US735889A - Steam-turbine. - Google Patents
Steam-turbine. Download PDFInfo
- Publication number
- US735889A US735889A US13833403A US1903138334A US735889A US 735889 A US735889 A US 735889A US 13833403 A US13833403 A US 13833403A US 1903138334 A US1903138334 A US 1903138334A US 735889 A US735889 A US 735889A
- Authority
- US
- United States
- Prior art keywords
- wheel
- channel
- steam
- opening
- inlet
- 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
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/30—Exhaust heads, chambers, or the like
Definitions
- Reaction steam-turbines having circumferential discharge of steam through openings between buckets may be combined with a channel disposed in the wheel-casing and surrounding the wheel discharge-outlet. Said channel then receives the exhaust from the wheel and operates to increase the efficiency of the steam, as fully described in my patent applications Serial Nos. 85,747 and 87,346. Ihave found that when the channel at its inlet is of a Width (measured in the direction of the axis of rotation of the wheel) equal to that of the Wheel discharge-outlet slight lateral movements of thewheel (similarly measured) are apt to impair the said efficiency.
- My invention has for its object the prevention of this difficulty; and it consists in constructing the channel inlet aforesaid of greater width than the wheel-outlet, so that it extends beyond the latter on both sides, and then converging the sides of the channel form this inlet, so that at a point farther outward radially they reach a width about equal to that of the discharge-opening.
- Figure 1 is a section of the outer portion of a reaction turbine-wheel with a channel in ,its casing, the cross-section of said channelincreasing in the direction of the steam-jet, as fully de scribed in aforesaid applications, the parts being in the positions which they assume when the wheel is symmetrical with reference to said casing.
- Fig. 2 represents the same parts, the wheel, however, no longer being symmetrically disposed in its casing, but shown as havingmoved laterally to the left of the figure.
- A represents a portion of the wheel, body formed by the heads B O, united by crossbolts, one of which is "shown at D.
- Circumferentially around the. wheel is formed the exhaust-opening E, through which the steam escapes between buckets, one of which is represented at F.
- G shows a part of the wheelcasing in which is the chamber H, in which the wheel A rotates. Said'chamber communicates with the annular passage or channel I, the cross-sections of which increase,- as above mentioned.
- said increasing is such that thewalls a'b diverge outwardly, so that'the width of the passage (measured in the direction of the axis of rotation of the wheel) is greater at its outlet than at its inlet at L.
- the channel I is provided with an inlet portion or nozzle, the side walls e f of which converge from its mouth K in the chamber H to'the point L of the channel I, said mouth or inlet-opening (similarly measured) being wider than the exhaust-opening E, so that the opposite edges of said opening overlap the sides of the inlet by equal distances 8 d.
- the opening at L thus becomes the true channel-opening, so far as the function of the channel itself is concerned.
- the converging portion from L to K has no effect on the action of said channel, but simply permits of the lateral displacement of the wheel without causing the production of an abrupt shoulder or the narrowing of the entrance.
- the escaping jet (indicated by. the dotted lines) moves in the direction of the arrow straight from the wheel exhaust-opening to the channel-aperture at L. If, howeveiythe wheel be laterally displaced, as illustrated in Fig. 2, it is obvious that the enlarged opening K permits the jet to enter unobstructed and pass to and through the opening L in a direct course.
- an annular channel surrounding said I width of said channel is reduced to about the Width of said Wheel discharge-opening, substantially as described.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Turbines (AREA)
Description
T. G. E. LINDM/ARK.
STEAM TURBINE.
APPLICATION FILED JAN. 9, 1903.
WITNESSES PATENTED AUG. 11, 1903.
.I. Q. V
INVENTOR Patented. August 11, 1903. I
PATENT OFFICE.
TORE GUS'IAF EMANUEL LINDMARK, OF STOCKHOLM, SWEDEN.
STEAM-TURBINE.
"SPECIFICATION forming part of Letters Patent No. 735,889, dated August 1 1, 1903. Application filed January 9, 1903. Serial No.138.334. (No model.)
To aZZ whom it may concern:
Be it known that I, TORE GUSTAF EMANUEL LINDMARK, a subject of the King of Sweden and Norway, residing at Stockholm, Sweden, have invented a new and useful Improvement in Steam-Turbines, of which the following is a specification.
Reaction steam-turbines having circumferential discharge of steam through openings between buckets may be combined with a channel disposed in the wheel-casing and surrounding the wheel discharge-outlet. Said channel then receives the exhaust from the wheel and operates to increase the efficiency of the steam, as fully described in my patent applications Serial Nos. 85,747 and 87,346. Ihave found that when the channel at its inlet is of a Width (measured in the direction of the axis of rotation of the wheel) equal to that of the Wheel discharge-outlet slight lateral movements of thewheel (similarly measured) are apt to impair the said efficiency. This is due to the fact that as soon as the wheel thus becomesdisplaced not only does the actual effective inlet become contracted in width, but a shoulder is formed in it by the now overlapping inner periphery of the casing against which a portion of the escaping steam-jet impinges and so uselessly expends its energy.
