equally from the center line of the airplanes or ships, respectively~ the bodies of the airplanes or ships are lifted and balanced.
Furthermore, if the systems are mounted at the leading or rear end of the bodies with the lengthwise axis being ; parallel with the floor, the bodies are propelled toward the ~ direction perpendicular to the byoyancy acting direction.
~; If the syste~s are mounted at the surface parallel to the direction intended to propel with the lengthwise axis bein~
parallel with the floor, the bodies are turned from side to ;^- side.
, .
As being provided within the airtight room, the , systems are rarely influenced by weather change or a ; ~ treacherous air current such as a storm, or the change of i5 the air density, resulting in normal operation. Futhermore.
',. an airplane can he taken off and landed perpendicularly ~ without using a runway.
'.`,J In case the the above-de æ ribed system is used as a buoyancy sYstem, an outside body 230 is fixed to the outer surface of the sYstem to prevent overheat which may be .Y~ .
~; caused by the movement of the fluid. The outer body 230 is - ~; open at its upper and bottom surfaces. With the r3t tion of the rotatable bcx~y 210, the outside fluid flows along the i outer surface of the support ~ody 220, thus bringing oil cooling or air cooling . Conversely, in case the abov~-described system is u~ed as propulsion system, the fluid within the airtight room is apt to be cooled. To ~''~ ' ,,.~
. . ~ . .
.~ . .
- 23 - 2~8836~
`~ prevent the cooling, heat maY ~e supplied to the interior fluid from the outside fluid.
It is desired that the fluid in the airtight roo~ 2~0 have uniform pressur~ and the uniform pressure be exerted on the interior of the airtight room 2~0. Even not shown in the - drawings, an extra fluid reservoir and pressure control de~ice comprising a pressure sensor and a suction or discharging pump are desired to be mounted at a suitable location out of t~e airtight room 250.
`~ 10 The pressure control device comprises a rotatable b~dY
210 and a support body 220 which are rota~ed respec~ively.
. . .
With this construction, to rotate the rotatable b~dy 210, ~ the center bottom of the rotating axis 212 of the rotatable ',,`;,`:! body 210 communicates with the interior of the airtight room 250 so that a pressure is controlled by the inooming and ,.`~`7 outgoing of the interior fluid in respect to pressure ~: .
control tube and the airtight room 250 through an opening in ,;~`s the rotating axis 212.
~ Fig. 32-B, a generator is mounted on the rotating axis ~ `.
~ ~ 20 212 of an outer wing Z11 on which an absorption wing 221 of ,. ......................................... .
the propulsion system is mo~nted. With this arrangement, an electric power is obtained by the power produced by the rotation of the absorption wing 221. Furthermore, the rotatable body 210 on which is mounted the absorption wing -25 221 may be fixed and not rotated to serve only as a guiding ..
wing.
, ~The support kody 220 is dri~en thrcugh transfer mans W092/2tX62 PCT/KR92/00020 2~ ~8 36'l ~ 24 mounted at the dri~ing motor. To increase the effect of the propulsion system 200, simultaneous with the driving of the rotatable body 210 ~nd its fixed wing 211, the absorption wing 220 facing the wing 211 is driven in the same direction as the fixed wing 211.
The power transfer means 240 comprises a rotatable ~ axis 212 and a pluralitY of gears engaging with one another - and ~eing mounted on the bot ~ n face of the support body ^ 220. With this construction, the rotation force is 10 respectively transferred to the rotatable body 210 and the support body 220. A different deduction rate may be obtained depending ~n the number and diameter of the teeth of the gears 241. With the deduction rate, the velccity of the rotatable wing is faster than that of the support bodY
15 of the absorption wing 221. Hbwe~er. it is desired that the ~' absorption wing 221 and the rotatable wing have ,~ comparatively fast velocity.
It is within the scope of the present in~ention that ., .
~ ' the minute grooves 222 and absorption grooves 225 have anY
.,~, .
,, 20 shape or configuration so long as the groove~ 222 nd 225 `~ are able to form turbulent flow when contaced with the ~, fluid. That is, the minute grooves 222 and 225 have a ~î'l hemispherical or semicylindrical shape, and a partitioned semicylindrial or slanted double surface type.
~ ~ .
' 25 To increase the effect of absorption, another minute .~ .
;~ grooves may be pro~ided on the surfaces of the ~inute ~, grooves 222 and absorption grooves 225, thu~ constituting : ~, `;
, `` - 25 - 2088361 double grooves.
It is desired that a guidin~ member 231 be mounted at an upper end of the outer body Z30 so that the outside fluid has lcw flu~d resistance and be suc~ed smoothly. ~ach 5 bearing to deduce friction resistance is mounted a lo~ation at which the support body 220 and the rotatable body 210 contact wit}- each other and support the rotation thereof .
Fig. 36 shows a third embodiment of the propulsion system Z00 wherein the spiral fluid pipe 260 and compression 10 means 280 provide buoyancy or propulsion force c~used when ;~.-the fluid is forcedlY and wavely fed within the airtight ; ~pipe and then directed upwardlY.
......
. .~A semispherical or semicYlindrical-shaped groo~es are :,.closely provided on the bottom face 262 of the fluid pipe ~.15 120 of wavy shape. The fluid flc~/s along the wavy-shaped pipe 120. The pressure exerting on the bottom face by the .~1ower fluid pas~A~i~ is decreased by the grooves 263. The .-J
. ~upper and lower width of the fluid passa~e of the center of : ::the upper fluid pass~e is nar.rowed to exert the pressure on ~;~:20 the upper part strongly, whereby buoyancy or propulsion ~force of the bodies of the airplane or ship is obtair~d bY
a united force. Further.~ore, the compression force by the fluid in the spiral pipe is further obtained, thus increasing the fluid velooity, w~ereby greater buoyancy is 25 n~ditionally obtained.
At this time, for the continuous feedir~ of the fluid ~...
~ ~. in compre~sion, compression mean5 having similar ~ WO92/21862 PCT~KR92/00020 i construction as the centrifugal pump and thus having feeding force by the rotation of the 40.
In Figs. 38, 39 and 40, a semispherical or ~,` semicylinderical groo~e 266 is provided in the lowermost location amon~ the locations at which wavy curved faoe s are formed. With this arrangement, when the fluid is fed . ~
~-forcedly, the pressure exerting on the bottom of the fluid ::;
passage by the d~wnwardly flowing fluid, is absorbed or ~ortexed by the grooves 266, whereby upward1y buoyancy or ,.
,.
~`~10 propulsion force is increased. It is within the scope of ~ the present invention that the grooves 266 have any curved !~
configuration such as a semispherical or semicylindrical or slanted double faced or similar curved shapes.
In Figs. 41, 42 and 43, wavy, curved formation is ; ~15 provided on the bottom 262 of the interior of the spiral pipe 120, wherein the grcoves 266 are formed in the lcwer portion and the width of the upper and lG~er portion of the fluid passage i5 gradually narrowed at the uppermost , ,iportion, whereby a turbulent flow by the ~urved turning j, ~A'~
~20 portion of the upper fluid pasC~e is prevented and strong .'.'1 ;` ~pressure is exerted on the upper surface , resulting in the ,;, ~:: f~ production of the upward buoyancy.
, . . .
~The effect by the wave is different according to the ... .
size of the width of the upper and lower part of the fluid ~25 passage and distance between the pitch of the wavy curved -~formation. It is desired that the distance and size be ~adjusted most efficiently.
. .
~ ' .
2~8~3 Fig. 45 is a fifth emb3diment of the propulsion system 200 of the present invention. A slanted double face groove Z62 is formed on the bottom and upper faces of a long fluid pipe. The iong fluid pipe is w~und spirally by the same ~ S manner of the fourth embodiment of the pcwer generating ;- system as shcwn in Fig. 12. With this arrangement, the forced feeding of the fluid by the compression means 130 -~ tcward to the spiral fluid pipe 120 results in the ; difference of the pressure between the upper ~ace and the bottom face by the turbulent flcw of the fluid in the . ."
slanted double face groove~ and by the difference of the surface area. ~hat is, an upwardly pressure is increased ,~ by the fluid at the upper surface and a downwardly pressure is decreased at the b~ttom surface, resulting in the . .
~ 15 production of the buoyancy. The effect is further increased , ;j, in that the effect of t~ compression of the fluid is additionally obtained.
The direction of a location having a large slope angle ,~ at the bottom surf~ '? of the slanted double face OErcove is .. , ii - .
~ 20 same as the direct.on in which fluid meets. The upper '~
~,` surface of the slanted double face groove is formed by a ~, manner in contrast with the above~ scribed m~nner. The ':' ' ~i .
;~ fluid pipe has a square or ladder 3hape in its section causing the upper and lower walls of the fluid pipe to be ,~J 25 graduallY distant and the section of the fluid pasæage to be ., :
uniformly maintained or graduallY enlarged.
In one surface having a large angle of the slanted ~
. :~,....................................................................... .
,,~
W092/2~862 PCTiKR92/00020 f~, 2088361 28 - `'-~
double face groove may be provided with a doub~e groove of semispherical or semicylindrical shape. The uppermost and lowermost of the slanted face are rounded.
Fig. 47 is a sixth embodiment of the spiral fluid pipe 5 of the propulsion system wherein a semicylindrical fluid pipe is spiral 1Y wcunded and has a semicircular ~ottom of continuous wheel shape having a negative curved rate and having a comparati~elY long center line at one direction. A
groo~e is provided in the bottom of which both sides have a 10 small curved radius to produce buoyancy by the fluid flowing along the spiral formation. While the fluid flows through the semicYlindrical spiral fluid p csage and circulates through the upper and lower fluid pass es, the groove formed in the bottom face of the fluid pipe having small 15 curved radius both si~es lowers a downward pressure . With the construction of the tw~ upper fluid passages wherein the upper and lower width of the fluid passage of the upper fluid passage gradually narrows, resulting in the uppermost portion having a minimum width.
