GB191208351A - Improvements in and relating to Turbines. - Google Patents

Improvements in and relating to Turbines.

Info

Publication number
GB191208351A
GB191208351A GB191208351DA GB191208351A GB 191208351 A GB191208351 A GB 191208351A GB 191208351D A GB191208351D A GB 191208351DA GB 191208351 A GB191208351 A GB 191208351A
Authority
GB
United Kingdom
Prior art keywords
stage
blades
nozzles
turbines
relating
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
Delevan Paul Upson
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 GB191208351A publication Critical patent/GB191208351A/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
    • F01D1/34—Non-positive-displacement machines or engines, e.g. steam turbines characterised by non-bladed rotor, e.g. with drilled holes

Landscapes

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

Abstract

8351. Upson, D. P. April 9. Axial-flow type. -Radial blades 14, Figs. 1 and 3, are mounted upon disks 9, Fig. 1, secured to a shaft 7. Fixed partitions 6 and bushings 11 prevent leakage between stages. Steam is admitted by a conduit 2 to the nozzle 16 of the first stage. The exhaust is received in a recess 15, whence it is transmitted through two nozzles 16 to the second stage, and so on. The length of the recesses 15 and the number of nozzles 16 increase progressively from stage to stage to allow expansive working. Blades. - As shown in Fig. 3, the blades have flat working faces, and bevelled backs. Reference has been directed by the Comptroller to Specifications 11,701/01 and 26,454/03.
GB191208351D 1912-04-09 1912-04-09 Improvements in and relating to Turbines. Expired GB191208351A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB191208351T 1912-04-09

Publications (1)

Publication Number Publication Date
GB191208351A true GB191208351A (en) 1912-10-31

Family

ID=32571548

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191208351D Expired GB191208351A (en) 1912-04-09 1912-04-09 Improvements in and relating to Turbines.

Country Status (1)

Country Link
GB (1) GB191208351A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2767673A4 (en) * 2011-10-04 2015-12-02 Hyuk Sun Choi Axial turbine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2767673A4 (en) * 2011-10-04 2015-12-02 Hyuk Sun Choi Axial turbine

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