GB190622690A - Improvements in Elastic-fluid Turbines, Turbo-compressors, Turbine Fans, and the like. - Google Patents

Improvements in Elastic-fluid Turbines, Turbo-compressors, Turbine Fans, and the like.

Info

Publication number
GB190622690A
GB190622690A GB190622690DA GB190622690A GB 190622690 A GB190622690 A GB 190622690A GB 190622690D A GB190622690D A GB 190622690DA GB 190622690 A GB190622690 A GB 190622690A
Authority
GB
United Kingdom
Prior art keywords
blades
roots
blocks
engage
rings
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
Victor Gelpke
Paul Kugel
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 GB190622690A publication Critical patent/GB190622690A/en
Expired legal-status Critical Current

Links

Abstract

22,690. Gelpke, V., and Kugel, P. Oct. 13. Elastic-fluid turbines.-Relates to the setting and fixing of blades in turbines, turbine fans, &c. Two or more strips b<1>, b<2>, Figs. 1 and 9, are perforated to accommodate the roots of the blades a. The blades are secured in position by blocks d, which engage cot-away parts of the blade roots, or by any suitable means. Instead of the 'strips b<1>, b<2> being made in the form of continuous rings, they may be formed as filling-pieces, one piece being placed between two adjacent blades at the top of the root and another at the bottom. In a modification, the rings b<1>, b<2> are made of angular sections so as to engage the blocks d more securely. In another modification, the lower ring b<1> is replaced by two copper rings which are pressed by the blocks d against the roots of the blades. In a further modification, the blade roots are made with studs which engage with the drum, the ring b<1> again being dispensed with. One spacing-ring only need be used if the blades are prolonged so far toward the centre of the drum that their roots abut against each other. The blocks d may be made integrally with the disks in that type of turbine in which the rotor consists of a number of parallel bladed disks. The outer ends of the vanes may be joined together and fitted with shrouds in a manner similar to that described above. The invention is also applicable to guides.
GB190622690D 1906-10-13 1906-10-13 Improvements in Elastic-fluid Turbines, Turbo-compressors, Turbine Fans, and the like. Expired GB190622690A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB190622690T 1906-10-13

Publications (1)

Publication Number Publication Date
GB190622690A true GB190622690A (en) 1907-02-21

Family

ID=32205111

Family Applications (1)

Application Number Title Priority Date Filing Date
GB190622690D Expired GB190622690A (en) 1906-10-13 1906-10-13 Improvements in Elastic-fluid Turbines, Turbo-compressors, Turbine Fans, and the like.

Country Status (1)

Country Link
GB (1) GB190622690A (en)

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