US1456085A - Elastic-fluid turbine - Google Patents
Elastic-fluid turbine Download PDFInfo
- Publication number
- US1456085A US1456085A US525666A US52566621A US1456085A US 1456085 A US1456085 A US 1456085A US 525666 A US525666 A US 525666A US 52566621 A US52566621 A US 52566621A US 1456085 A US1456085 A US 1456085A
- Authority
- US
- United States
- Prior art keywords
- blades
- elastic
- fluid turbine
- blade
- turbine
- 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
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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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/141—Shape, i.e. outer, aerodynamic form
Description
May 22, 1923.
J. WILKINSON ELASTIC FLUID TURBINE Filed Dec. 29, 1921 l'nve'r'flzo'r- James Wilkinson,
6 v .c .wd X a Y Z e atented his 22, 31% 23.
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ELASTIC-FLUID TURBINE.
Application filed December 29, 1921. Serial No. 525,686.
To all whom it may concern-.-
Be it known that I, JA ES WI INSON, a citizen of the United States, residing at Schenectady, in the county of Schenectady, State of New York, have invented certain new and useful Improvements in Elastic-Fluid Turbines, of which the following is a specification.
The present invention relates to elastic fluid turbines and has for its object to provide an improved bucket or blade structure.
For a consideration of what I believe to be novel and my invention, attention is directed to the accompanying description and the claims appended thereto,
In the drawing Fig. l is a side elevation of a part of a turbine rotor element having blades or buckets embodying my invention; Fig. 2 is a radial sectional view of Fig. 1 taken between two adjacent blades, and Fig. 3 comprises three sectional views marked X, Y and Z of adjacent blades, the views being taken on lines X-X, Y-Y and ZZ, respectively, Fig. 1.
Referring to the drawing, 5 indicates a turbine rotor member here shown in the form of a disk or wheel. Mounted on its periphery is a ring of blades or buckets 6 which may be attached to it in any suitable manner. The foregoing is to be taken as typical of any turbine rotor comprising a carrying member with a ring or rings of blades or buckets mounted thereon.
According to my invention, I provide blades or buckets of such shape that when mounted on the carrying member the ratio of the pitch to the width of blade or bucket is constant, or substantially constant,
throu hout the length of blade or bucket.
By pitch is meant the distance between blades, being the distance indicated by a in Fig. 3, and by width of blade is meant the distance between the entrance edge and the exit edge indicated by Z) in Fig. 3. At every point throughout the length of the blades %=constant. To this end the blades are This gives a constant ratio between pitch and width, sincethe blades all radiate from the center of the rotor. Furthermore, I preferably shape the blades so as to obtain uniform overlap, by overlap being meant the amount which the concave side of a blade overlaps the convex side of the next adjacent blade. With blades having a uniform taper converging to the center of the rotor, uniform overlap is obtained by a blade, having a radius of curvature which increases uniformly throughout its length from root to tip.
It is well recognized that for given conditions, a certain ratio of pitch to width and a certain amount of overlap gives the highest efficiency. With blades of uniform width, however, these conditions must be successively compromised. It is clear that with such blades if the ratio of pitch to width has its most eflicient value midway between the ends of the blades then toward the roots the ratio becomes too small while toward the tips it becomes too great. In other words, the blades are too close together at their roots and too far apart at their tips. Also if the overlap is correct midway between the ends of the blades, then it becomes too great at the base and insufficient at the tip. By my invention I overcome these difficulties and thereby increase the efficiency of the blade ring.
In accordance with the provisions of the patent statutes, I have described the principle of operation of my invention, together with the apparatus which I now consider to represent the best embodiment thereof, but I desire to have it understood that the apparatus shown is only illustrative and that the invention may be carried out by other means.
What I claim as new and desire to secure by Letters Patent of the United States, is
1. In an elastic fluid turbine, a carrying member and blades projecting radially there-- from, the ratio of pitch to width being substantially uniform throughout the length of the blades.
2. In an elastic fluid turbine, a carrying member and blades projecting radially therefrom, said blades being widest at their tips and tapering toward the roots,
3. In an elastic fluid turbine, a carrying member andblades projecting radially therefrom, said blades having substantially uniform overlap throughout their length.
4. In an elastic'fluid turbine, acarrying member and blades projecting radially therefrom, the ratio of pitch to width being substantially uniform throughout the length of the blades, and said blades having substantially uniform overlap throughout their lengths.
5. In an elastic fluid turbine, a carrying member and blades projecting radially there "from, saidblades being widest at'their tips and tapering toward the roots, the taper being along lines which converge to the center of the carrying member.
6. As an article of manufacture, a turbine blade which tapers outwardly from its root to its tip." e i 7. As an article ofmanufacture, a turbine blade which tapers outwardly from its root gradually increasing carrying member;
In witness whereof, I have hereunto set my hand this 28th day of December, 1921.
JAMES WILKINSON;
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US525666A US1456085A (en) | 1921-12-29 | 1921-12-29 | Elastic-fluid turbine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US525666A US1456085A (en) | 1921-12-29 | 1921-12-29 | Elastic-fluid turbine |
Publications (1)
Publication Number | Publication Date |
---|---|
US1456085A true US1456085A (en) | 1923-05-22 |
Family
ID=24094155
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US525666A Expired - Lifetime US1456085A (en) | 1921-12-29 | 1921-12-29 | Elastic-fluid turbine |
Country Status (1)
Country | Link |
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US (1) | US1456085A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3135496A (en) * | 1962-03-02 | 1964-06-02 | Gen Electric | Axial flow turbine with radial temperature gradient |
FR2404101A1 (en) * | 1977-09-26 | 1979-04-20 | Hitachi Ltd | BLADE STRUCTURE FOR AXIAL FLUID MACHINE |
US5286168A (en) * | 1992-01-31 | 1994-02-15 | Westinghouse Electric Corp. | Freestanding mixed tuned blade |
-
1921
- 1921-12-29 US US525666A patent/US1456085A/en not_active Expired - Lifetime
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3135496A (en) * | 1962-03-02 | 1964-06-02 | Gen Electric | Axial flow turbine with radial temperature gradient |
FR2404101A1 (en) * | 1977-09-26 | 1979-04-20 | Hitachi Ltd | BLADE STRUCTURE FOR AXIAL FLUID MACHINE |
US5286168A (en) * | 1992-01-31 | 1994-02-15 | Westinghouse Electric Corp. | Freestanding mixed tuned blade |
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