In Fig. 49, an outer body 230 enclosed the outer sur~ace of t~e spiral fluid pipe 260 and a fluid duct 290 is mounted at the upper portion of the pipe 260, the fluid duct 290 bein~ served to move an outer fluid upwardly or downwardly. With this arrangement. the airtight interior 25 fluid maY be cooled or heated by the outer fluid. It is desired that the outer surface of the s~iral pipe have a -large area ~or good heat tr~nsmission.
~ :
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- 29 - 2~8836~
Fig. ~0 is a seventh embodiment of the propulsion system wherein an airtight ro~m 250 has a circular shape in cross-~ection and a wing member 268 is mounted radially to serve as a guiding win~ of the centrifugal fluid duct and slantedly toward the rotation direction of the rotatable body 210. When the rotatable body 210 is rotated, the interior fluid circulates by the wing member 268 and the buoyancy is exerted on the wing member. The buoyancy effect may be obtained by the pressure decrease at the bottom face of the grooves 269.
In this construction, the absorbing groove 225 is provided in the lower surface 224 of the support body 220, an upward pressure is exerted on the unseen face of the rotatable wing 221, the upper and lower fluid width of the upper part graduallY decreases resulting in the minimum width of the uppermost part and the rotation of the rotatable body is performed by the driving motor M.
Fi~s. 53 and ~4 are eighth embodiment of the propulsion system 200 of the pre æ nt invention, wherein an absorbing groove 266 is formed in the i~ner bottom-262 of the spiral fluid pipe 260. the width of the fluid pas~ge of the upper fluid passage gradual~y narrows resulting in the minimum width of the uppermost par~ ~00. With thic arrangement, an upward buoyancy or propulsion force may be obtained by the difference of the pressure exerting on the upper and bottom faces.
As shcwn in Fig. ~, a ~roo~e has a slanted double :.
faces and the slanted groove in the bottom of the lcwer fluid passage and the upper face of the upper fluid passage is directed oppositelY, at the bottom of the lcwer fluid passa~e and the upper face of the upper fluid passAee.
Fig. ~6 is an ninth embodiment of the propulsion system., wherein disk-shaped members 216 of multistage shape are repetitivelY mounted on the rotatable body 210 and a slanted double face groove 262 is formed in the upper or lcwer face thereof to obtain buoyancy or propulsion force at one side thereof. One of the slanted faces has a small angle and the other slanted face has a large angle. The large angled face 262 is directed to the rotation direction and the lcwer face is directed oppositely.
Cutoff bars 264 are provided crisscross with one i5 another between the rotatable disk-shaped members provided at each end of the fluid passage to prevent the movement of . . .
the fluid toward the rotation direction of the rotatble disks, thus increasing buoyancy. For easy cutoff and passing of the fluid at the same time , the cutoff bar has a negative curvature at the side ther~of. The rotatable dislcs may have a cone shape or its inver~e shape.
To prevent sudden rise or fall of the temperature of the inner fluid of the above-described propulsion or b~oyancy system, the heat exchange system 150 may be mounted . . .
at one side of the fluid pipe. Otherwise, the fluid is cooled bY the outer f luid from the outside of the system.
Though not shown in the drawings, the outer f luid f ~ c~
': ', .
- 31 - 2~883~1 throu~ a pipe which is connec~ed ~o the inner fluid. A
pressure control tank provided with a pressure sensor and a suction and discharging pump is provided at the outside of the system to control the pressure of the inner fluid uniformly.
Fig. 23 shows a connection of the fluid which acts is vortexed in the minute grooves of the propulsion system 200 and acts at one side. Fig. 24 is an enlarged view which sh~ws a double groove construction wherein a plurality of 10 another minute groo~es sre sdditioned to the surface of the minute grooves to increase the effect of the propulsion system 200. Fig. 2~ shows the slanted double face groove is formed in the surface of the upper and lower part of the fluid pipes snd Fig. 26 shows another grooves or semispherical or semicylindric~l ~- w ve~ sre sdditioned to the surface of the slanted double fsce groove to effect the effect of the system.
Fig. Z7 shows a connction of the rotatsble body 210 of the propulsion system 200 with the support body 220 wherein 20 the distance ketween upper and lower f`ace of the center of the upper part of the airtight room 2~0 is shortest and the absorption grooves 22~ are pro~ided in the lower faoe, resulting in the difference of the pressure so that buoyancy or propulsion force is produced.
In summary, the power generating system is operated by an ~lectric pow~r from outside. In case the supply of the outside power is interrupted, self-generating power is-.
W O 92/21862 PC~r/KR92/00020 ',..
~ - 32 ~1~88361 produced, thereby buoYancY or propulsion force to operate bodies of airplanes or ships is produ oe d. The power generatir~ system absorbes heat from the outside fluid and operates by the self-generating power. By this electric S energy, one-side directed po~er is pro~uoe d in the interior of the propulsion system. thus producing buoyancy or propulsion system. With the present invention, airplanes, ~ehicle or ships may be operated pr~perly even in a~normal atmospheric phenomena. Furthernore, to obtain the po~er generating system and propulsion or buoyancy generating sYstem maY be combined for suitable use or purpose.
Otherwise, only the power generating system is utilized to operate an electric ~ehicle or industrial or home implements. The heat exchanger is utilized as cooling apparatus The forgoing detailed description has been given for clearness of understanding only, and no unnecessary limitations should be understood therefrom, as some clodlfi~tions wi 1 l bs obvious to those ski l led in the rt.
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3~
PoWER AND PROPULSIGN SYSTEM UTILIZING FLUID
etailed DescriPtion of the Invention This invention relates to a power and a propulsionsyste~s wherein the power is obtained by utilizing t~e `5 compressive force of fluid passing through a fluid passage and the power is applied to a buoyancy or propulsion sYstem without influencing the exterior of the body of an aeroplane or ship.
A power system which is presently used, to propel ` 10 aeroplane, ship or vehicle, is operated by the high-speed ., .~
rotation of an engine which is operated by an oil fuel. For example~ an aeroplane's bodY is propelled by the rotation of jet engine while the buoyancy of the body is obtained by ~1 the lift utilizing the curved airfoil.
In ~e of a ship or a ~ehicle, their bodies are d propelled bY power transfer means which opera~ed by the rotation of engine.
~ The above-described power generating system results in ;~ the consumption of large amounts of energy. Furthermore, 20 the structure of the typical -~Ystem is comple~, causing a frequent breakdown of the system ~nd a rise in the ~ manufacture cost.
;~ In parti ar, a buoyancy sYstem is required to buoy the aeroplane or ship. helicopter and airship are 25 propelled and buoyed by the rotation and curved configuration of the air~oil which contacts directly the ai-r. The propulsion and buoyancy of the helicopter and ~ WO92/2l862 PCT/KR92/00020 `.. ~. ~i 2~88361- 2 -airship are influenced bY such weather conditions as .
irregular air current or difference of air density, thus ` resulting in the abnormal phenomenon which may cause the -- suspension of the operation of the ship or the aeroplane. or a sudden accident.
.' .
Summarv of the Invention . , .
An object of the present invention $S to provide a ; , power system which produces pcwerful and high-speed turning Y -'~j' force utilizing a small quantity of energy.
;,'- 10 Another object of the present invention is to provide ;, a power system which is simple in construction and effective ;, .~
in operation.
Still another object of the present invention is to i~ ~
,,~ provide a propulsion system wherein fluid flows within an ~`~ 15 airtight room and propulsion force is produoe d in one ~ direction, whereby buoyancy or propulsion may be exhibited ...~
-' independently of the outside air.
~'i The invention will be further descri~ed with reference '~ to the accompanying drawin~s.
.
,' 20 Brief DescriPtion of the Drawin~s . .
r;~ FigC. 1 to 3 are schematic views of the present invention;
Fig. 4 shows a power generating system of the prese~t 'i', invention;
Fig. 5 is a side view of magnification ,means in oper,ation;
WO92~21862 PCT/KR92/00020 .- _ 3 '~8~361 . Fig. 6 is an enlarged ~iew of an essential portion in Fig. ~ in operation;
Fig. 7 is a second embodiment of the power generating system of the present i~vention;
Fig. 8 is an enlarged ~iew of an essential portion in . Fig. 7, in operation;
Fig. 9 is a third embodiment of the power generating of the present in~ention;
: Fig. 10 is an enlarged view of an essential portion in 10 Fig 9;
Fig. 11 is a fourth embodiment of the power generating system of the present invention;
.' Fig. 12 is a fifth embodiment of the power generatin~
system of the present in~ention;
:~ 15 Fig. 13 is a sectional view of a portion of Fig. 12;
Fig. 14 is a sixth embodiment of the pcwer generating .
system of the present invention;
Fig. 1~ is a se~enth embodiment of the power generating system of the present inventioni ~`~6 20 Fig.16 shcws compression means of the power generating system of the present invention;
Fig. 17 is a sectional view of a side of Fig. 17;
Fig. 18 shows second embodiment of the compression ~d~ means of the power generating s~stem of the present 25 invention:
~i~ Fig. 19 an enlarged schema~ic view of a section of -.
~' fluid passing pipe of the power generating system of the . .
' ;
.
