GB237611A - - Google Patents

Info

Publication number
GB237611A
GB237611A GB18680/25A GB1868025A GB237611A GB 237611 A GB237611 A GB 237611A GB 18680/25 A GB18680/25 A GB 18680/25A GB 1868025 A GB1868025 A GB 1868025A GB 237611 A GB237611 A GB 237611A
Authority
GB
United Kingdom
Prior art keywords
stage
point
abrupt change
radialflow
assignees
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
GB18680/25A
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of GB237611A publication Critical patent/GB237611A/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)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

237,611. International General Electric Co., Inc., (Assignees of Allgemeine Elektricitõts Ges.). July 24, 1924, [Convention date]. Combined-flow type. - In turbines with an abrupt change of diameter of the rotor, a radialflow stage e is arranged in the steam passage at the point of the abrupt change. The stator blades of the stage e are mounted on insertions f introduced into openings in the disc-shaped wall at the point of transition.
GB18680/25A 1924-07-24 1925-07-22 Expired GB237611A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE237611X 1924-07-24

Publications (1)

Publication Number Publication Date
GB237611A true GB237611A (en) 1925-10-15

Family

ID=5903187

Family Applications (1)

Application Number Title Priority Date Filing Date
GB18680/25A Expired GB237611A (en) 1924-07-24 1925-07-22

Country Status (1)

Country Link
GB (1) GB237611A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1027530A1 (en) * 1997-10-27 2000-08-16 Kenneth Douglas Horner An air turbine motor

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1027530A1 (en) * 1997-10-27 2000-08-16 Kenneth Douglas Horner An air turbine motor
EP1027530A4 (en) * 1997-10-27 2004-05-12 Kenneth Douglas Horner An air turbine motor

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