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GB191306692A - Improvements in Turbo Compressors and Turbines. - Google Patents

Improvements in Turbo Compressors and Turbines.

Info

Publication number
GB191306692A
GB191306692A GB191306692DA GB191306692A GB 191306692 A GB191306692 A GB 191306692A GB 191306692D A GB191306692D A GB 191306692DA GB 191306692 A GB191306692 A GB 191306692A
Authority
GB
United Kingdom
Prior art keywords
flow
blades
chamber
turbines
rotary
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
Montague Herbe Churchill-Shann
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 GB191306692A publication Critical patent/GB191306692A/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

6692. Shann, M. H. Churchill-. March'18. Combined-flow type. -A turbine, which may, with reversed flow, be used as a compressor, comprises a high-pressure chamber B with spaced nozzles C1, rotary blades C of the radialaxial type, fixed blades D, rotary axial-flow blades E, and fixed blades F delivering to the exhaust chamber A. The blades D, E, F are spaced as shown in Fig. 4, and the shrouds diverge as shown in Fig. 1 in order to give a predetermined centre line of flow. Packing-ribs are provided at E<1> and C<1>. The number of axial flow-wheels may be varied, and the steam may be introduced tangentially into the chamber B.
GB191306692D 1913-03-18 1913-03-18 Improvements in Turbo Compressors and Turbines. Expired GB191306692A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB191306692T 1913-03-18

Publications (1)

Publication Number Publication Date
GB191306692A true GB191306692A (en) 1914-02-26

Family

ID=34359163

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191306692D Expired GB191306692A (en) 1913-03-18 1913-03-18 Improvements in Turbo Compressors and Turbines.

Country Status (1)

Country Link
GB (1) GB191306692A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2951678A (en) * 1954-05-04 1960-09-06 Thompson Ramo Wooldridge Inc Aerodynamic overspeed control for turbines

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2951678A (en) * 1954-05-04 1960-09-06 Thompson Ramo Wooldridge Inc Aerodynamic overspeed control for turbines

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