~ WO92/21862 PCT/~R92/00020 ~ `~088361 - 4 - ~
present invention;
Fig. 20 is a perspective view of a fluid pass~ge ~- dividing pipe of the pcwer gcnerating system of the present inYention;
Fi~. 21 is a sectional view of a heat exchange system e~bodying the present invention;
Fig. 22 is an enlarged view of a portion of Fig. 21;
Figs.23 t~rough 27 are schematic views of a propulsion system of the present invention;
Figs. 28 through 31 are perspective views of a groove of the propulsion system of the present invention;
Fig. 32-A shows the propulsion system of the present invention in operation;
Fig. 32-B shows the propulsion system of the present 15 invention showing another operation state;
~`,i`
~i~ Fig. 33 is an enlarged view of an essential portion of ,. . .
~ ~ Fig. 32 showing the ope~ation of an airfoil with respect to `:.' ;~ an absorption airfoil;
~ Fig. 34 a perspective view of a rotation body of the ,s 20 propulsion system of the present invention, thr rotating ~, body having 8 cut-away portion;
'., .
Fig. 35 a perspective view of a support member of thr ;! propulsion system of the present invention, the support ~ member ~aving a cut-away portion;
,i Fig. 36 is another em~odiment of the propulsion system of the present invention;
;, Fig. 37 is a perspective view of a main buov~ncy .... .
. :
,:
,~
W092/2t862 PCT/KR92/00020 '~ ;, : - 5 - ~1~ 8 8 ~
system of a spiral pipe of Fig. 36 showing the internal structure of the main buoyancy system;
Fig. 38 shows a construction of a wavy patterned spiral pip~ of fig. 36;
. 5 Fig. 39 shows another construction of the wa~y patterned spiral pipe of Fig. 36; .
Fig. 40 shows still another construction of the wavy patterned spiral pipe of Fi~. 36;
Fig. 41 is an enlarged view of a portion of Fig. 37;
Fig. 42 is an enlarged, perspective view of another ` embodiment of 36;
Fig. 43 is an enlarged, perspective view of sti ll , anot~er embodiment of Fig. 36;
i . Fig. 44 is an enlarged, perspective view of another .~ 15 embodiment of Fig. 36;
~ Fig. 4~ is a perspective view of another embodiment of .' the propulsion sYstem of the ~resent invention, the : propulsion system having a cut-away portion;
.~! Fig. 46 is a perspective view of an essential part of 20 Fig 4~;
, Fig. 47 is a perspective view of another embodiment of i~ the fluid passin~ pipe of the pro~ulsion of the present . ~ .
- invention;
.1 Fig. 48 shows an essential part of Fig. 47 in :~ 25 operatio~;
Fig. 49 is a sectional vie.w of the fluid passage pipe . which i5 ~ooled b~ outside fluid;
' ! :
, ~ W092~2l862 PCT/KR92/00020 2~88361 - 6 ' : Fig. 50 is another operation state of the propulsion system of the present invention;
Fig. ~1 is an enlarged view of a cut-away portion of ~` Fig. ~O:
5Fig. 52 is a perspective view of Fig. 51;
Fig. 53 is a perspective view of the spiral fluid passing pipe in another operation of the propulsion system of the present invention;
~1 Fig. 54 is a sectional view of a portion of Fig. ~3;
.~
10~ig. 5~ is a sectional view of a portion of another groo~e construction of the spiral fluid passing pipe of Fig.
~3;
Fig. 56 is a sectional view of a portion of another embodiment of the propulsion system;
'~ 15Fig. 57 is a perspective view of a portion of Fig. ~6;
,~
Fig. ~8 is a perspective view of Fig.~6 with a portion cutted-away;
Fig. ~9 is a perspective ~iew of Fig. ~4 with a , 1 portion cutted-away;
20Fig. 60 is a sectional view of another operation state , ~.
i of the pr~p~ulsion system;
.,~. .
:i Fig. 61 is a sectional view of another operation state of the propulsion systam;
Detailed DescriPtion of the In~ention ~' 25Referring to the drawings, a pcwer ge~erating system 100 is provided with an electric motor M , compression means :~ :
~ 10 which produces feeding force from one to the other , ''' :
W O 92/21862 PC~r/KR92/00020 - 7 ~ 2~S83~
direction, fluic~ velocity increasing means 130 in which fluid velocity is increased at an input side of the means 130 by t~e character of the construction of the fluid pasisa~e and a turbine 140. A propulsion system 200 is - 5 provided with a driving motor M, a rotation body 210. an absorption airfoil Z21, a support body 220 and an enlclosed compartment 2~0.
~ The dri~ing motor M is dri~en by the electric power ; from the pcwer generating system 100. Airfoils 211 are fixed slanted on the periphery of the rotation kody 210 to move fluid ds~nn~ards. The abso~ption airfoil 221 is pro~ided with se~eral minute grooves 222 and mounted on the - support body 220. The groo~es 222 are slanted in the same ; . .
direction as the airfoil 211 of the rotation body 210 and 'î
are provided in the opposite surface of the airfoil Z11.
~l With the grooves 222, the downward flc~ing direction of the ; fluid moved by the rotation of the airfoil 211 is converted . :~ and the compression of the fluid is fluctuated turblently.
~`! Propulsion means is constituted by the airfoils 211 and the ;,~ 20 absorption airfoils 221 and provi~ed in the enc~losed ,~ compartment 2~0 of which upper and 1ower surfaces are .~ enclosed by the support body 220. The fluid in the enclosed ~ compartment 250 has buoyancy or propulsion produced . ~,;
, ,~ji upwar~ 1 y .
~i 25 The power generating system 103 produces power by ~ means of the fluid velocity increasing means 130 which .~ increases fluid ~elocity of the ~luid filled in the fluid ;
...
- ~, .1 : ~ j ~f ~`~`WO92/21862 PCT/KR92/00020 `2~88361 - 8 --pipe I20 by the character of the fluid passage.
Fig. 4 shows a first embodiment of the power ~`generating system lOO wherein the motor M, cc~,pre~sion mea~s 110, fl~id velocity increasin~ means 130 and turbine 140 are ;5 pro~ided at one side of the fluid pipe 120 in which fluid is filled.
~le electric motor M rota-tes the c~mpression means 110 upon being driven.
`~The campression means llO is a centrifugal pump tyFe in which, as shown in the drawings, rotating wings are :,, mounted radially and have a straight or radial type and `guiding wings 112 for turning the fluid which directs directly and induced to an induction port of the center of the pump, t~ward the circumference, minimize the angle with 15 the rotating direction of the rotating wings. When induced, the fluid has the same direction as the fluid in the turbulent compartment 113 at the outside of the rotating wings. With the ab,ove, arran~eme,nt, the fluid is turned at .~ :
the outside of the guiding wings 112, thus producing `20 centrif~,2~l power by which ~c~,pression effect is increased.
With the above-described cc~nstruction, the fluid ~;filled in the interior of the compression means 110 is .. .
compresse,d at the exit *hereof. Whe~n fed by str,,ng feeding force, the fluid is induced to the lnlet of the fluid `' 25 velocity increasing means 130.
The fluid is fed and turned, ha~ing ~n angle Wit21 re~pect ot the th~ ~enter 132. like the direc*ion shown in : .
. ~, ~, . j,. . .
~ W O 92/21862 PC~r/KR92~00020 .
. _ g _ 2~8&361 Fig. 1~. By the centrifugal force of the turning fluid, the - compression of the fluid at the center 132 is lcwer at the'':`
-small- radius location than at the large-radius location of the center 134. and in proportion to the radius to the critical point. With this construction, the compression of the fluid is higher than at the exit of the ~uiding wing 131. The fluid is emitted to the dischar~e port at the state of increased kinetic energy compared with the inlet and drives the turbine 140 to obtain electric energy.
The power to operate the turbine 140 may be obtained by a single fluid velocity increasing means 130. However, to obtain further stronger power, a number of the fluid ; velocity increasing means 130 (In the drawings, three means are shown) are desired to be connected in series. With this arrangement, gradually increasing force is obtained before electric energy i5 obtained. To ~inimize the decrease of ~i~ the effectiveness cau æ d by the difference of the fluid 3`
-~ velocity among each fluid ~elocity increasing means, the ~' fluid pipe at the exit of each fluid velocity increasing ,~
~i20 means is de5ired to ~e made as a straight pipe which is extendible gradually at the sectional area thelc~f.
. - .:
`~The wing of the turbine 140 sre forced to be rotated by the feed of the fluid to obtain electric energy.
The fluid. after having been compressed bY the fluid '25 velocity increasing means and by the turbine 140, is cooled. The fluid is further cooled ~y the repetitlve induction from the -compression means 110 to the fluid W092/2l862 PCT/KR92/00020 : 2088361 velocity incrteasing means 130, whereby the operation of the " system is stopped. To keep the system being operated, a heat-suction pipe 1~1 and a heat exchanger 1~0 are mounted in the middle of the fluid pipe 120 which constitutes a closed circuit.
.~
The heat exchanger 1~0 supplies the outside air to a radiator 152 by a fan 153 and compensate heat for a heat t~ansmitting pipe which transmits heat to the cooled fluid to maintain the normal temperature. With this ar~angement, the interior of the fluid pipe 120 has adequate temperature ` by the radiating pipe.
Accordingly, the power generating system of the pre ænt invention operates smcothly at the no~mal ~ temperature.
; 15 The fluid velocity increasing means has their inlets ~ - ,i. .
and outlets contacted with one nother and increases the fluid as followings.
As shown in Figs. ~ and 6, when flowing through the ` suction port of the fluid velocity increasing means 130 b the compression means 110, the fluid has the direction of ~ the fluid pas~e out of the center of the centripetal axis i , 132 by the guiding wing 131.
AccordinglY the fluid toward ar~und the centrip~tal axis 132 turns around the centripetal axis, thus producing the centrifugal force. By the centrifugal ~orce, the ccmpression of the fluid is low at a small-radius location.
.~
itl Hbwever, to the critical point the larger the radius is, the ... .
,'~,............. .... ... . .
WO92/21862 PCT~KR92/00020 ~ '.
