US788006A

US788006A - Compound marine turbine.

Info

Publication number: US788006A
Application number: US22198604A
Authority: US
Inventors: James Wilkinson
Original assignee: WILKINSON TURBINE Co
Current assignee: WILKINSON TURBINE Co
Priority date: 1904-08-24
Filing date: 1904-08-24
Publication date: 1905-04-25
Anticipated expiration: 1922-04-25

Description

No. 788,006. PATBNTED APR. 25, 1905. J. WILKINSON.

GOMPOUND MARINE TURBINE.

APPLIUATION FILED AUG. 24, 1904.

4 SHEETS-SHEET 1.

Wmme@ PATENTED APR. 25, 1905.

J. WILKINSON.

GOMPUUND MARINE TURBINE.

APYLIOATION FILED AUG. 24, 1904.

4 SHBETS-BHEET 2.

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PATENTED APR. 25, 1905. J. WILKINSON, GMPUUND MARINE T-URBINE.

APPLICATION FILED AUG.24,1904.

4 SHEETS-SHEET a.

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@ w mw No. 788,006. PATBNTBD APR. 25, 1905. J. WILKINSON.

GOMPOUND MARINE TURBINE.

APPLIOATION FILED AUG.24, 1904.

4 SHEETS-SHEET 4.

UNTTED STATES Patented April 25, 1905.

ATENT Price.

JAMES M'ILKINSON, OF BIRMINGHAM, ALABAMA, ASSIGNOR 'IO WILKINSON 'lURBINE COMPANY, OF BIRMINGHAINI, ALABAMA, A CORPORATION OF ALABAMA.

COMPOUND MARINE TURBINE.

SPECIFICATION forming part of Letters Patent No. 788,006, dated April 25, 1905.

Application filed August 24, 1904. Serial No. 221,986.

To Irl/fomy if 11mg/ con/ecrit.

Beit known thatl, Janes lViLkiNsoN, a citizen of the United States, residing at Birmingham, in the county of Jefferson and State. of

passag'es of each of these latter turbines un- 5o der the control of their respective controller mechanisms. Ihen reversing the vessel, these secondary units become high-pressure Alabama, have invented new and useful Im turbines, the motor-fluid pressure being' adprovements in Compound Marine Turbines, of mitted directly to their high torque-reversing 55 which the following is a specification. workingpassages,whiletheircontroller mech- My invention relates to improvements in a anisms close the forward-driving working pascompound marine turbine the several turbine sag'es. '.lhus being independent, one of these IO units of which are so constructed and coupled latter turbines may operate in series with thel up that I am enabled to secure ina comparatively simple manner and without loss in the efficient action of the motor fluid the requisite variations in speed and power as well as I5 independent control of the several propellershafts necessary for the successful propulsion and steering' of vessels. At the same time l adapt one or more of the turbine units to reverse with high torque.

initial turbine while the other is reversing', 6o or both may operate in multiple, driving the vessel forward, or both may reverso when the high-pressure turbine will be out of service, its only communication with the exhaust or condenser being tln'oug'h the full-speed work- 65 ing passages of the secomlary turbines which are then maintained closed. For cruising motor fluid is admitted to the half-speed work- Having in patents heretofore issued to me ing passages of the initial turbine' to drive shown turbines provided with independent l its propeller-shaft slowly, and the fluid ex- 7o groups of working' passages designed to drive hausting into one or both of the secondary the shaft at two speeds --one representing full turbines will be lower in pressure than when and the other cruising' speedmand having' operating at full speed, so that the speed and shown these turbines adapted to reverse the power of these latter turbines will be reduced.

