US997635A

US997635A - Gearing for turbines.

Info

Publication number: US997635A
Application number: US57006210A
Authority: US
Inventors: Charles Algernon Parsons
Original assignee: Individual
Current assignee: Individual
Priority date: 1910-07-02
Filing date: 1910-07-02
Publication date: 1911-07-11
Anticipated expiration: 1928-07-11

Description

G. A. PARSONS. GEARING FOR 'IV'URBINES. APPLICATION FILED TULY2, 1910.

Patented July 11, 1911.

-3 SHEETSSHEBT 1.

G. A. PARSONS. GEARING FOR TURBINES.

APPLIUATION FILED JULY 2,1910. 997,635., Patented July 11,1911.

3 SHEETS-SHEET 2.

Fig.1.

G. A. PARSONS.

GEARING FOR TURBINES. APPLICATION FILED JULYZ 1910.

Patented July 11, 1911.

3 SHEETS-SHEET 3.

Figm.

s'rarus Ar rib.

s GEARING FOR TURBINES.

To all whom it may concern:

Be it known that I, CHARLES ALGERXON Paasoxs, a subject of the King of Great Britain and Ireland residing at Heaton \Yorks, Xewcastle-upon-Tyne, in the county of Northumberland, England, have invented certain new and useful Improvements in and Relating to Gearing for Turbines and the Like. of which the following'is a specification. I

This invention relates to gearing for turbines and the like. A

It has already been proposed to group together a number of separate turbines. and to fit the ends of their shafts with pinions. each pinion gearing with a single wheel mountedon a common shaft. Such turbines have also been arranged to receive the steam in series. but they have only been arranged to run at the same speed.

The object of the present invention is to provide an arrangement of turbines as indicated above inwhich the energy of the working fluid is utilized to the best advantage.

To this'end the invention consists in designing each separate turbine in relation to its most economical speed, and then arranging 'the differently speeded turbines suitably to drive the common shaft.

Further, the invention may be applied for a similar purpose to ship propulsion sys tems having one or more astern turbines. and in which one or more special turbines known as cruising turbines are added for cruising purposes.

Thus the invention also consists in a'rranging such cruising or astern turbines to drive through gearing shafts to which the other ormain turbines are coupled direct. such gearing being adapted to allow the cruising or astern turbines to rotate at their most efficient speed. In some casessuch cruising turbines or even the main turbines may be arranged to drive the propeller shaft, through double reduction gearing. By this means it ispossible to run the turbines at their most economical speed withoutinvolving too great a reduction in a single gear with the consequent practical difiiculties occasioned thereby.

This invention is equally applicable to turbines of the Parsons, impulse or mixed Parsons and impulse type. as by means of single or double reducing gear, such turbines or turbine parts can be run attheir most Specification of Letters Patent.

Patented July 11, 1911.

Application filed July 2, 1910. Serial No. 570,062.

economical speed. Further, the turbine ele ments on one or more shafts may be cross coupled or by-passed in whole or in part in any suitable manner. If desired, clutches of any convenient type may be used to disconnect the cruising or astern turbines at high speeds or when not in operation.

The invention further consists in the improved turbine arrangements hereinafter described.

Referring now to the accompanying drawings, which represent the invention as applied to marine propulsion and are diagrammatic only. Figures 1 and 2 represent in plan and end elevation a two propeller shaft installation with single reduction throughout. Figs. 3 and i show a fourshaft installation. Figs. 5 and 6 show a three-shaft installation.

-..In the illustrations it will be noted that no supports have been shown for the various turbine shafts as these do not form part of the present invention.

.In carrying this invention into effect according to one manner, I arrange that the pressure drop of the working fluid shall be distributed in a known manner over a number of turbines. for instance. as shown in Figs. 1 and 2, over one high pressure tur bine A. one intermediate pressure turbine B and one low pressure turbine C. The arrangement in these figures show two such sets of turbines. Each'of the turbines A and B is mounted on' a separate shaft 0 which carries a pinion b gearing with a large wheel 0 mounted on the propeller shaft (I. A condenser e is also provided for each set of turbines and an astern turbine D is mounted on a separate shaft a which also carries a pinion b gearing with the large wheel a. 'hen such an installation is arranged for ahead running the steam enters the high pressure turbine A and as indicated by the arrows. flows through the intermediate pressure and low pressure turbines B and C respectively and thence to the condenser e, the turbines A, B and C thus being in series. During astern running. steam is admitted to the astern turbine D which exhausts directly to the condenser 6 while for maneuvering purposes it will be seen that the turbines on one side .of'the ship may be running ahead while the remaining turbines are arranged for astern running.

The arrangement shown in Figs. 3 and 4 represents a four shaft installation in which 1 ner.

a high pressure turbineAis mounted on-each of the side propeller shafts d and a low pressure turbine C upon the' central propeller shaft. High and low pressure astern turbines 5 D-and G are also provided as shown on the side and central shafts, both ahead and astern high andthe low pressure turbines being mounted directly "on propeller shafts and therefore driving in the ordinary man- On an extension of the central shaft is provided a gear wheel 0, with which engage the pinions b 0n the shaft a of the cruising turbine E. Bythis means the cruising turbines can be made to rotate at their most efficient speed. Suitable. clutches may be provided to disconnect such cruising turbines when not in operation, thus avoiding any drag upon the propeller shaft d. For cruising speeds, steam is supplied to the cruising turbine E and passed in series through the turbine A, and thence to the condenser e as indicated by arrows, while for higher speeds the cruising turbine E is disconnected and steam is supplied directly v to the (turbine A. F or astern running, the

steam fiows through theturbines D and G in series as. indicated.