3 ~ 1 .
higher the c~mpression of fluid is.
In the biginning, the compression of fluid is different at a large-radius location by the centrifugal force. The ~irection of fluid which is turning around the centripetal axis 132 at a high-pressure location does not disturb flowing fluid even thcugh the fluid pressure at the high-pressure location is higher than that at the exit of the guidin~ wing 131. The reason is that the oe ntripetal .force corresponding the centrifugal force is formed in the center part, whereby the velocity component acts as ioint `~forces which joins a straight driving component (cen~rifugal force with suction force tcward the center part), and turns.
Accordingly, the kinetic energy of fluid at the exit is greater than that at the suction port, t~ereby producing the kinetic energy of fluid increased over that of fluid pushed by the compression means 130.
,i'The grade of an oblique angle of the fluid of the exit ... .
` ~of the guiding wing 131 with respect to the center is adjusted by the fluid velocity and compression difference between inlet and exit. It should be noted that, when the `~angle is ad~usted, the fluid, when sucked, iS further slanted towards the direction of th~ center as the fluid velocity is the greater. As shown in Fig. 19, to minimize the decrease of the effect caused by the decrease of the Z5 fluid, the fluid pipe at the exit of the compression means I10 is deslred to be made as a straight pipe which has a gradual 1Y increasing section area.
.!
`~WO92/21862 PCT/KR92/00020 ,~,~,, . ~.
~20~8~61 12 The fluid velocity increased as the abo~e-described way drives the turbine 140, thus rotating the motor and the ;compression means 110. The fluid ha~ing its ener~y re-reduoe d is fed to the exit from the suction port of the 5 fluid velocity increasing means 130 to o~tain strong and fast energy and circulated. At this time, the remaining electric energY in the turbine 140 after driving the motor rotates a generator 141, thereby ~eing utilized to operate other electric appliance used for another purpose.
Fig. 1~ shows another fluid ~elocity increasing means ~",`'.:
~-, 130 comprising a number of fluid velocity increasing means elements connected one another, wherein suction port 134 and exit 135 fluid pipe are of cylindrical shape and the guiding wing which is lccated at the exit and directed in 15 the center , converts the fluid flcwing in the center so that the fluid passes around the centripetal axis and then turned toward the axis directi~n naturally.
~, I
Fig. 7 is a second embcdiment of the fluid velocity ~ increasing means 130. The construction of the power -~ 20 generating system in the seoond embodiment oompriæs the i same elements as that of the first embodiment. Hcwever, the ;~ ~ type of the fluid passage in the mean3 130 is different.
A disk-shaped fluid paS~n~e oonverts the fluid flowing in the centripetal direction to a radial direction For 3; 25 this purpose, the disk-shaped fluid pass e has a curved .~3 surface 133 so that the fluid flows perpendicular to the ~i-~ flowing- in ~direction. A guiding wing 131 is mounted in :''~ i W O 92/21862 PC~r/KR92/00020 _ 13 - 208~61 the middle of the curved surface 133 and has the same diameter of the inlet.
The guiding wing 131 is designed in such a manner that the radially discharging fluid is gradually oonverted with a smooth curvature and discharged toward the periphery at one end of the guiding wing.
` The fluid having been compressed initially flows in the inlet of the fluid velocity increasing means 130 and is turned along the radial fluid pas~ee and then discharged to the oulet of the fluid pipe 120. There fter, the direction ;~' of the fluid flowing straightly at the end of the guiding wing 131 is changed by the direction of the i~ner surface of the fluid pipe 120, thereby centrifugal force and force ,. ;;~ , further compressing outward fluid toward the exit are produced, resultin~ in the difference between the compression of the fluid near the center and the centrifugal force acting on the outward fluid. Consequently, the compression at the inlet of the fluid velocity increasing s 130 becomes ~reater than that at the outlet of the means 130, ~hus resultin~ in su~stantial kinetic energy of the fluid. Accordingly, pcwer is obtained by the remaining kinetic energy of the turbine 140.
Fig. 10 is a third em~odiment of the fluid velocity ~, increasing means 130.
~ 25 A U-turn fluid pas~e is added to the outside of the - ~ f luid pas~e of the secone embodiment. A curved surface 133 is provided at the interior of the center. A plurality ,~':@ . , ~.:J
20883'~`1 of guiding wings 131 are spaced and extends radially . The guiding wings 131 are of a curved shape. Inlets and outlets are connected with on~ another. The inlet has two pas~ges and the outlet has a divided two fluid passages. The fluid 5 flcws in the suction port 134 of the center and the suction port 13~ of the outside, r~spectively.
With the tw~ suction ports. the fluid turns from the outside of the cylindrical formation to the circumference, and then makes a U-turn. The oneside of the fluid pip~ 120 10 enclosing the guiding wing has small diameter and the other j~ end has large diameter. With this structure, the diameter ~i increases gradually from the inlet to the outlet, resultir~
.~ :
- in the outlet having a maximul diameter.
Accordingly, the fluid having b~en sucked in the guiding wing 131 flows in the center and then turns toward circumference. Thereafter, the compression at the outside ' increases by the centrifueal force. The velocity component ... .
of the fluid spreads toward the center of the fluid pipe ~-i 120. The velocity component spreaded taward the center is ,~` 20 utilized to turn the fluid at the outlet of the guiding wing ~` 131. Consequently, the fluid at the outlet increases bY the ~'~ centripetal and centrifl~e~l force.
X Fig. 11 shows a third embodiment of the fluid velocity ;~ increasing means 130. The suction port 137 at the outside 5~ 25 is used as a pas~ee through which the fluid is fed by the compressian means 110. The suction por~ 138 of the center is open to the outside. In the suction port- 130 is sucked 'l WO92/21862 PfCT/KR9Y/00020 ~i - 15 - ~ ~8~361 outside fluid ot~er than the fluid flowing in within the ;~ pipe. With this construction, the fluid at the center turns ~ by the influence of the fluid flowing in the inlet 134 and .
the outlet. Whfen the pressure at the center d~creases fy the centriffugal force, the outside fluid is sucked. The same a~.ount of the outside fluid as the amount of the fluid which is sucked in to the center from a portion of the fluid :' pipe of the circulating passage, is discharged. A portion of the circulating inner fluid is discharged and sucked.
`~ 10 With this costructure, the velocity increasing means has . .
~ ` both a closed and an open pf~sage.
. .
y Fig. 12 is a fourth embodiment of the fluid velf~city incr~asing means. As the most different construction, a ladder-shaped fluid pipe is additionally provided. The 15 ladder-~haped pipfe i-~ wcfund spirally and has a gradually .'`."f ~
decreased curved radius. With the ladder-shaped fluid pipe.
the pressure of the fluid passing through the spiral pip~ is ,~
lfowf at center having a small curved radius, and the pressure ~ f ~ of the fluid flowlng near an outside wall 161 is high. As .;
t,'j' 20 the curved radius of the outer waIl of the spiral pipe "f dec~eases ff~radually, the adjacently flf~wing fluid pr~vifdes biased forc~ tow2rd the center with a portion of the ouside fluid, b~ a collision with an outer surf~ce of the spiral pipe.
WiW~ the ~iased force, the centripetal force is strengthened. The strengthened centriFeta1 fo~ce increases ''i ' -~, the velocity of th~ fluid. As the length of the inner wal-l .,~
~. : , . - , .
, 20~3~1 - 16 or center axis and the outer wall 161 of the spiral pipe gradually lengthened, the biased force tcward the flowing direction of the fluid is strengthened and the velocity of the fluid further increases since greater biased force is formed around t}le center axis.
As shcwn in Fig. 12, when the spirally e~tending center axis at the outlet is thicker than other portion, only the hi~-pressure fluid at the outside is discharged, thus obtaining stronger kinetic energy.
10 It is desired that the spiral pipe 160 be gradually, upwardly lengthened at the outer wall 161 and inner wall ~ .
and an interior angle between the bottom face of the fluid pipe and the outer wall be uniform.
;~ With the le~gtll of the outer wall 161 which is ~.
` 1~ maintained toward the oulet, same effect may be obtained e~en the sectional area of the fluid passage decreases gradually toward the outlet. As shown in fig. 14, the fiuid pipe may have a square shape in-its cross-section.
J Fig. 13 is a cross-section of the spiral pipe 120 20 having a cut-away portion. The spiral pip~ 120 is wound upwardly, spirally.
x Figs. 16 and 17 shc~s the compression means of the . ~ . ',f~
power generating system. The compression means i5 provided ~, with a fluid pipe having the same construction as the velocity increasing means. At the outside of the guidin ~ wing 112 of the fluid pip~ is provided a plurality of '" :'~, ';
~ ~radial~y extending straight and short rotatable wings 111.
'~.; ' ~
;1 W092/2t862 PCT/KR92/00020 ~ .
- 17 - 2~8~61 ; Wlth this arrangement. the sngle when the fluid at the outlet is turned and sucked conforms with the rotation direction. The construction of the rotatable wing is j - similar to that of the radial-winged centrlfugal fluid duct.
However, the rotatable wing is short and narr~w upper and lower ends. The effect of the compression system further increases since the direction of the fluid sucked in the rotatable wing conforms with the direction of the rotatable wing. Further, the pressure at the outlet increases by the centrifugal force of the turning fluid.
Fig. 18 shcws another embodiment of the compressicn means wherein the suction port 139 is provided at the both sides of the axial direction.
