US903454A - Elastic-fluid turbine. - Google Patents
Elastic-fluid turbine. Download PDFInfo
- Publication number
- US903454A US903454A US42877708A US1908428777A US903454A US 903454 A US903454 A US 903454A US 42877708 A US42877708 A US 42877708A US 1908428777 A US1908428777 A US 1908428777A US 903454 A US903454 A US 903454A
- Authority
- US
- United States
- Prior art keywords
- bucket
- groove
- turbine
- elastic
- partition
- 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.)
- Expired - Lifetime
Links
Images
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
- F03B—MACHINES OR ENGINES FOR LIQUIDS
- F03B1/00—Engines of impulse type, i.e. turbines with jets of high-velocity liquid impinging on blades or like rotors, e.g. Pelton wheels; Parts or details peculiar thereto
- F03B1/04—Nozzles; Nozzle-carrying members
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/4932—Turbomachine making
- Y10T29/49321—Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member
Definitions
- This invention relates to improvements in elastic fluid turbines.
- the objects of my'invention are: first, to increase 'the efficiency-moi elastic fluid turbines bv a more effective form of the buckets in combination with the nozzle; second, to lessen the cost of construction both in the economizing of material and in lessening the labor cost of production; third, to provide a construction which is readily assembled and disassembled, and in which' injured parts can be quickly substituted or repaired; and fourth, to improve the specific details of construction of the bucket.
- Figure 1 is a sectional view transversely throu h the rim of a turbine, showing a detail of the rough blank in the first step of the rooess of manufacturing the buckets of my improved turbine, the view bein Y taken on a plane indicated by the section l-fines ZZ of Figs. 6 and 7.
- Fig. '2 is a similar sectional view showing the-next step of the-method of manufacture in which the annular groove for the buckets has been formed in the blank.
- Fig. 3 is a similar sectional vicw, showing the groove formed for receiving and seating the partition walls between the buckets.
- Fig. 1 is a sectional view transversely throu h the rim of a turbine, showing a detail of the rough blank in the first step of the rooess of manufacturing the buckets of my improved turbine, the view bein Y taken on a plane indicated by the section l-fines ZZ of Figs. 6 and 7.
- Fig. 4 is a detail elevation view of one of the said partition walls or plates.
- Fig. 5 is a detail sectional view similar to that appearing in Fi it. 2 and 3, except that the rim of the tur nor is laid on its side, showing the partition nulls in place in the lllll.
- Fig. (3 is a detail View of a portion of the rim of a turbine and nozzle in position, being a. side elc- .vation looking squarely at the side into the buckets.
- Fig. 7 is a. detail sectional view of the structure as appearing in Fig. 6, taken or. a lane corres onding to the curved line X--l of Fig. 6, coking in the direction of the little arrow.
- Fig. 8 shows a modified arrangement of the turbine wheel with the buckets on the periphery in place of on the face; and
- Fig. .9 is a cross section throughthe turbine nozzle 10.
- a bucket segment or ring 1 is formed in-the manner usual with my construction of elastic fluid turbine engine with a suitable shank with bolt hole therethrough for attachment to the central disk nothere shown.
- This broad groove 2 is read-- ily turned outafter the'turbine wheel has been assembled with the ring 1, either a full or segmental ring. After this has been done,
- I cut grooves 4 transversely across the ann'ular bucket groove at an angle of about 20 degrees, by a suitable rotary cutter.
- the ellipse is of such form that when the cutter is set atan angle of 20 degrees it forms a true circle, so that the tool cuts an even groove out of the back wall.
- This tool in cutting the metal, turns up a thin bur.
- the buckets are 'formed by inserting semicircular pieces of sheet metal 7 with lugs 5 formed at: the upper outer angle within the groove 4.
- a. bin S is raised around the edge of the some from the action of the punch, which bur I :nn careful to preserve on this sheet metal partition wall. It is utilized in the proper securing of the said partition wall within the bucket groove 2.
- 'lhcsemi-circular partition wall7 is inserted in the groove with the *kted down intothe' notch 5, whenthe partifirst I tam theminsuitable slots.