vessel at half speed or drive it forward at This will effect a relatively slowspeed of pro- 75 cruising speed in addition to their normal or pulsion of the vessel without sacrificing any eration in driving forward at full speed, it is economy in operation. lt will thus be evimy purpose in my present invention to comdent that with a minimum number of turbine these novel types of turbine to provide bines I am able to secure a highly-efficient a multiple or compound marine turbine of action of the steam both to drive the vessel 8O high efficiency and wide range of usefulness at fulland cruisingspeeds and to reverse with which is compact in form and 'apable of behigh power, the several turbines being'of such ing' readily controlled. W'ith this object in a character that they can be independently view I provide a group of three two-speed controlled to secure the necessary independturbines, each of which drives a separate pro ent operation to utilize them in steering' and 85 peller-shaft and is provided with an independmaneuvering the veseel. ent controller mechanism` so that they are A further object of my present invention capable of independent action. Motor fluid is to provide these several turbines with inde- 40 to drive the vessel forward is admitted to the pendent controller mechanisms capable of initialorhigh-pressuretwo-speednon-reversivarying the volume and controlling' the flow 90 ble turbine, with which the sccomlary twoof motor fluid through the several groups of speed reversible turbines are coupled up by working passages of each turbine. The consuitable conduits in what may be termed multroller mechanisms for the reversing-turbines tiple series" e.. a separate conduit leads constitute the subject-mattei' of a pending apfrom the exhaust-head of the high-pressure turbine to the supply-heini of each secondary turbine, from which the pressure has access to the full-speed Vforward-driving working plication, upon which, however, the controller mechanism for the initial turbine is an improvement in that it is adapted to control the admission of motor fluid to either group the supply-head and bucket-Wheel of one of of working passages therein or to both of them simultaneously. The purpose of this is to enable all the working passages to be thrown open to increase the volume of motor iiuid tlowing through the initial turbine to secure an overload power from the secondary turbines. rIhe loss in efficiency in the action of the fluid in the initial turbine is compensated by the increased power and speed derived from the low-pressure turbines.

I simplify the control of the several turbines by providing operating means for their respective controller mechanisms, which can be manipulated from a common point of control.

My invention further comprises the details of construction and arrangement of parts hereinafter described, and illustrated in the accompanying drawings, which form a part hereof, and in which- Figure 1 is a side elevation of my compound marine turbine. Fig. 2 is a top plan view of the same. Fig. 3 is a broken-away view through the reversible turbines, taken to show in section part of the inner and outer working passages. Fig. 4 is a detail sectional view of the bucket-wheel in Fig. 3. Fig. 5 is a view similar to Fig. 3, taken through the two-speed forward-driving turbine. Fig. 6 is a sectional view of the bucket-wheel in Fig. 5. Fig. 7 is a View similar to Fig'. 3 of the other oppositely-acting reversing-turbine, taken, however, through one of the diaphragms to illustrate the similarity of the supply and stage valves of the several turbines. Fig. 8 is a sectional view of the bucket-wheel in Fig. 7. Fig. 9 is an enlarged view of the two-speed forward-driving turbine, partly broken away to illustrate internal construction. Figs. 10 and 11 are similar views of the two reversible turbines. Figs. 12. 13, and 14 show the controller mechanism for the non-reversible turbine in different operating positions, and Fig. 15 is a detail sectional View of the half and full speed nozzles and their valve-controller mechanism. Fig. 16 is a longitudinal sectional view of a controller mechanism along the line ft' Fig. 14. Figs. 17 and 18 are sections along the lines y y and e a of Fig.- 16. Fig. 19 is a sectional view of a modified form of controller mechanism for the reversible turbines.

Similar reference -numerals refer to the same parts throughout the drawings.

The

turbine units

1, 2, and 3 of the battery are preferably arranged as shown'and mounted upon a common bed-plate.

The

turbines

2 and 3 are of the multiplestage reversible type more fully described in Letters Patentissued to me, Nos. 752,496 and 761,866, and here briefly described as comprising an inner casing formed by a plurality of abutting diaphragms 4, provided each with i two rows of reversely-disposed nozzles 5 and l 6, which discharge motor fluid against buckets 7 and 8, respectively, disposed in concentric rows on a bucket-wheel 9 and at different radial distances from the shaft to which the Wheel is keyed. The succeeding nozzle-passages and interposed buckets form inner and outer working passages, which increase in area across stages in proportion with the eX- pansion of the iuid and act with opposite driving effects upon the shaft.

Each wheel 9 carries two parallel rows of buckets 8, between which is interposed a stationary row of intermediateslO. I therefore fractionally abstract the velocity of the motor uid a greater number of times in the outer than the inner working passages, thus securing, when fluid is admitted to the outer passages, a relatively slower rate of speed.