Fig. 10 shows a fluid p~se~ee dividing pipe whioh is lS provided at a location at which the section of the fluid passage of the suction port decreases of the fluid velocitY
~ increasing means of the pcwer generating system. The fluid ~ ,;,! p2ssage dividing pipe is provided with a plurality of coaxial cylindrical fluid pipes of which leading end is , 20 thick and rear end is thin. With the coaxial cylindrical pipes, the fluid from a large-sectioned location of the . . .
fluid pipe is sucked uniformly over the~ who~e s~ction of the b!~',i fluid pipe. The section of the fluid pipe between the fluid dividing pipes i5 greatly decreased at the leading end. To the rear end, the fluid pipe has a uniform section or a section of small reduction rate. It is noted that the pipe has any configuration at its section, such as square or oval . ~ .
~ ~3 j ~
: W O 92t21862 PC~r/KR92/00020 20883~I 18 shape. The heat exchange system 150 exchanges the fluid of ordinarY temperature with the inner f 1 Uid by means of heat and supply heat to the inner fluid. The heat exchange system compri æ s a fan 153, a r diator 152 which is 5 connected to a heat sucking pipe 1~1 and a compressor. With ~, .
the heat exchange system, the over heat of the f luid circulatin~ the interior of the fluid pipe is prevented.
-~ resulting in the smooth operation.
Fig. 21 shows the heat exchange system 270 to 10 compensate heat for the interior of the system by absorbing the heat of the nor~al temperature of the outside of the `~ system. With the heat exchange system 270, the freezing of ,, .~
~ the moisture in the air by the absorption of the heat of the r, ,.~ I .
' air, is pre~ented.
In detail, the freezing of the heat exchange system . .
270 is prevented by the follcwing repetitive process. that , is, a water-soluble antifreezing solution flows in the interior of the radiatGr and then is raiæ d along a guiding pipe to the circulating system consisted of a pump.
~ .
~ 20 When the antifreezing solution beoomes lcw in its f .~ concentration the æolution passes through the fluid pipe in ~ a d~y ta~ which is provided with curve(~ radiating pins and } Y then is heated by a heater Z77 under the fluid pipe, whereby the air in the upper space of the dry tank is 25 discharged ~ a vacuum pump 279, resulting in the interior . -,i "~ of the dry tank 276 being made vacuous. Consequently, the solution is returned to a moisture-evaporated ordinary .. ... .
~ ','1 ' ` ~, 9 - ~08~361 solution, thus permitting a repetitive use of the antifreezing solution.
The heat exchange system 270 heat cool air of the interior of the propulsion system 200. With this ~ 5 construction, the heat exchange system 270 supply heat to - the outside ~eat sucking pipe 272 by means of a fan 271 which is located at one end of the radiator 273 w~lile-cooling some obiects by the cool air from t~e heat suction pipe 272. As described above, the heat exchange system 270 10 may be utilized as a cool system such as air conditioner or . . .
~ a refrigerator.
.. , : -`Fig. 1 shows the fluid velocity increasing means of the power generating system 100 wherein the press~re of the ~ fluid increases by the centripetal force. Fig. 2 and 3 show :~15 spiral piped fluid pascAge of the fluid velocity increasing ;3 ~;~system and the po~er generating system utilizing centrifugal force, respectiti~ely.
In the propulsion system 200 the pressure is produoe d to one side according to the flowing direction of the fluid ;~20 and the pressure is absorbed in the other direotion. The . ,.. ~ .
i~difference between the produced and absorbed pressure results in producing b~yancy or propulsion.
Fi~. 32 is a *irst embodi~ent of the enclosed propulsion system 200, wherein the dri~ing motor M is 25 rotated by electric energy obtained fro~ the pawer generating sYStem 100. thus rotating the rotatable body of cylindrical shape which is open at its upper and lower ends.
,~ '' ~, !-;
:, .,' WO92/21862 PCT/KR~2/00020 2~ 88 3 6 1 - 20 The rotatable W 210 has slanted, multi-stepped, ccoperable wings 211 on the periphery thereof. Each of the wings 211 is wide and should be mounted in such a manner that the angie between rotation direction and the wing is small.
The suppo~t W 220 consists of upper and lcw~ir surfaces 223, 224 and side surfaces to tightly close the ,;: rotatable body 210 and wings 211. The support W 220 has wings on the inner face fixed thereto which are crisscross with and have the isame slanted direction as the wings 211 of the rotatable body 210.
-; As shown in fig. 13, the wing 221 has minute grooves 222 in the upper face thereof to increase the area on which, when the fluid containing air or liquid flows dbwn~rdly~
5 the fluid acts, and to decrease the downwardly acting :` pressure by the turbulent fluid in the minute groo~es 222.
"
Accordingly, the wings 211 rotated by the driving ~- motor feeds downwardly the fluid filled in the support W
;~ 220. Furthermore, the ~uoyanCY to lift the wings 211 :
:1 20 together with the rotata~le body 210. In summary, The ~y ' phenomenon arises at every location at which thei wings 211 ~ and the crisscross absorption wing 221 rotate fast. The .~ bu~YancY force obtained at this time is united to be served as strong propulsion force or buoyancy.
Th~ fluid moves downwardly by the rotation of the ,5X, wings 211. The support body 220 has absorption grooves 225 ;~
~i ~ in the -lower sur*ace 224 theireof having the same "~
. .~, .
.
,i , - ~ . ..... , . -- -, . ; - - - - . . . . . .. .. . ..
' . ' ', ,;: ' ` ' ' ` ' ' ".': -' ''. : ' ' ' '. ` . ` '': - ' ' - :- ' ' ' ' .`.: :
.~ . .
~ . i configuration and construction as the minute gr~oves 222 in the wings 211~ With this arrangement, the upwardly pressure by the fluid acts strongly further than the downwardly pressure, thus obtaining more stronger buoyancy.
Th~? distal absorption wing 221' and other absorption wings 221 are mounted at different angle so that the fluid flows in the center in slightly deflected dir~ction. With-this arran~ement, additional effect of the increase of the pressure of t~e upwardlY f luid frvm the center, is obtained by the same theory as in the fir~t embodiment of the fluid increasing means of the p~wer generating system to produce the centrifugal force of thie fluid flowing toward the center to adjust the direction of the fluid flowing through the center. In addition, the diameter of the bearing-supporting location at the upp~r portion is larger than the center, therebv on]~ high-pressure fluid havirg large turning radius is disc}~rged and turned at the upper portion. As the upper and lo~er width of th~ fluid passage of the :?
~ ; uppermost part of the upper being narro~, the pressure at . ~
~^~i 20 th~? upper surface is higher than that at the lcwer surface, thus increasing the buoyarcy further.
With the difference of the pressure acting on the upper part and the lower part by the m?ovement of the fluid, ~ buoyancy or propulsion force from the airti~ht interior to i 25 one direction is obtained. The buoyancy or propulsion force ' ,?
is used for ships or air~lanes.
~ 1n case the ab~v~-described systems of the sa~ ~ number ....
",: . - ~. . : : . , W O 92/21862 PC~r/KR92/00020 20 8~3 6 ~ ~ 22 are mounted at both sides of and spaced equally from the center line of the airplanes or ships, respectively~ the bodies of the airplanes or ships are lifted and balanced.
Furthermore, if the systems are mounted at the leading or rear end of the bodies with the lengthwise axis being ; parallel with the floor, the bodies are propelled toward the ~ direction perpendicular to the byoyancy acting direction.
~; If the syste~s are mounted at the surface parallel to the direction intended to propel with the lengthwise axis bein~
parallel with the floor, the bodies are turned from side to ;^- side.
, .
As being provided within the airtight room, the , systems are rarely influenced by weather change or a ; ~ treacherous air current such as a storm, or the change of i5 the air density, resulting in normal operation. Futhermore.
',. an airplane can he taken off and landed perpendicularly ~ without using a runway.
'.`,J In case the the above-de æ ribed system is used as a buoyancy sYstem, an outside body 230 is fixed to the outer surface of the sYstem to prevent overheat which may be .Y~ .
~; caused by the movement of the fluid. The outer body 230 is - ~; open at its upper and bottom surfaces. With the r3t tion of the rotatable bcx~y 210, the outside fluid flows along the i outer surface of the support ~ody 220, thus bringing oil cooling or air cooling . Conversely, in case the abov~-described system is u~ed as propulsion system, the fluid within the airtight room is apt to be cooled. To ~''~ ' ,,.~
. . ~ . .
.~ . .
- 23 - 2~8836~
`~ prevent the cooling, heat maY ~e supplied to the interior fluid from the outside fluid.
It is desired that the fluid in the airtight roo~ 2~0 have uniform pressur~ and the uniform pressure be exerted on the interior of the airtight room 2~0. Even not shown in the - drawings, an extra fluid reservoir and pressure control de~ice comprising a pressure sensor and a suction or discharging pump are desired to be mounted at a suitable location out of t~e airtight room 250.
`~ 10 The pressure control device comprises a rotatable b~dY
210 and a support body 220 which are rota~ed respec~ively.
. . .
With this construction, to rotate the rotatable b~dy 210, ~ the center bottom of the rotating axis 212 of the rotatable ',,`;,`:! body 210 communicates with the interior of the airtight room 250 so that a pressure is controlled by the inooming and ,.`~`7 outgoing of the interior fluid in respect to pressure ~: .
control tube and the airtight room 250 through an opening in ,;~`s the rotating axis 212.
~ Fig. 32-B, a generator is mounted on the rotating axis ~ `.
~ ~ 20 212 of an outer wing Z11 on which an absorption wing 221 of ,. ......................................... .
the propulsion system is mo~nted. With this arrangement, an electric power is obtained by the power produced by the rotation of the absorption wing 221. Furthermore, the rotatable body 210 on which is mounted the absorption wing -25 221 may be fixed and not rotated to serve only as a guiding ..
wing.
