GB191005219A - Ahead and Astern Turbines. - Google Patents

Ahead and Astern Turbines.

Info

Publication number
GB191005219A
GB191005219A GB191005219DA GB191005219A GB 191005219 A GB191005219 A GB 191005219A GB 191005219D A GB191005219D A GB 191005219DA GB 191005219 A GB191005219 A GB 191005219A
Authority
GB
United Kingdom
Prior art keywords
ahead
partition
impulse
stage
stages
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
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.)
BBC Brown Boveri AG Switzerland
BBC Brown Boveri AG Germany
Original Assignee
BBC Brown Boveri AG Switzerland
Brown Boveri und Cie AG Germany
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 BBC Brown Boveri AG Switzerland, Brown Boveri und Cie AG Germany filed Critical BBC Brown Boveri AG Switzerland
Application granted granted Critical
Publication of GB191005219A publication Critical patent/GB191005219A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D15/00Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • F01D15/02Adaptations for driving vehicles, e.g. locomotives

Landscapes

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

Abstract

5219. Akt.-Ges. Brown, Boveri, et Cie. Oct. 25, 1909, [Convention date]. Axial-flow type; balancing moving parts; reversing.-In combined ahead and astern turbines of the kind in which the two turbines are arranged on the same shaft with their exhaust ends adjacent and separated by a partition, the ahead turbine is provided with an impulse stage at its steam inlet followed by a reaction stage, the exhaust end of which carries a dummy piston, of the kind described in Specification 6435/04, subjected to the pressure of the steam delivered from the impulse stage, so that the propeller thrust is balanced. Ahead and astern turbines A, B are mounted on a common shaft, and their adjacent exhaust ends are separated by a partition a, which carries a packing b connected through chambers k to passages in the partition communicating with a lower pressure stage of another turbine, or with the atmosphere, or with the condenser. The ahead turbine A comprises impulse stages d and reaction stages f. Steam from the impulse stages is conducted through openings n to act on a dummy piston g, the areas of which are so arranged that the propeller thrust is balanced. Packing m is provided between the partition a and the exhaust end of the reaction stages.
GB191005219D 1909-10-25 1910-03-02 Ahead and Astern Turbines. Expired GB191005219A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE191005219X 1909-10-25

Publications (1)

Publication Number Publication Date
GB191005219A true GB191005219A (en) 1910-07-28

Family

ID=32478916

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191005219D Expired GB191005219A (en) 1909-10-25 1910-03-02 Ahead and Astern Turbines.

Country Status (1)

Country Link
GB (1) GB191005219A (en)

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