In Figs. 5 and 6 there is shown a threeshaft installation suitable/for a torpedo boat. The high pressureturbine'Aand in-- termediate turbine B in this case are mounted directly on the wing ropeller shafts and the low pressure turbineg is mounted directly on the central shaft. A cruising turbine E and an astern turbine" D1 are shown in gear with the wheels 0 mounted on the cen- These latter turbines can beeither permanently coupled to the central tral shaft.

shaft or suitable clutches may be provided to 40 disconnect them when not in-operation. The power can be distributed over various shafts in any desired manner, for instance,

the power developed by the central shaft may be arranged to be about double that developed on-each of the wing shafts.

- At cruising speeds the arrangement shows that steam flows through turbines E, A, B

and C'to the'condenser e, the steam being supplied directly to theturbine A for higher powers; while for reversing, the turbine D by-passed. The larger the number of sep- "Karate turbines the easier it is to obtain any desired grouping. The diameterof the pinion b is so chosen in relation to the diameter of the large wheel 0 with which. the pinio'ns engage and in relation to thespeed of rotation of the propeller shaft that each separate turbine shall 'run at its most economical speed of rotation. Thus the high pressure turbine would be designed for a As shown inthe accompanying drawings, I

an astern turbine may be provided either separately mounted or incorporated with another turbine-and this astern turbine may be designed with reference to its most economical speed and is suitably geared to the propeller shaft. As has before been stated suitable clutches, either mechanical or-- electrical, may be providedto disconnect the cruising or astern-turbines when required.

It will be seen that the present invention is in no way limited to the number of tur-' bines or to the number of shafts or to the manner in which the various turbines are grouped, the various arrangements described whole of the cruising and high pressure turaction type or a combination of impulse and reaction. Suitable arrangements are also provided for absorbing the thrust on the turbine shafts, such as balancing or dummy pistons arranged within the turbine or by providing suitable thrust blocks on the tur bine shafts. Or balancing may be provided for in other known ways or effected by the thrust of the gear. H

By this invention I am enabled to obtain the highest economy for ships under all conditions and also it facilitates the design and I constructions of a turbine to obtainthe high- .est degree of efficiency as already explained.

It will be seen that many modifications can be made in the manner of carrying this invention into effect without .in anyway departing from-the spirit of the same. y l Having now described my invention what I claim as new and desire to secure by Letters Patent is .1. marine turbine installation comprising in combination one-or more propeller shafts, a plurality of other shafts, gearing means between said shafts, and turbine ele- Y 2 mentssome of which are reversing turbine elements distributed over all ofsa-id shafts whereby said turbine elements can' be ar ranged to run at their most economical. speed independently of the speed of the propeller shafts.

2. A marine turbine installation comprising in combination one or more propeller shafts, a plurality of othershafts, low pressure turbine elements mounted on all of the pro eller shafts and high pressure turbine elements on the other shafts, gearing means 90 herein being examples only. Part of the I between said shafts whereby said turbine elements can be arranged to run at their most economical speed independently of the speed of. the propeller shafts.

3. A marine turbine installation comprising in combination one or more propeller shafts, a plurality of other shafts, low pressure turbine elements mounted on all of the propeller shafts, and high pressure turbine elements on the other shafts, reversing turbine elements on some of said shafts, and gearing means between said shafts whereby said turbine elements' can be arranged to run at their most economical speed independently 'of the speed of the propeller shafts.

4. A marine turbine installation comprising in combination one or more propeller shafts, a plurality of other shafts, an ahead and astern turbine element mounted on each of the propeller shafts and higher pressure turbine elements on the other shafts, gearing means between said shafts whereby. said turbine elements can'be arranged to run at their most econo ical speed independently of the speed of the propeller shafts.

5. A marine turbine installation comprising in combination one or more propeller shafts, a plurality of other shafts, low pressure turbine elements mounted on the 'propeller shafts, and cruising and high pressure turbine elements on the other shafts, gearing means between said shafts whereby said turbine elements can be arranged to run at their most economical speed independently of the speed ofthe: propeller shafts.

6. A marine turbine installation comprising in combination one or more propeller speed independently of the speed of the proshafts, a plurality of other-shafts, low pres; sure turbine elements mounted on the propeller shafts, and cruising and high pressure turbine elements on the other shafts, astern turbine elements on some of said shafts and gearing between said shafts whereby said turbine elements can .be arranged to run at their most economical peller shafts.

7. A marine turbine installation comprislng 1n combmatlon one or more propeller= shafts, a plurality of other shafts, combined ahead and astern turbine elements mounted shafts.

on the propeller shafts, cruisinghigh pressure turbine elements on the other shafts, and gearing means between said shafts whereby saidturbine elements can e arranged to run at their most economical speed independently of the speed of the propeller shafts.

8. A marine turbine installation comprising in combination one or more propeller shafts, a plurality of other shafts, combined ahead and astern turbine elements mounted on the propeller shafts, cruising high pressure turbine elements on the other shafts, and gearing means bet-ween said cruising turbine shafts and the propeller shafts whereby said turbine elements can be arranged to run at their mosteconomical speed independently of the speed of the propeller 9. marine turbine installation comprising in combination one or more propeller shafts, a plurality of other shafts, low pres sure turbine elements mounted on' some of the propeller shafts, cruising turbine elements-and high pressure and reversing tur bine elements distributed over the other shafts, and gearing means between the latter shafts and the propeller shafts whereby said turbine elements can be arranged to run at their most economical speed independently of the speed of the propeller shafts. t I

10. A marine turbine installation'comprising in combination one or more propeller shafts, a plurality of other shafts, low pres- ,Sure turbine elements mounted on 'some of the propeller shafts, cruising turbine ele- CHARLES ALGFlRNON PARS 0N8.

Witnesses:

FREDERICK GORDON HAY Bnorom), WILLIAM SHEARER.