, ~The support kody 220 is dri~en thrcugh transfer mans W092/2tX62 PCT/KR92/00020 2~ ~8 36'l ~ 24 mounted at the dri~ing motor. To increase the effect of the propulsion system 200, simultaneous with the driving of the rotatable body 210 ~nd its fixed wing 211, the absorption wing 220 facing the wing 211 is driven in the same direction as the fixed wing 211.
The power transfer means 240 comprises a rotatable ~ axis 212 and a pluralitY of gears engaging with one another - and ~eing mounted on the bot ~ n face of the support body ^ 220. With this construction, the rotation force is 10 respectively transferred to the rotatable body 210 and the support body 220. A different deduction rate may be obtained depending ~n the number and diameter of the teeth of the gears 241. With the deduction rate, the velccity of the rotatable wing is faster than that of the support bodY
15 of the absorption wing 221. Hbwe~er. it is desired that the ~' absorption wing 221 and the rotatable wing have ,~ comparatively fast velocity.
It is within the scope of the present in~ention that ., .
~ ' the minute grooves 222 and absorption grooves 225 have anY
.,~, .
,, 20 shape or configuration so long as the groove~ 222 nd 225 `~ are able to form turbulent flow when contaced with the ~, fluid. That is, the minute grooves 222 and 225 have a ~î'l hemispherical or semicylindrical shape, and a partitioned semicylindrial or slanted double surface type.
~ ~ .
' 25 To increase the effect of absorption, another minute .~ .
;~ grooves may be pro~ided on the surfaces of the ~inute ~, grooves 222 and absorption grooves 225, thu~ constituting : ~, `;
, `` - 25 - 2088361 double grooves.
It is desired that a guidin~ member 231 be mounted at an upper end of the outer body Z30 so that the outside fluid has lcw flu~d resistance and be suc~ed smoothly. ~ach 5 bearing to deduce friction resistance is mounted a lo~ation at which the support body 220 and the rotatable body 210 contact wit}- each other and support the rotation thereof .
Fig. 36 shows a third embodiment of the propulsion system Z00 wherein the spiral fluid pipe 260 and compression 10 means 280 provide buoyancy or propulsion force c~used when ;~.-the fluid is forcedlY and wavely fed within the airtight ; ~pipe and then directed upwardlY.
......
. .~A semispherical or semicYlindrical-shaped groo~es are :,.closely provided on the bottom face 262 of the fluid pipe ~.15 120 of wavy shape. The fluid flc~/s along the wavy-shaped pipe 120. The pressure exerting on the bottom face by the .~1ower fluid pas~A~i~ is decreased by the grooves 263. The .-J
. ~upper and lower width of the fluid passa~e of the center of : ::the upper fluid pass~e is nar.rowed to exert the pressure on ~;~:20 the upper part strongly, whereby buoyancy or propulsion ~force of the bodies of the airplane or ship is obtair~d bY
a united force. Further.~ore, the compression force by the fluid in the spiral pipe is further obtained, thus increasing the fluid velooity, w~ereby greater buoyancy is 25 n~ditionally obtained.
At this time, for the continuous feedir~ of the fluid ~...
~ ~. in compre~sion, compression mean5 having similar ~ WO92/21862 PCT~KR92/00020 i construction as the centrifugal pump and thus having feeding force by the rotation of the 40.
In Figs. 38, 39 and 40, a semispherical or ~,` semicylinderical groo~e 266 is provided in the lowermost location amon~ the locations at which wavy curved faoe s are formed. With this arrangement, when the fluid is fed . ~
~-forcedly, the pressure exerting on the bottom of the fluid ::;
passage by the d~wnwardly flowing fluid, is absorbed or ~ortexed by the grooves 266, whereby upward1y buoyancy or ,.
,.
~`~10 propulsion force is increased. It is within the scope of ~ the present invention that the grooves 266 have any curved !~
configuration such as a semispherical or semicylindrical or slanted double faced or similar curved shapes.
In Figs. 41, 42 and 43, wavy, curved formation is ; ~15 provided on the bottom 262 of the interior of the spiral pipe 120, wherein the grcoves 266 are formed in the lcwer portion and the width of the upper and lG~er portion of the fluid passage i5 gradually narrowed at the uppermost , ,iportion, whereby a turbulent flow by the ~urved turning j, ~A'~
~20 portion of the upper fluid pasC~e is prevented and strong .'.'1 ;` ~pressure is exerted on the upper surface , resulting in the ,;, ~:: f~ production of the upward buoyancy.
, . . .
~The effect by the wave is different according to the ... .
size of the width of the upper and lower part of the fluid ~25 passage and distance between the pitch of the wavy curved -~formation. It is desired that the distance and size be ~adjusted most efficiently.
. .
~ ' .
2~8~3 Fig. 45 is a fifth emb3diment of the propulsion system 200 of the present invention. A slanted double face groove Z62 is formed on the bottom and upper faces of a long fluid pipe. The iong fluid pipe is w~und spirally by the same ~ S manner of the fourth embodiment of the pcwer generating ;- system as shcwn in Fig. 12. With this arrangement, the forced feeding of the fluid by the compression means 130 -~ tcward to the spiral fluid pipe 120 results in the ; difference of the pressure between the upper ~ace and the bottom face by the turbulent flcw of the fluid in the . ."
slanted double face groove~ and by the difference of the surface area. ~hat is, an upwardly pressure is increased ,~ by the fluid at the upper surface and a downwardly pressure is decreased at the b~ttom surface, resulting in the . .
~ 15 production of the buoyancy. The effect is further increased , ;j, in that the effect of t~ compression of the fluid is additionally obtained.
The direction of a location having a large slope angle ,~ at the bottom surf~ '? of the slanted double face OErcove is .. , ii - .
~ 20 same as the direct.on in which fluid meets. The upper '~
~,` surface of the slanted double face groove is formed by a ~, manner in contrast with the above~ scribed m~nner. The ':' ' ~i .
;~ fluid pipe has a square or ladder 3hape in its section causing the upper and lower walls of the fluid pipe to be ,~J 25 graduallY distant and the section of the fluid pasæage to be ., :
uniformly maintained or graduallY enlarged.
In one surface having a large angle of the slanted ~
. :~,....................................................................... .
,,~
W092/2~862 PCTiKR92/00020 f~, 2088361 28 - `'-~
double face groove may be provided with a doub~e groove of semispherical or semicylindrical shape. The uppermost and lowermost of the slanted face are rounded.
Fig. 47 is a sixth embodiment of the spiral fluid pipe 5 of the propulsion system wherein a semicylindrical fluid pipe is spiral 1Y wcunded and has a semicircular ~ottom of continuous wheel shape having a negative curved rate and having a comparati~elY long center line at one direction. A
groo~e is provided in the bottom of which both sides have a 10 small curved radius to produce buoyancy by the fluid flowing along the spiral formation. While the fluid flows through the semicYlindrical spiral fluid p csage and circulates through the upper and lower fluid pass es, the groove formed in the bottom face of the fluid pipe having small 15 curved radius both si~es lowers a downward pressure . With the construction of the tw~ upper fluid passages wherein the upper and lower width of the fluid passage of the upper fluid passage gradually narrows, resulting in the uppermost portion having a minimum width.
In Fig. 49, an outer body 230 enclosed the outer sur~ace of t~e spiral fluid pipe 260 and a fluid duct 290 is mounted at the upper portion of the pipe 260, the fluid duct 290 bein~ served to move an outer fluid upwardly or downwardly. With this arrangement. the airtight interior 25 fluid maY be cooled or heated by the outer fluid. It is desired that the outer surface of the s~iral pipe have a -large area ~or good heat tr~nsmission.
~ :
' ' .
, ,, . , ~, . . : , ~ , . ..... . . .
- 29 - 2~8836~
Fig. ~0 is a seventh embodiment of the propulsion system wherein an airtight ro~m 250 has a circular shape in cross-~ection and a wing member 268 is mounted radially to serve as a guiding win~ of the centrifugal fluid duct and slantedly toward the rotation direction of the rotatable body 210. When the rotatable body 210 is rotated, the interior fluid circulates by the wing member 268 and the buoyancy is exerted on the wing member. The buoyancy effect may be obtained by the pressure decrease at the bottom face of the grooves 269.
In this construction, the absorbing groove 225 is provided in the lower surface 224 of the support body 220, an upward pressure is exerted on the unseen face of the rotatable wing 221, the upper and lower fluid width of the upper part graduallY decreases resulting in the minimum width of the uppermost part and the rotation of the rotatable body is performed by the driving motor M.
Fi~s. 53 and ~4 are eighth embodiment of the propulsion system 200 of the pre æ nt invention, wherein an absorbing groove 266 is formed in the i~ner bottom-262 of the spiral fluid pipe 260. the width of the fluid pas~ge of the upper fluid passage gradual~y narrows resulting in the minimum width of the uppermost par~ ~00. With thic arrangement, an upward buoyancy or propulsion force may be obtained by the difference of the pressure exerting on the upper and bottom faces.
As shcwn in Fig. ~, a ~roo~e has a slanted double :.
faces and the slanted groove in the bottom of the lcwer fluid passage and the upper face of the upper fluid passage is directed oppositelY, at the bottom of the lcwer fluid passa~e and the upper face of the upper fluid passAee.
Fig. ~6 is an ninth embodiment of the propulsion system., wherein disk-shaped members 216 of multistage shape are repetitivelY mounted on the rotatable body 210 and a slanted double face groove 262 is formed in the upper or lcwer face thereof to obtain buoyancy or propulsion force at one side thereof. One of the slanted faces has a small angle and the other slanted face has a large angle. The large angled face 262 is directed to the rotation direction and the lcwer face is directed oppositely.
Cutoff bars 264 are provided crisscross with one i5 another between the rotatable disk-shaped members provided at each end of the fluid passage to prevent the movement of . . .
the fluid toward the rotation direction of the rotatble disks, thus increasing buoyancy. For easy cutoff and passing of the fluid at the same time , the cutoff bar has a negative curvature at the side ther~of. The rotatable dislcs may have a cone shape or its inver~e shape.
