GB191022969A - Improvements in and relating Turbines. - Google Patents

Improvements in and relating Turbines.

Info

Publication number
GB191022969A
GB191022969A GB191022969DA GB191022969A GB 191022969 A GB191022969 A GB 191022969A GB 191022969D A GB191022969D A GB 191022969DA GB 191022969 A GB191022969 A GB 191022969A
Authority
GB
United Kingdom
Prior art keywords
turbines
relating
balancing
stages
impulse
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
Charles Algernon Parsons
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 GB191022969A publication Critical patent/GB191022969A/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
    • F01D1/04—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 traversed by the working-fluid substantially axially

Landscapes

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

Abstract

22,969. Parsons, C. A. July 15. Drawings to Specification. Axial-flow type; balancing moving parts.- The intermediate and low-pressure stages of a turbine are formed as a combined turbine of the type described in Specification 2295/10, and the high-pressure stage comprises one or more impulse stages. The intermediate and lowpressure portions may be divided into two equal parts, placed one on each side of the impulse section, the working-fluid passing through them in oppositedirections. Packing and balancing are thereby facilitated.
GB191022969D 1910-07-15 1910-07-15 Improvements in and relating Turbines. Expired GB191022969A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB191022969T 1910-07-15

Publications (1)

Publication Number Publication Date
GB191022969A true GB191022969A (en) 1911-07-17

Family

ID=34356491

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191022969D Expired GB191022969A (en) 1910-07-15 1910-07-15 Improvements in and relating Turbines.

Country Status (1)

Country Link
GB (1) GB191022969A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2355177A1 (en) * 1975-06-17 1978-01-13 Bradbury Inventions Pty Ltd Multi-stage axial flow turbine - has stator blades at 45 degrees in opposition to blades on rotor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2355177A1 (en) * 1975-06-17 1978-01-13 Bradbury Inventions Pty Ltd Multi-stage axial flow turbine - has stator blades at 45 degrees in opposition to blades on rotor

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