- ' ring may be roughly formed to shape'an Y ,tion walls can then be inserted by the action ofa light tool, forming a comparatively indicated in Figs. 5 and 6.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Description
G. W. DAKE. BLASTIG'FLUID TURBINE. APPLICATION FILED APB.23,1908.
903,454. Patented Nov. 10, 1908.
E EI 1 5"- F a g 3 5' I 4 WITNESSES" f INVENTOIR. ma v 2 .2 2;
A Ira/m5 K.
UNITED STATES PATENT OFFICE. v
OHARLES W. DARE, OF GRAND RAPIDS, MICHIGAN, ASSIGNOR TO THE BAKE-AMERICAN STEAM TURBINE UUMFANY, (IF GRAND RAPIDS, MICHIGAN.
Ensure-rum: runnmn.
Specification of Letters latent.
Patented Nov. 10, 1903.
To all whom it may concern:
Be it known that I, CHARLES \V. Dane, 11.
' citizen of the United States, residing at the city-of Grand Rapids, county of Kent, State of Michigan, have invented certain new and useful Improvements in Elastic-Fluid Turbines, of which the following is a specification. a
This invention relates to improvements in elastic fluid turbines.
The objects of my'invention are: first, to increase 'the efficiency-moi elastic fluid turbines bv a more effective form of the buckets in combination with the nozzle; second, to lessen the cost of construction both in the economizing of material and in lessening the labor cost of production; third, to provide a construction which is readily assembled and disassembled, and in which' injured parts can be quickly substituted or repaired; and fourth, to improve the specific details of construction of the bucket.
Further ob'ects will definitely appear from the detai ed description to follow.
I accomplish the objects of; my invention by the devices and means described in thefollowing specification.
The invention is clearly defined and pointed out in the claims.
In the accompanying drawing I illustrate such parts of an elastic fluid turbine as are necessary to the ,pro er understanding of my invention, in whic Figure 1 is a sectional view transversely throu h the rim of a turbine, showing a detail of the rough blank in the first step of the rooess of manufacturing the buckets of my improved turbine, the view bein Y taken on a plane indicated by the section l-fines ZZ of Figs. 6 and 7. Fig. '2 is a similar sectional view showing the-next step of the-method of manufacture in which the annular groove for the buckets has been formed in the blank. Fig. 3 is a similar sectional vicw, showing the groove formed for receiving and seating the partition walls between the buckets. Fig. 4 is a detail elevation view of one of the said partition walls or plates. Fig. 5 is a detail sectional view similar to that appearing in Fi it. 2 and 3, except that the rim of the tur nor is laid on its side, showing the partition nulls in place in the lllll. Fig. (3 is a detail View of a portion of the rim of a turbine and nozzle in position, being a. side elc- .vation looking squarely at the side into the buckets. Fig. 7 is a. detail sectional view of the structure as appearing in Fig. 6, taken or. a lane corres onding to the curved line X--l of Fig. 6, coking in the direction of the little arrow. Fig. 8 shows a modified arrangement of the turbine wheel with the buckets on the periphery in place of on the face; and Fig. .9 is a cross section throughthe turbine nozzle 10.
In the drawing,. similar numerals of'reference refer to similar parts throughout the several views.
Considering the numbered parts drawing, a bucket segment or ring 1 is formed in-the manner usual with my construction of elastic fluid turbine engine with a suitable shank with bolt hole therethrough for attachment to the central disk nothere shown. In the face of this segment or ring, I cut a roove 2 which is in form one-half 'of an elipse, the ellipse being divided on the long axis. This broad groove 2 is read-- ily turned outafter the'turbine wheel has been assembled with the ring 1, either a full or segmental ring. After this has been done,
of the I cut grooves 4 transversely across the ann'ular bucket groove at an angle of about 20 degrees, by a suitable rotary cutter. The ellipse is of such form that when the cutter is set atan angle of 20 degrees it forms a true circle, so that the tool cuts an even groove out of the back wall. This tool, in cutting the metal, turns up a thin bur. After the groove is'cut, I cut a notch 5, which is a continuation of the groove 4 out through the edge of the outer portion of the ring to receive a lug on the bucket partition wall.