To prevent sudden rise or fall of the temperature of the inner fluid of the above-described propulsion or b~oyancy system, the heat exchange system 150 may be mounted . . .
at one side of the fluid pipe. Otherwise, the fluid is cooled bY the outer f luid from the outside of the system.
Though not shown in the drawings, the outer f luid f ~ c~
': ', .
- 31 - 2~883~1 throu~ a pipe which is connec~ed ~o the inner fluid. A
pressure control tank provided with a pressure sensor and a suction and discharging pump is provided at the outside of the system to control the pressure of the inner fluid uniformly.
Fig. 23 shows a connection of the fluid which acts is vortexed in the minute grooves of the propulsion system 200 and acts at one side. Fig. 24 is an enlarged view which sh~ws a double groove construction wherein a plurality of 10 another minute groo~es sre sdditioned to the surface of the minute grooves to increase the effect of the propulsion system 200. Fig. 2~ shows the slanted double face groove is formed in the surface of the upper and lower part of the fluid pipes snd Fig. 26 shows another grooves or semispherical or semicylindric~l ~- w ve~ sre sdditioned to the surface of the slanted double fsce groove to effect the effect of the system.
Fig. Z7 shows a connction of the rotatsble body 210 of the propulsion system 200 with the support body 220 wherein 20 the distance ketween upper and lower f`ace of the center of the upper part of the airtight room 2~0 is shortest and the absorption grooves 22~ are pro~ided in the lower faoe, resulting in the difference of the pressure so that buoyancy or propulsion force is produced.
In summary, the power generating system is operated by an ~lectric pow~r from outside. In case the supply of the outside power is interrupted, self-generating power is-.
W O 92/21862 PC~r/KR92/00020 ',..
~ - 32 ~1~88361 produced, thereby buoYancY or propulsion force to operate bodies of airplanes or ships is produ oe d. The power generatir~ system absorbes heat from the outside fluid and operates by the self-generating power. By this electric S energy, one-side directed po~er is pro~uoe d in the interior of the propulsion system. thus producing buoyancy or propulsion system. With the present invention, airplanes, ~ehicle or ships may be operated pr~perly even in a~normal atmospheric phenomena. Furthernore, to obtain the po~er generating system and propulsion or buoyancy generating sYstem maY be combined for suitable use or purpose.
Otherwise, only the power generating system is utilized to operate an electric ~ehicle or industrial or home implements. The heat exchanger is utilized as cooling apparatus The forgoing detailed description has been given for clearness of understanding only, and no unnecessary limitations should be understood therefrom, as some clodlfi~tions wi 1 l bs obvious to those ski l led in the rt.
, - -, , , , :, , ,; . ~ -- . ... . , . , ~ - - ,
Claims (17)
1. A system for generating power, propulsive force or buoyancy by utilizing fluid comprising power generating means and propulsion means, the power generating means comprising:
an electric motor rotated by an outside power supply;
compression means for feeding a fluid forcedly by the rataion of the electric motor;
fluid velocity increasing means including a disk-shaped fluid pipe, whereby the fluid flows from the outside or input side of the disk-shaped fluid pipe toward the center of the fluid velocity increasing means perpendicularly to the axis of the center thereof and deflectively from the center thereof and in a radial direction of the centrifugal direction thereof, and then turns about the center, thus producing centrifugal force, whereby an outlet is provided by pressure difference at a high pressure location at which kinetic energy is stronger than that of the input side;
a turbine for generating power from the energy in a stream of fluid which is discharged from the velocity increasing means, whereby the fluid cooled by heat energy taken from the turbine is fed by the compression means; and heat exchanger means for obtaining the taken heat energy from a fluid of the normal temperature and re-introducing the fluid of the normal temperature into the velocity increasing means;
the propulsion means comprising:
feeding means for forcedly feeding a fluid from one side to the other side by an electric energy from the power generating means;
a first fluid pipe having a groove in the surface of a turning portion thereof to forcedly convert fluid passage and to direct the fluid to the surface of the fluid passage with a gradient; and a second fluid pipe which has a gradually decreasing section, whereby the pressure of the fluid exerts strongly on the surface of the second fluid pipe, thus producing pressure difference causing the production of a force directed in one side.
an electric motor rotated by an outside power supply;
compression means for feeding a fluid forcedly by the rataion of the electric motor;
fluid velocity increasing means including a disk-shaped fluid pipe, whereby the fluid flows from the outside or input side of the disk-shaped fluid pipe toward the center of the fluid velocity increasing means perpendicularly to the axis of the center thereof and deflectively from the center thereof and in a radial direction of the centrifugal direction thereof, and then turns about the center, thus producing centrifugal force, whereby an outlet is provided by pressure difference at a high pressure location at which kinetic energy is stronger than that of the input side;
a turbine for generating power from the energy in a stream of fluid which is discharged from the velocity increasing means, whereby the fluid cooled by heat energy taken from the turbine is fed by the compression means; and heat exchanger means for obtaining the taken heat energy from a fluid of the normal temperature and re-introducing the fluid of the normal temperature into the velocity increasing means;
the propulsion means comprising:
feeding means for forcedly feeding a fluid from one side to the other side by an electric energy from the power generating means;
a first fluid pipe having a groove in the surface of a turning portion thereof to forcedly convert fluid passage and to direct the fluid to the surface of the fluid passage with a gradient; and a second fluid pipe which has a gradually decreasing section, whereby the pressure of the fluid exerts strongly on the surface of the second fluid pipe, thus producing pressure difference causing the production of a force directed in one side.
2. A system for generating power, propulsive force or buoyancy by utilizing fluid comprising power generating means and propulsion means, the power generating means comprising:
an electric motor rotated by an outside power supply;
compression means for feeding a fluid forcedly by the rataion of the electric motor:
fluid velocity increasing means for increasing the kinetic energy of the fluid, the velocity increasing means including a spiral fluid pipe having a gradually decreasing radius, whereby the fluid turns parallel to the periphery of the centripetal axis and the velocity component of the fluid is deflected toward the center while contacting the inner sureface of the wall of the spiral pipe at the outside, thus increasing centripetal force, thus increasing fluid velocity, and consequently the fluid velocity increases at an oulet at which radius decreases gradually, whereby only outer fluid having a high pressure is discharged at the outlet, thus increasing the kinetic energy of the fluid:
a turbine for generating power from the energy in a stream of fluid which is discharged from the velocity increasing means, whereby the fluid cooled by heat energy taken from the turbine is fed by the compression means; and heat exchanger means for obtaining the taken heat energy from a fluid of the normal temperature and re-introducing the fluid of the normal temperature into the velocity increasing means;
the propulsion means comprising;
feeding means for forcedly feeding a fluid from one side to the other side by an electric energy from the power generating means;
a spiral fluid pipe having a groove in the surface of a turning portion thereof to forcedly concert fluid passage and to direct the fluid to the surface of the fluid passage with a gradient; and a fluid pipe which has a gradually decreasing section, whereby the pressure of the fluid exerts strongly on the surface of the spiral fluid pipe, thus producing pressure difference causing the production of a force directed in one side.
an electric motor rotated by an outside power supply;
compression means for feeding a fluid forcedly by the rataion of the electric motor:
fluid velocity increasing means for increasing the kinetic energy of the fluid, the velocity increasing means including a spiral fluid pipe having a gradually decreasing radius, whereby the fluid turns parallel to the periphery of the centripetal axis and the velocity component of the fluid is deflected toward the center while contacting the inner sureface of the wall of the spiral pipe at the outside, thus increasing centripetal force, thus increasing fluid velocity, and consequently the fluid velocity increases at an oulet at which radius decreases gradually, whereby only outer fluid having a high pressure is discharged at the outlet, thus increasing the kinetic energy of the fluid:
a turbine for generating power from the energy in a stream of fluid which is discharged from the velocity increasing means, whereby the fluid cooled by heat energy taken from the turbine is fed by the compression means; and heat exchanger means for obtaining the taken heat energy from a fluid of the normal temperature and re-introducing the fluid of the normal temperature into the velocity increasing means;
the propulsion means comprising;
feeding means for forcedly feeding a fluid from one side to the other side by an electric energy from the power generating means;
a spiral fluid pipe having a groove in the surface of a turning portion thereof to forcedly concert fluid passage and to direct the fluid to the surface of the fluid passage with a gradient; and a fluid pipe which has a gradually decreasing section, whereby the pressure of the fluid exerts strongly on the surface of the spiral fluid pipe, thus producing pressure difference causing the production of a force directed in one side.