I provide a rotary fluid-actuated valve 11 tol govern the admission of Huid-pressure to each nozzle 5 and similar valves 12 for the nozzles 6. Any suitable controller mechanism, such as that described in the above-mentioned patents, may be used to operate the valves of these

turbines

2 and 3, that shown in the drawings constituting the subject-matter of a pending application. I have, however, illustrated it in connection with the controller mechanism for turbine 1, both mechanisms comprising a casing 13, secured to the side of the outer turbine-shell 14, between which and the turbine-casing is formed an annular fluidpressure-supply chamber 15. This casing 13 has two rows of

openings

16 and 17, which register with openings in the shell leading to

pipes

18 and 19, respectively. These pipes, which are connected through hand-holes 2O in the shell, are disposed around the inner casing and are adapted to communicate with reciprocating fluid-pressure motors 21, seated in the supply-head and diaphragms and having pistons 22, which move both the supply and

stage valves

11 and 12 by means of suitable stems and cranks. The pipes 18 conduct duid-pressure to operate the valves 11 in the outer working passages, while pipes 19 control the valves for the other working passages. Within casing 13 of the controller mechanism for

turbines

2 and 3, which I am now describing, is arotary shell 23, having a single row of openings 24, adapted to register with either 16 or 17. Motor-iuid pressure is admitted to chamber 15 through a port 25 and by a passage 26 from the chamber through an opening leading from a groove 27 into one end of shell 23, which constitutes a cylinder for the controller-piston 28. The shell communicates by an opening 26/ at its other end with port 29 in the casing, which leads to the atmosphere or other low or exhaust pressure. The shell acts as a valve to prevent the escape IOO IIO

IIS

of the pressure in the casing through port 29 suitably geared or connected, and by its position determines the number ofl openings Q4 exposed to the pressure ot' the atmosphere. VIt will be observed that shell 23 is reduced, except where openings 21 lead through it, to leave a clearance. between it and the casing 13, which constitutes a chamber practically surrounding the shell and exposed to the high pressure which is admitted to the easing through opening' 26 from chamber 15. This pressure holds the shell 23 as a valve firmly against the easing 13 to prevent leakage into the openings 16 and 1T or Q9. Then pressure is not supplied to motors 21, springs 31, such as shown in the motors tor the valves of' turbine 1, may be used to open the turbine-valves. Hence in all the turbines the valves of' the working passages controlled by the pipes exposed to the high pressure in the casing will all be held closed, as will also so man y valves ot' the active working passages as have pressure admitted to their motors by the controller-piston Q8. It may be here noted that each

pipe

18 or 19 may bysuitable branches, such as 16' and 1.9/` control a plurality of motors *21 for the valves, admitting fluid to any one ofI the compartments or to all ot' the compartments or to a row or rows of' motors in the line ot' the finids flow across compartments.

By reference to Fig. 1l it will be seen that the tiuid pressure in the supplychamber 15 ofl turbines and 3 is admitted by passages 32, leading through supply-heads to only the nozzles 6 for the outer row of half'- speed-reversing working' passages. The inner row ot supply-nozzles 5 open into the supply-chamber f'ormed by a casing 34, secmed to the end otl shell 14C or to the annular retaining-ring 35, which interlocks with the shell and serves as an abutment to lock head 33 in place. This and all the preceding description applies equally to

turbines

2 and 3, it being noted that their respective shafts 36 and 3T are provided with propellers 3S and 31), designed to rotate in reverse directions while driving the vessel forward. For this reason the corresponding buckets on their respective wheels 9 are reversed, as may be seen by comparing' Figs. 3 and T.

