GB185194A - Improvements in turbines - Google Patents

Improvements in turbines

Info

Publication number
GB185194A
GB185194A GB1478621A GB1478621A GB185194A GB 185194 A GB185194 A GB 185194A GB 1478621 A GB1478621 A GB 1478621A GB 1478621 A GB1478621 A GB 1478621A GB 185194 A GB185194 A GB 185194A
Authority
GB
United Kingdom
Prior art keywords
rotor
blades
nozzles
openings
radial length
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
Application number
GB1478621A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to GB1478621A priority Critical patent/GB185194A/en
Publication of GB185194A publication Critical patent/GB185194A/en
Expired legal-status Critical Current

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
    • F01D1/02—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines
    • F01D1/026—Impact turbines with buckets, i.e. impulse turbines, e.g. Pelton turbines

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

185,194. Corthesy, J. H., and Dickson, W. K. L. May 27, 1921. Axial-flow type; circular-flow type; oppositelyrunnning rotor type; blades.-A turbine rotor is formed of an uninterrupted hollow annular drum R with blades 1 and openings in one of its side walls. Working fluid is supplied through nozzles N in a stator chamber S which has a small clearance at the nozzles but elsewhere has ample clearance to allow the working fluid to flow from the interior of the rotor into the stator chamber. The radial length of the blades and openings should be about twice the radial length of the nozzles. The rotor may be formed of two flanged discs d, in which the blades and openings have been stamped, separated by a hub h acting as a distance-piece. A number of rotors may be compounded on one shaft. Working-fluid from one rotor may pass to a second rotor running in the opposite direction.
GB1478621A 1921-05-27 1921-05-27 Improvements in turbines Expired GB185194A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1478621A GB185194A (en) 1921-05-27 1921-05-27 Improvements in turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1478621A GB185194A (en) 1921-05-27 1921-05-27 Improvements in turbines

Publications (1)

Publication Number Publication Date
GB185194A true GB185194A (en) 1922-08-28

Family

ID=10047453

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1478621A Expired GB185194A (en) 1921-05-27 1921-05-27 Improvements in turbines

Country Status (1)

Country Link
GB (1) GB185194A (en)

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