GB191207321A - Improvements in or relating to Turbines. - Google Patents
Improvements in or relating to Turbines.Info
- Publication number
- GB191207321A GB191207321A GB191207321DA GB191207321A GB 191207321 A GB191207321 A GB 191207321A GB 191207321D A GB191207321D A GB 191207321DA GB 191207321 A GB191207321 A GB 191207321A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blades
- shaft
- secured
- rotor
- chamber
- 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
Links
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
- F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
- F01D1/24—Non-positive-displacement machines or engines, e.g. steam turbines characterised by counter-rotating rotors subjected to same working fluid stream without intermediate stator blades or the like
- F01D1/26—Non-positive-displacement machines or engines, e.g. steam turbines characterised by counter-rotating rotors subjected to same working fluid stream without intermediate stator blades or the like traversed by the working-fluid substantially axially
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
7321. Gill, T. March 26. [Cognate Applications, 10,412/12 and 11,283/12.] Axial-flow type; oppositelyrunning rotor type; casings; rotors; reversing.-Relates to turbines with axial flow and screw fans and pumps of the turbine type, and consists in building up the machine by assembling a number of longitudinal sections. A turbine of the type having oppositelyrunning rotors comprises an inner rotor formed from a number of flanged disks f, Fig. 1, bolted together and secured to a shaft m. To each disk, a ring of blades h is secured. If required, each ring of blades may be provided with a shroud n. The outer rotor comprises a number of rings c, secured together by bolts d, each ring carrying a set of blades g, the inner ends of which are secured to disks e. The lengths of the blades increase progressively from inlet to exhaust, and the blades g, h rotate in opposite directions. The oppositelyrotating parts are geared together by epicyclic gearing w carried by a part v. Fluid is admitted through the hollow shaft m to a chamber p, whence it flows through the blades to a chamber t and exhausts through ports x. A cover a and exhaust-pipe b are shown in dotted lines. In a modification, each of the oppositely-rotating members is mounted upon a shaft provided with a loose pulley and clutch mechanism, whereby power can be taken off either shaft alternatively. In a. further modification, the rings c and blades g are stationary, the shaft m being divided into two parts, one of which carries the rotor and the other the stator. In a pump of the turbine type, the stator is supported by a stationary shaft k, Fig. 11, while the rotor is secured to a shaft 10. Fluid enters the hollow shaft k and passes through perforations 9 to the chamber 8, whence it is pumped through to the chamber p, being finally discharged through the hollow shaft 10.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB191207321T | 1912-03-26 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB191207321A true GB191207321A (en) | 1913-03-06 |
Family
ID=32571042
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB191207321D Expired GB191207321A (en) | 1912-03-26 | 1912-03-26 | Improvements in or relating to Turbines. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB191207321A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3981460A (en) * | 1973-08-30 | 1976-09-21 | Robert N. Starr | Staggered channel wing-type aircraft |
US4090681A (en) * | 1975-12-11 | 1978-05-23 | Dornier Gmbh | Airplane with two superposed wings |
-
1912
- 1912-03-26 GB GB191207321D patent/GB191207321A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3981460A (en) * | 1973-08-30 | 1976-09-21 | Robert N. Starr | Staggered channel wing-type aircraft |
US4090681A (en) * | 1975-12-11 | 1978-05-23 | Dornier Gmbh | Airplane with two superposed wings |
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