The buckets are 'formed by inserting semicircular pieces of sheet metal 7 with lugs 5 formed at: the upper outer angle within the groove 4. When these se1nicirculardisks are punched from a sheet of metal, a. bin S is raised around the edge of the some from the action of the punch, which bur I :nn careful to preserve on this sheet metal partition wall. It is utilized in the proper securing of the said partition wall within the bucket groove 2. 'lhcsemi-circular partition wall7 is inserted in the groove with the *kted down intothe' notch 5, whenthe partifirst I tam theminsuitable slots.
' ring may be roughly formed to shape'an Y ,tion walls can then be inserted by the action ofa light tool, forming a comparatively indicated in Figs. 5 and 6.
-' elastic fluid-most efl'ectively into the buckinet'al bucket partitions, which are made proper strength onlybeingrequired.
'inserted' in transverse grooves bent .by'the rubbing action of a tool, somewhat like the spinning of metal, to engage the bur on the semi-circular partition plateand this very eflectively retains the said artition in place. The lug 5' is then rivt-ion wall is'efiectively and safely held in place. When this is done, the turbine wheel isput intoallathe" and the partition walls turned oil to' make them even, and a broad notch' 7 is formed in the same towards the receiving end .of the bucket, the discharge end of the bucket being indicated at 6. The
osition of this bucket partition 7 is clearly A nozzle 10 with itsend' cut'oblique is arranged in this broad'notch 7 to deliver the ets, and, as this construction enables Very .thin partition-walls to be placed between the buckets, the bucket capacity of a turbine is correspondingly increased and the angle of the nozzle and the position which it occupies, projecting into the notch, enables the elastic fluid to be thus delivered most eflect- The result is a very marked increase efiicieny of the entire engine.
In Fig. 8,'I' have shown how thebuckets can be arranged on the peripherv-of a turbinewheel, in which event I refer to form lugs 5 on both sides of'the ucket and re From this de scription it will-be seen that the hue 'e turned true. The bucket groove'2. may then be formed therein by the use of a heavy tool, cutting the metal very rapidly; .The partishallow groove to receive the thinflsheet from punchings. The pnnohings should not be finished, because the buris utilized as a partof. the attaching means. This forms the buckets very economically and very ef fectively, andby then shaping the buckets with the broad notchto receive theobIique-r ended no'zzle, the fullbucket capacity and the most eifective delivery of elastic fluidis secured. Aside'froni economy in construc: tion, greater efliciency in the elastic fluid turbine is thus secured. The partitions 7 can bereadily withdrawn and repaired or new ones -in serted,'a tool of Having thus des ibed my invention, what I claim as ne'wan desire to secure by Let-' ters Patent is: v v
- 1*. In an elastic fiuidturbine, the combination of the turbine wheel, wi h' a -bjucket ring with an annular groove to 10d therein of semi-elliptical cross section on the long axis; seirsi c irc iar rest metal basket rtitiens in tlie'bucket into a notch inthe .w purpose specified.
groove and set at .an angle theret f Said" sheet metal partitions having-a bur formed on their edgbe and being retained by coinpressing" the ur on the edge of the said transv rse groove against the same, the saidpar tit" ts having a lug extending to one side and riveted'into a suitable notch, t e said 'bucket-s'partitions having a broad not" h 7 in their nee edges; and a nozzle with its. end
cut oil obliquely ,to', conform to the said notch, coacting substantially as described and for the purpose 5 ecified.
2. In anelastlc flui 'turbine,'thecombination of the turbine wheel, with 'a bucket' -ring with an annular bucket groove formed;
thereinsemi-elli tical in cross section on the long. axis 0 the ellipse; substantially semi-circular sheet metal bucket partitions inser ed at an angle in the'said bucket" groove and ret-ainedthere by suitable means,
a broad notch being formed inthe free ed e of the'sai'd' partitions; and a suitable nozzle with its end cut off oblique to; conform 'to the said notclrin said .partition's, coacting substantially: asdescribed and for the 'fpurpose specified.