The turbine 1 is also provided with nozzles 5/ and 6/ and valves 11/ and 12' ot' similar construction to the corresponding parts ot' turbinesQ and 3. These, together with buckets T and 8', constitute inner and outer working passages operating to drive the turbine at different speeds; but here all the passages are similarly disposed and act to drive the turbine in but one direction and that forward. The motor-fluid pressure, which is admitted to the supply-chamber l5 through port 10, enters passages 41, leading' inwardly through supply-head 42 to the inlet ends of the supply-nozzles t'or all the working passages, its admission to the inner or the outer row ot' passages, or both, being controlled bya governing mechanism which differs from that already described Vfor turbines 2. and 3 in that the rotary shell 43, which corresponds to Q3, is provided on its under side with a plurality of' circum f'erentially-elongated recesses 1%, formed in the portion through which the openings 24 pass. Each opening' Qsl. opens into one of these recesses, all of' which are sut'- ficiently wide to span both ot' a pair of oppositely-disposed

openings

16 and 17 in the casing 13 when the shell is moved to an intermediate position. The opening 26 in the shell enters one ofl these recesses, which registers with port 29, being in communication therewith throughout the operating positions ot' the shell. 1n this position the high pressure around the shell will not have access to either group of' pipes, and consequently the piston Q8 will simultaneously control the valves of' all the working passages by opening their controller-pipes to the high or exhaust pressure in the shell.

The stem 4:5 of.l the piston projects through a hollow spindle 16, integral with an end ofl the shell 3, and this, with the said spindle 17, projects through suitably-packed openings 18 in the casing 1?), which thus serves as a bearing for the shell. A crank or handle e9 is fixed to the spindle 16, and a packinggland prevents leakage around stem 45. A rack 51 is connected to the outer end et' the stem and meshes with a pinion on a rod 53, mounted in bearings 54 and provided with universal joints, so that it can be operated vf'rom the same point with rodsZ-O, which shif't the controller-pistons for

turbines

2 and 3. lith the same object in view l provide a jointed rod to operate crank L19 from the point of' common control to rotate shell 43 to open either or both ot' the rows otl working passages in turbine 1, and similar means may be used to operate shells Q3. lVhen shell TLS i's moved to either extreme position, it will act in the same manner as shell to cut the inner or the outer working passages out ot' service, while the piston controls the flow of' fluid through the active passages. This method of' control for a two-speed non-reversible turbine l claim, broadly, herein without limitation to any specific mechanism for carrying it into efl'ect. .l also desire to protect hereby the detailed construction of' the controller mechanism `for turbine 1 as a modification of the controller mechanism constituting, broadly, the subject-matterof'a pending application.

Having thus described the independent operation ot' each of the turbine units, .I will now re'f'er to the manner in which they coperate in driving the vessel. Motor-fluid pressure is supplied to turbine 1 through pipes 56, which join and enter port 40. Branch pipes 5T admit pressure to ports f'or

turbines

2 and 3. The Huid-pressure fiowing IOO IOS

IIO

' working passages in turbine l; also, by openthrough the working passages in turbine l is only partly converted into velocity, so that it enters the exhaust-head 58 of that turbine under considerable pressure. From this head 58 lead two

branch conduits

59 and 60 to the supply-chambers 34 of

turbines

2 and 3, respectively. From chambers 34 it Hows under the control of Valves 11 through the inner working passages to the exhaust-heads 61 of these turbines, when it will have been expanded to the atmosphere or condenser pressure. I provide suitable bearings 62 for the

shafts

36 and 37 and also for shaft 63 of turbine 1, which is provided with a propeller 64, designed to drive forward in the same direction as propeller 38.

rIhe controller mechanisms for the several turbines being independent, either

turbine

2 or 3 may be cut out of communication with turbine l by closing the inner row of working passages. Also by admitting initial pressure to the outer working passages of the turbine thus cutoutit will reverse at high torque. All the turbines may be forced, at slight loss in etiiciency in turbine 1, by opening all the ing all the forward working passages in turbine 1 and varying the number open in

turbines

2 and 3 pressure will bank up in turbine l until it practically constitutes a conduit to admit full pressure to

turbines

2 and 3 to increase the speed of rotation. When desired, both

turbines

2 and 3 may be caused to reverse when turbine l will be out of service, due to the fact that all exhaust of pressure therefrom is interrupted by valves 1l. These and other combinations may be effected to secure a wide range and varied character of control for the group of turbines.

Though the motor uid is expanded and the Huid-pressure thereof is fractionally abstracted a greater number of times in the hightorque reversing-passages of

turbines

2 and 3 than in the forward-driving passages, yet since these latter working passages normally operate in series with turbine l the forward and reversing speeds of

turbines

2 and 3 are substantially the same. This enables the proper proportioning of the propellers for most efcient action when driven in either direction.

