GB190629203A - Improvements in Expansible Fluid Turbines, Compressors and the like. - Google Patents

Improvements in Expansible Fluid Turbines, Compressors and the like.

Info

Publication number
GB190629203A
GB190629203A GB190629203DA GB190629203A GB 190629203 A GB190629203 A GB 190629203A GB 190629203D A GB190629203D A GB 190629203DA GB 190629203 A GB190629203 A GB 190629203A
Authority
GB
United Kingdom
Prior art keywords
wheel
guide
sides
channels
blades
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
Benjamin Silliman Church
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 GB190629203A publication Critical patent/GB190629203A/en
Expired legal-status Critical Current

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  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

29,203. Church, B. S. Dec. 21. Elastic-fluid turbines.-An elastic-fluid turbine which may be adapted for use as a compressor or the like is shown in Figs. 1 and 2. The turbine wheel G<1> has a ring of blades V on each side co-operating with nozzle rings R<1>, R<2>. The steam inlet H opens into a channel K connected to guide - channels formed on both sides of the casing and leading the steam to the nozzle rings on both sides of the wheel. The casing has guide - channels g and nozzle channels y<1> arranged in two semicircular sets on both sides of the wheel and leading the steam in a serpentine course from the inlet H to the exhaust J and causing it to impact repeatedly on the wheel. The nozzles and guide-channels increase in size from the inlet to the exhaust and are proportioned so that the steam issues from all the nozzles at a uniform speed. The guide channels g at their peripheral portions like the channel K are open from end to end so that any inequalities of pressure between the two sides of the wheel are neutralized. A modification has two rows of blades on each side of the wheel and two rows of guide-blades, the nozzles being proportioned to deliver jets proportionate to the velocities of the blades. The turbine may be adapted for running at half-load by making the two sides of the wheel independent by extending the partition f, and it may be adapted for use as a reversible marine turbine by arranging the two halves for forward and reversed running respectively.
GB190629203D 1906-12-21 1906-12-21 Improvements in Expansible Fluid Turbines, Compressors and the like. Expired GB190629203A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB190629203T 1906-12-21

Publications (1)

Publication Number Publication Date
GB190629203A true GB190629203A (en) 1907-11-14

Family

ID=32257831

Family Applications (1)

Application Number Title Priority Date Filing Date
GB190629203D Expired GB190629203A (en) 1906-12-21 1906-12-21 Improvements in Expansible Fluid Turbines, Compressors and the like.

Country Status (1)

Country Link
GB (1) GB190629203A (en)

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