3.111 an elastic turbine, the'combina -i tion of the turbine-wheel with a bucket ring with an annular buck t groove formed theret'ransverse 'to'the said-bucket groove in a suitable notch'in the, wall thereof; a burformed on the said sheet metal a-rtition, enagedbyva bur on the ed e 0 ,the groove, eing compressed against t e same, coac'ting 4; .In an elastic fluid turbide the combination 'of'theturbine wheel with a bucket, ring with an annular bucket groove formed there in; a sheet metal bucket partition arranged transverse to the said .bucket. groove in a suitable 'notc ,formed on the said sheet metal aged by a bur on the edge 0 ei'ng compressed a ainst thesame, an expartition, en-
tension .or lug of t e said partition beingriveted, into a notchnin the wheel, coacting forthe purpose specified. 5. In an elastic fluid turb ne, the combination of the turbine wheel with a bu'cket'ring I I with an annular bucket groove formed: there I ingja sheetinetal bucket-partition arranged.
the groove, I
in; a sheet metalibuc et partition'arranged in a the wall thereof; a bur transverse to the said Y bucketzgroove a' suitable notch in the wall thereof, an extension or lug of the said artition beingrriveted In witness whereof, I my hand and seal inlthe presef ceuo witnesses, p a;
CHARLES BAKE. -[i..s'.]
Witnesses: r
wa s. a Jngr NI; rm-swearin eel, coaeting for the
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US42877708A US903454A (en) | 1908-04-23 | 1908-04-23 | Elastic-fluid turbine. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US42877708A US903454A (en) | 1908-04-23 | 1908-04-23 | Elastic-fluid turbine. |
Publications (1)
Publication Number | Publication Date |
---|---|
US903454A true US903454A (en) | 1908-11-10 |
Family
ID=2971881
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US42877708A Expired - Lifetime US903454A (en) | 1908-04-23 | 1908-04-23 | Elastic-fluid turbine. |
Country Status (1)
Country | Link |
---|---|
US (1) | US903454A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2505820A (en) * | 1945-02-28 | 1950-05-02 | Borg Warner | Means for assembling and retaining radially disposed vanes |
US3081528A (en) * | 1958-05-09 | 1963-03-19 | Arthur W Hanna | Method of manufacturing female electrical sockets |
-
1908
- 1908-04-23 US US42877708A patent/US903454A/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2505820A (en) * | 1945-02-28 | 1950-05-02 | Borg Warner | Means for assembling and retaining radially disposed vanes |
US3081528A (en) * | 1958-05-09 | 1963-03-19 | Arthur W Hanna | Method of manufacturing female electrical sockets |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2641440A (en) | Turbine blade with cooling means and carrier therefor | |
US2640679A (en) | Turbine or compressor stator ring | |
US1749528A (en) | Blading for reaction turbines | |
US2790620A (en) | Multiple finger dovetail attachment for turbine bucket | |
US903454A (en) | Elastic-fluid turbine. | |
US1366605A (en) | Blade-securing means and method of making the same | |
US1470506A (en) | Method of manufacturing turbine elements | |
US926442A (en) | Turbine-bucket. | |
US1073623A (en) | Steam-turbine blade. | |
US764230A (en) | Wheel for steam-turbines. | |
US1362853A (en) | Turbine-wheel and bucket-mounting | |
US532232A (en) | de laval | |
US995367A (en) | Steam-turbine. | |
US764452A (en) | Turbine-bucket cover. | |
US924546A (en) | Turbine. | |
US1307082A (en) | Josee y | |
US809277A (en) | Turbine. | |
US1187448A (en) | Steam-turbine. | |
US1266973A (en) | Nozzle construction for elastic-fluid turbines. | |
US874443A (en) | Steam-turbine. | |
US961329A (en) | Turbine-blade. | |
US840457A (en) | Steam-turbine. | |
US880365A (en) | Elastic-fluid turbine. | |
GB190724870A (en) | Improvements in and relating to the Vanes of Turbines | |
US1762361A (en) | Turbine blade |