TheV utilization of valve means to independently close the low-pressure working passages of the secondary turbines enables me to vary the supply of exhaust fluid thereto at highest economy and at the same time to control the flow of motor fluid through the initial turbine by regulating' the exhaust therefrom. In View of the multiple series in which the turbines of the set are grouped this valve control enables me to regulate the cooperation of all the turbines to produce an efiicient and very flexible control for any required speed or power.

Having thus described my invention, what I claim as new, and desire to secure by Letters Patent, is ,n

l. In a set of turbines driving separate shafts, a high-pressure multicellular turbine having full and cruising speed working passages, and one or more turbines coupled up in series with said high-pressure turbine.

2. In a set of turbines driving separate shafts, a high-pressure multicellular turbine having full and cruising speed working passages, and a plurality of turbines coupled up in series with said high-pressure turbine.

3. In a set of turbines driving separate shafts, a high-pressure multicellular turbine having full and cruising speed, forward-driving, working passages, one or more low-pressure turbines having forward-driving working' passages, and means to connect said latter working passages in series with the working ing passages of said high-pressure turbine.

4. In a set of turbines driving independent shafts and having independent working passages, a high-pressure turbine having an exhaust-head, a low-pressure turbine having a supply-head, a conduit between said heads, valve means to control the admission of motor iiuid successively to the several supply-nozzles for the working passages of the low-pressure turbine and to control the exhaust from said high-pressure turbine.

5. In a set of marine turbines driving independent shafts, a plurality of turbines operating in series, the low-pressure turbine or turbines connected to an exhaust or condenser and having a plurality of valve-controlled, motor-iuid-supply passages, and means to ope-n or close said passages to control both the supply to the low-pressure turbines and the exhaust from the high-pressure turbine.

6. In a set of marine turbines operating in series and driving independent shafts, a highpressure turbine, one or more low-pressure turbines having a plurality of motor-iiuid-admission passages, a motor-fiuid-supply chamber or chambers for said passages into which said high pressure turbine exhausts, and means to control the cooperation of the set of turbines by opening or closing said passages.

7. In a set of marine turbines driving different shafts, a high-pressure turbine, one or more two-speed, axial-How, reversible turbines, and means to compound said turbines.

8. A plurality of turbines drivingindependent shafts, a two-speed, non-reversible, highpressure turbine with substantially the same initial and exhaust pressure for both driving speeds, a low-pressure turbine. and means to exhaust the pressure from said high to said low pressure turbine.

9. In a set of marine turbines, ahigh-pressure turbine operating by the instrumentality of different working passages to drive forward at full and cruising speeds, and one or more turbines compounded with said highpressure turbine and adapted to operate as IOO IZO

low-pressure forward-driving turbines and as independent highpressure reversing-turbines, said latter turbines operating in either direction at substantially the same speed and efliciency.

1l). VIn asetof nnilticellular marine turbines driving different shafts, a two-speed, forwardl driving, high-pressu re turbine, a low-pressure forward-driving turbine adapted to reverse at high torque, and means to connect said turbines so that they operate in series in driving forward.

l1. ln a setof marine turbines, a high-pressure turbine, one or more turbines having axially-disposed forward and reversing working passages, means to supply high pressure to said reversing working passages and to said high-pressure turbine` and means to exhaust the pressure from said latter turbine into the forward-driving working passages of said reversible turbines.

1Q. ln a setof marine turbines drivingI different shafts. one or more multieellular reversible turbines having independent working passages, a high-pressu re turbine, connections 1 to direct the motor fluid in series from said high-pressure turbine through the low-pressure working passages of said reversible turbine or turbines, and means to admit a high pressure to the otherl working passages of said latter turbine or turbines.

13. ln a set of marine turbines driving different shafts, a high-pressure two-speed nonreversible turbine, two or more axial-flow high-torque reversible turbines, conduits to connect said turbines with said high-pressure turbine so that they ope-rate in series therewith in driving forward, and means to admit high pressure to the high-torque reversingpassages of said reversible turbines.

la. In a set of compound axial-flow turbines, an initial high-pressure, forward-driving, turbine having working passages for driving a propeller-shaft at full speed, and working pass-ages for driving said propellershaft at a lower speed, a secondary turbine having low-pressure working passages connected up in series with said initial turbine, and high-pressure, high-toupie` reversingpassages, and means to control the admission of motor fluid to the working passages of said turbines.