3. A system for generating power, propulsive force or buoyancy by utilizing fluid comprising power generating means and propulsion means, the power generating means comprising:
an electric motor rotated by an outside power supply;
compression means for feeding a fluid forcedly by the rataion of the electric motor;
fluid velocity increasing means for increasing kinetic energy including a disk-shaped fluid pipe and a cylindrical turbulent flow room provided in the centrifugal direction and having a gradually increasing radius of curvature at the outside portion thereof, whereby the fluid flows toward the center and turns toward the periphery and then flows into the turbulent flow room, and consequently, the fluid pressure at a location adjacent to the inner surface of the turbulent flow room becomes higher than that at a location adjacent to the center, thus increasing the kinetic energy at the outlet of the fluid velocity increasing means;
a turbine for generating power from the energy in a stream of fluid which is discharged from the velocity increasing means, whereby the fluid cooled by heat energy taken from the turbine is fed by the compression means: and heat exchanger means for obtaining the taken heat energy from a fluid of the normal temperature and re-introducing the fluid of the normal temperature into the velocity increasing means:
the propulsion means comprising;
feeding means for forcedly feeding a fluid from one side to the other side by an electric energy from the power generating means:
a spiral fluid pipe having a groove in the surface of a turning portion thereof to forcedly convert fluid passage and to direct the fluid to the surface of the fluid passage with a gradient: and a fluid pipe which has a gradually decreasing section, whereby the pressure of the fluid exerts strongly on the surface of the spiral fluid pipe, thus producing pressure difference causing the production of a force directed in one side.
an electric motor rotated by an outside power supply;
compression means for feeding a fluid forcedly by the rataion of the electric motor;
fluid velocity increasing means for increasing kinetic energy including a disk-shaped fluid pipe and a cylindrical turbulent flow room provided in the centrifugal direction and having a gradually increasing radius of curvature at the outside portion thereof, whereby the fluid flows toward the center and turns toward the periphery and then flows into the turbulent flow room, and consequently, the fluid pressure at a location adjacent to the inner surface of the turbulent flow room becomes higher than that at a location adjacent to the center, thus increasing the kinetic energy at the outlet of the fluid velocity increasing means;
a turbine for generating power from the energy in a stream of fluid which is discharged from the velocity increasing means, whereby the fluid cooled by heat energy taken from the turbine is fed by the compression means: and heat exchanger means for obtaining the taken heat energy from a fluid of the normal temperature and re-introducing the fluid of the normal temperature into the velocity increasing means:
the propulsion means comprising;
feeding means for forcedly feeding a fluid from one side to the other side by an electric energy from the power generating means:
a spiral fluid pipe having a groove in the surface of a turning portion thereof to forcedly convert fluid passage and to direct the fluid to the surface of the fluid passage with a gradient: and a fluid pipe which has a gradually decreasing section, whereby the pressure of the fluid exerts strongly on the surface of the spiral fluid pipe, thus producing pressure difference causing the production of a force directed in one side.
4. A system for power generating, propulsive force or buoyancy by utilizing fluid according to any of Claims 1 to 3, wherein the power generating means includes heat.
exchanger means.
exchanger means.
5. A system for power generating, propulsive force or buoyancy utilizing fluid acccorrding to any of claims 1 to 3, wherein the compression means of the power generating means and the propulsion means includes a plurality of guiding wing are spaced at a predetermined distance from the centripetal axis, a turbulent flow room mounted in a centrifugal direction, a cylindrical member having a gradually increasing radius of curvature at the outside thereof and a plurality of short and straight wings extending radially in the interior of the turbulent flow room, whereby the fluid flown into the center of the fluid pipe turns the guiding wings and flow into the turbulent flow room causing the difference of angle between the inner face of the cylindrical member and the fluid, resulting in the conversion of the direction of the fluid.
6. A system according to Claim 2, wherein the velocity increasing means of the power generating means is an airtight fluid pipe which has a gradually decreasing radius of curvature and is mounted spirally.
7. A system according to any of Claims 1 to 3, wherein the propulsion means includes a rotatable or fixed absorption wings having a plurality of grooves formed therein, a compression wing on which a pressure is exerted in a direction of buoyancy by a reaction of pushing the fluid, the compression wing is wide and mounted in a manner that, when rotated, the angle of the rotatary direction and mounting portion is small, and includes a support body and a plurality of absorption grooves formed in the bottom of the fluid passage.
8. A system according to Claim 7, wherein the direction of the fluid sucked into the center of the absorption and the compression wing is deflected slightly from the center, resulting in the turning of the fluid in the center and wherein the support body at the upper part is protruded circularly, whereby the fluid with increased pressure is discharged.
9. A system according to Claim 7, wherein the support.
body of the propulsion means is provided with transfer means which transfers the rotation force of the absorption and the rotation wings to one another by the engagement of the teeth of a driving means.
body of the propulsion means is provided with transfer means which transfers the rotation force of the absorption and the rotation wings to one another by the engagement of the teeth of a driving means.
10. A system according to Claim 7, wherein a generator is mounted on a driving axis of the absorption wing of the propulsion means, whereby the generator rotates upon the rotation of the absorption wing to produce electric energy.
11. A system according to any of Claims 1 to 3, wherein the spiral fluid pipe having a gradually decreasing radius of curvature is provided with an absorption groove at the lower fluid passage and has a gradually decreasing width of the upper and lower part of the upper fluid passage, resulting in an uppermost part having a minimum width.
12. A system according to any of Claims 1 to 3, wherein the spiral fluid pipe having a square or ladder shape in cross-section and a gradually decreasing radius of curvature is provided with double faced grooves in the upper and lower parts thereof, the upper and the lower slanted faces being arranged in an inverse manner.
13. A system according to any of Claims 1 to 3, wherein the fluid pipe of the propulsion means has a negative curvatureed semicircular bottom face and has a spirally wounded shape in cross-section and is provided with grooves in a location having a small radius of curvature.
14. A system according to any of Claims 1 to 3, wherein the airtight propulsion means has a circular shape in cross-section and is mounted radially on the rotatory axis and includes a wing member mounted slantedly in a rotational direction to serve as a rotatory wing of a centrifugal fluid duct, whereby buoyancy is exerted on the wing member upon circulation of the inner fluid, the cylindrical fluid pssage having a gradually decreasing upper and lower width of the upper part thereof, resulting in the cylindrical fluid passage having a gradually decreasing upper and lower width of the upper part thereof and absorption groove in the bottom thereof.
15. A system according to any of Claims 1 to 3, wherein the spiral fluid pipe having a square shape in corss-section is provided with absorption grooves in a lower fluid passage, or upper and lower fluid passages, or the upper surface thereof, the upper fluid passage of the spiral fluid pipe having a gradually decreasing width at the upper and lower parts to be have a minimum width.
16. A system according to any of Claims 1 to 3, wherein a motor of the driving axis of the propulsion means is provided with a rotatable body and a plurality of disk-shaped members in multi-stage shape is mounted on the rotatable body, the upper and lower surfaces of the rotatable body being provided with slanted double faced grooves and wherein a cutoff bar is mounted between each end of the rotatable disk members to cut off fluid upon rotating of the rotatable body.
17. A system according to any of Claims 1 to 3, wherein the heat exchanger means includes heat suction means for sucking heat of an outside fluid, a soluble antifreezing solution for flowing through a guiding pipe into a circulation device such as a vacuum pump, whereby the fluid is lifted along the guiding pipe and then injected again, and in case the density of the antifreezing solution becomes low, the antifreezing solution passes through a dry tank and is heated at the bottom of the dry tank so that air in the upper space is discharged to cause re-circulation of the evaporated antifreezing solution.
Applications Claiming Priority (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| KR910009133 | 1991-06-01 | ||
| KR91-9133 | 1991-06-01 | ||
| KR910009134 | 1991-06-03 | ||
| KR91-9134 | 1991-06-03 | ||
| PCT/KR1992/000020 WO1992021862A1 (en) | 1991-06-01 | 1992-06-01 | Power and propulsion system utilizing fluid |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA2088361A1 true CA2088361A1 (en) | 1992-12-02 |
Family
ID=26628631
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA002088361A Abandoned CA2088361A1 (en) | 1991-06-01 | 1992-06-01 | Power and propulsion system utilizing fluid |
Country Status (5)
| Country | Link |
|---|---|
| EP (1) | EP0541761A1 (en) |
| JP (1) | JPH06502707A (en) |
| AU (1) | AU650984B2 (en) |
| CA (1) | CA2088361A1 (en) |
| WO (1) | WO1992021862A1 (en) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11001378B2 (en) | 2016-08-08 | 2021-05-11 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
| AU2016338382B2 (en) | 2015-09-02 | 2021-04-01 | Jetoptera, Inc. | Ejector and airfoil configurations |
| US10464668B2 (en) | 2015-09-02 | 2019-11-05 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
| WO2019005937A1 (en) | 2017-06-27 | 2019-01-03 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
| DE102021004804B3 (en) * | 2021-09-23 | 2023-02-16 | Norbert Lother | Aerodynamic drive unit |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CH255536A (en) * | 1946-12-16 | 1948-06-30 | Airofiltre S A | Method and device for adjusting the angle of entry of fluid into a fan. |
| US2666453A (en) * | 1948-06-28 | 1954-01-19 | Power Jets Res & Dev Ltd | Gaseous fluid flow system |
| US4043126A (en) * | 1976-06-29 | 1977-08-23 | Jaime Rios Santos | Turbine engine for automotive vehicles |
| FR2507253A1 (en) * | 1981-06-09 | 1982-12-10 | Tissier Bruno | Compressed air drive for vehicle - has converted IC engine acting as compressor for air drive motor |
| FR2566845A1 (en) * | 1983-08-29 | 1986-01-03 | Cordier Jean | Air compression power station |
| DE3835048A1 (en) * | 1988-10-14 | 1989-05-18 | Genswein Annemarie | Heat engine for obtaining industrial work from atmospheric air heat |
-
1992
- 1992-06-01 WO PCT/KR1992/000020 patent/WO1992021862A1/en not_active Application Discontinuation
- 1992-06-01 EP EP92911453A patent/EP0541761A1/en not_active Withdrawn
- 1992-06-01 JP JP4511333A patent/JPH06502707A/en active Pending
- 1992-06-01 CA CA002088361A patent/CA2088361A1/en not_active Abandoned
- 1992-06-01 AU AU19086/92A patent/AU650984B2/en not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| AU1908692A (en) | 1993-01-08 |
| EP0541761A1 (en) | 1993-05-19 |
| AU650984B2 (en) | 1994-07-07 |
| JPH06502707A (en) | 1994-03-24 |
| WO1992021862A1 (en) | 1992-12-10 |
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| Date | Code | Title | Description |
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| EEER | Examination request | ||
| FZDE | Discontinued |