GB191328271A - Improvements in Elastic Fluid Turbines. - Google Patents

Improvements in Elastic Fluid Turbines.

Info

Publication number
GB191328271A
GB191328271A GB191328271DA GB191328271A GB 191328271 A GB191328271 A GB 191328271A GB 191328271D A GB191328271D A GB 191328271DA GB 191328271 A GB191328271 A GB 191328271A
Authority
GB
United Kingdom
Prior art keywords
cast
rotor
stage
chambers
spokes
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 Bemis Rearick
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 GB191328271A publication Critical patent/GB191328271A/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
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups

Landscapes

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

Abstract

28,271. Rearick, C. B. Dec. 9, 1912, [Convention date]. Reflexed-flow type; casings ; rotors.-A reflexedflow turbine with tangential jets comprises a rotor with a series of buckets 6, 9, 14, 18, 23, arranged side by side and co-operating with a stator comprising nozzles 4 and guide - chambers 10, 12, 17, 20. the motive fluid passing in succession from stage to stage. The capacity and inclination of guide-chambers and rotor buckets increase from stage to stage. The parts carrying the guide-chambers are connected to the casing by sliding joints 42, Fig. 2. The rim of the rotor is preferably cast in one piece with the buckets, e.g. by the process described in Specification 20,557/11, [Class 83 (i), Casting &c. metals], and the rim may be cast around spokes 26 of bronze or other suitable material. Subsequently, a cast-iron hub 48 is cast on to the inner ends of the spokes 26. The hub may have cast integrally therewith spoke supports 24 which, while allowing the spokes to expand radially, afford lateral support thereto. An additional sleeve 25 of steel may be placed on each spoke before casting on the hub and supports. Steam is admitted by way of a conduit 2 and steam-chest 3. The ends of the rotor are closed by side plates 40, Fig. 1.
GB191328271D 1912-12-09 1913-12-08 Improvements in Elastic Fluid Turbines. Expired GB191328271A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US191328271XA 1912-12-09 1912-12-09

Publications (1)

Publication Number Publication Date
GB191328271A true GB191328271A (en) 1914-09-17

Family

ID=32657007

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191328271D Expired GB191328271A (en) 1912-12-09 1913-12-08 Improvements in Elastic Fluid Turbines.

Country Status (1)

Country Link
GB (1) GB191328271A (en)

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