GB191101388A - Improvements in and relating to High Velocity Fluid Turbines. - Google Patents

Improvements in and relating to High Velocity Fluid Turbines.

Info

Publication number
GB191101388A
GB191101388A GB191101388DA GB191101388A GB 191101388 A GB191101388 A GB 191101388A GB 191101388D A GB191101388D A GB 191101388DA GB 191101388 A GB191101388 A GB 191101388A
Authority
GB
United Kingdom
Prior art keywords
nozzles
rotor
stator
pockets
flow type
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
Inventor
Allen Gosling
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
Application granted granted Critical
Publication of GB191101388A publication Critical patent/GB191101388A/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)

Abstract

1388. Gosling, A. Jan. 19. [Cognate Application, 1894/11.] Reflexed - flow type; combined - flow type; nozzles; regutating; reversing; working - fluid supply.-In a turbine of the reflexed-flow type having axial jets, the pockets o in the rotor parts e and in the stator parts f are formed by inclined partitions so that the working-fluid follows a path made up of smooth curves. It passes from the nozzles m through the first rotor pockets, then through the first stator pockets, over the edge of the first rotor and into the second rotor as shown. The stator partitions may project from the stator. The exhaust steam from such a turbine may be further expanded in a Parsons' or other reaction turbine. The diverging nozzles mare formed by the central part l and a ring s. The ring s may be dispensed with. Two similar turbines may be placed end to end, in which case one part may be used for reversing, or for overload working. The nozzles m are fed by passages g, h, each set of passages being under the control of a multiple-ported valve such as that described in Specification 8782/05. Some of the nozzles may be supplied with steam, and the others with combustion products.
GB191101388D 1911-01-19 1911-01-19 Improvements in and relating to High Velocity Fluid Turbines. Expired GB191101388A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB191101388T 1911-01-19

Publications (1)

Publication Number Publication Date
GB191101388A true GB191101388A (en) 1911-11-02

Family

ID=32638799

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191101388D Expired GB191101388A (en) 1911-01-19 1911-01-19 Improvements in and relating to High Velocity Fluid Turbines.

Country Status (1)

Country Link
GB (1) GB191101388A (en)

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