My invention has for its object the prevention of this difficulty; and it consists in constructing the channel inlet aforesaid of greater width than the wheel-outlet, so that it extends beyond the latter on both sides, and then converging the sides of the channel form this inlet, so that at a point farther outward radially they reach a width about equal to that of the discharge-opening.
In the accompanying drawings, Figure 1 is a section of the outer portion of a reaction turbine-wheel with a channel in ,its casing, the cross-section of said channelincreasing in the direction of the steam-jet, as fully de scribed in aforesaid applications, the parts being in the positions which they assume when the wheel is symmetrical with reference to said casing. Fig. 2 represents the same parts, the wheel, however, no longer being symmetrically disposed in its casing, but shown as havingmoved laterally to the left of the figure.
Similar letters of reference indicate like parts.
A represents a portion of the wheel, body formed by the heads B O, united by crossbolts, one of which is "shown at D. Circumferentially around the. wheel is formed the exhaust-opening E, through which the steam escapes between buckets, one of which is represented at F. G shows a part of the wheelcasing in which is the chamber H, in which the wheel A rotates. Said'chamber communicates with the annular passage or channel I, the cross-sections of which increase,- as above mentioned. In the drawings said increasing is such that thewalls a'b diverge outwardly, so that'the width of the passage (measured in the direction of the axis of rotation of the wheel) is greater at its outlet than at its inlet at L. At L said width is equal to or about equal to the width of the wheel exhaust-opening E. The channel I is provided with an inlet portion or nozzle, the side walls e f of which converge from its mouth K in the chamber H to'the point L of the channel I, said mouth or inlet-opening (similarly measured) being wider than the exhaust-opening E, so that the opposite edges of said opening overlap the sides of the inlet by equal distances 8 d. The opening at L thus becomes the true channel-opening, so far as the function of the channel itself is concerned. The converging portion from L to K has no effect on the action of said channel, but simply permits of the lateral displacement of the wheel without causing the production of an abrupt shoulder or the narrowing of the entrance. When the wheel is symmetrical in the casing, as shown in Fig.
1, the escaping jet (indicated by. the dotted lines) moves in the direction of the arrow straight from the wheel exhaust-opening to the channel-aperture at L. If, howeveiythe wheel be laterally displaced, as illustrated in Fig. 2, it is obvious that the enlarged opening K permits the jet to enter unobstructed and pass to and through the opening L in a direct course.
A slight lateral play of the wheel therefore becomes unobjectionable, since the disadvantages incident to it are thus fully overcome.
In combination with a radial-flow steamturbine having a circumferential dischargeopening an annular channel surrounding said I width of said channel is reduced to about the Width of said Wheel discharge-opening, substantially as described.
I11 testimony whereof I have signed my I 5 name to this specification in the presence of two subscribing witnesses.
'JORE GUS'IAF EMM'UEL LINDMARK.
Witnesses:
WALDEMAR BOMAN, T. EKEBoHn.
opening and receiving the exhaust therefrom the inlet to said channel (measured in the direction of the axis of rotation of the wheel) being Wider than said wheel discharge-opening and extending beyond the same on each side thereof and the Walls of said channel con- "erging from said inlet outwardly until the
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13833403A US735889A (en) | 1903-01-09 | 1903-01-09 | Steam-turbine. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13833403A US735889A (en) | 1903-01-09 | 1903-01-09 | Steam-turbine. |
Publications (1)
Publication Number | Publication Date |
---|---|
US735889A true US735889A (en) | 1903-08-11 |
Family
ID=2804397
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US13833403A Expired - Lifetime US735889A (en) | 1903-01-09 | 1903-01-09 | Steam-turbine. |
Country Status (1)
Country | Link |
---|---|
US (1) | US735889A (en) |
-
1903
- 1903-01-09 US US13833403A patent/US735889A/en not_active Expired - Lifetime
Similar Documents
Publication | Publication Date | Title |
---|---|---|
KR101401140B1 (en) | Optimized nozzle box steam path | |
FR2568307A1 (en) | IMPROVED STAGE FOR STEAM TURBINE | |
US735889A (en) | Steam-turbine. | |
US5927943A (en) | Inlet casing for a turbine | |
US20210404345A1 (en) | Screw rocket nozzle | |
US726315A (en) | Steam-turbine. | |
US584578A (en) | davidson | |
US1141473A (en) | Steam-turbine. | |
US613694A (en) | Robert lundell | |
US778499A (en) | Elastic-fluid turbine. | |
US546688A (en) | vojacek | |
US1553083A (en) | Elastic-fluid turbine | |
US1131645A (en) | Exhaust for steam-turbines. | |
US788000A (en) | Turbine-engine. | |
US800485A (en) | Turbine. | |
US871792A (en) | Turbine-engine. | |
US1283088A (en) | Rotary turbine-engine. | |
US797064A (en) | Elastic-fluid turbine. | |
US775462A (en) | Centrifugal gas-purifier. | |
US1308982A (en) | Setts | |
US764586A (en) | Steam-turbine. | |
US749739A (en) | Samuel lount | |
US751315A (en) | Tore gustaf emanuel lindmark | |
US915451A (en) | Steam-turbine. | |
US924852A (en) | Bucket for elastic-fluid turbines. |