15. In a two-speed forward-driving turbine, high speed working passages, low speed working passages, means to close one set of passages while controlling the admission of pressure to the other set. said means being also :alapted to control the admission simultaneously to both sets of working passages.

16. lna two-speed forward-driving turbine, one or more working passages operating efliciently to drive the turbineat full speed, one or more working passages operating efficiently to drive the turbine at a low speed,

means to cut said working passages into or out of service, and a controller mechanism for said means adapted to control either the full or low speed passage or passages, while cutting the other passage or passages out of service, and to control the admission of motor fluid to the working passages `for both driving speeds to compensate overload conditions.

1T. In a set of marine turbines, an initial high-pressure turbine operating in'series with one or more low-pressure turbines, said highpressure turbine comprising independent working passages to drive its propeller-shaft at two speeds in the same direction, and a controller means which varies the admission of Inotor fluid to high or low speed working passages under normal-load conditions, and which admits motor fluid under control to all of the working' passages under overload conditions.

18. ln a set of marine turbines, an initial highpressure turbine provided with independent groups of Vfull and cruising speed working passages, means to control the admission of high pressure to either or both of said groups of passages, and one or more lowpressure turbines adapted to operate in series with said high-pressure turbine.

19. 1n a turbine adapted to drive a propeller-shaft efficiently' at full and cruising speeds, working passages for effecting said driving speeds, and means to control the admission of pressure to said passages either independently or jointly, one or more secondary turbines having working passages coupled up in series with said two-speed turbine, and means to control the admission of pressure to the several working passages of said secondary turbine or turbines independently.

20. The combination of a compound turbine operating by stage expansion and having two independent working passages adapted t0 drive the turbine forward and comprising means to fractionally expand the motor fluid and abstract the velocity thereof a greater number of times in one than in the other of said passages, means to control the admission of motor fluid to either or both of said working passages, with one or more turbines operating in series with said first-mentioned turbine.

21. A turbine having two independent sets of working passages designed to drive the turbine at different speeds of rotation by the intel-position of a greater number of rows of buckets in one than in the other of said sets of working passages, a controller mechanism adapted to control the admission of motor fluid to either set of working passages while closing` the other, one or more secondary turbines operating in series with said first-mentioned turbine, and means to admit an overl load supply of motor fluid to said set of tur- IOO bines by admitting motor iiuid to both sets of working passages in said first-mentioned turbine. A

22. In combination with a multicellular turbine having working passages at different distances from its shaft center, the working passages being adapted to drive the turbine forward at different speeds. one or more secondary turbines having working passages at different distances from its shaft center, one set of said working passages operating in series with either or both of the working passages of said iirst-mentioned turbine, and means to admit high pressure to the other working passages of said latter turbine or turbines for the purpose of reversing it or them at high torque.

23. In an elastic-fluid turbine, two sets of nozzle-passages at different distances from the shaft center, different sets of rotatable buckets coperating with said sets of nozzles, independent valves for controlling the flow of motor fluid through said nozzles, in combination with a controller mechanism adapted to close one set ot' nozzle-passages, while controlling the flow of motor fluid through the other set, and to simultaneously-control the volume of motor fluid flowing through both sets of nozzle-passag'es and discharged thereby against said rotatable buckets.

24. In an elastic-fluid turbine, two sets of nozzle-passages, two independent sets of rotatable buckets cooperating respectively with said sets of nozzles, one set of nozzles and cooperating buckets being adapted to drive the turbine efficiently at a lower rate of speed than the other set of nozzles and cooperating buckets, fluid-actuated valve means to cut the nozzle-passages of each set out of service, and a controller mechanism for said valve means which is adapted to simultaneously control the volume of motor fluid discharged through said nozzle passages against both sets of buckets.

In testimony whereof I have hereunto set my hand in presence of two subscribing witnesses.

JAMES WILKINSON.

Witnesses:

Noma WELSH, H. M. HARToN.