GB190517373A - Improvements in Turbine Motors. - Google Patents

Improvements in Turbine Motors.

Info

Publication number
GB190517373A
GB190517373A GB190517373DA GB190517373A GB 190517373 A GB190517373 A GB 190517373A GB 190517373D A GB190517373D A GB 190517373DA GB 190517373 A GB190517373 A GB 190517373A
Authority
GB
United Kingdom
Prior art keywords
blades
shanks
groove
secured
wheel
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.)
Belliss and Morcom Ltd
Original Assignee
Belliss and Morcom Ltd
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 Belliss and Morcom Ltd filed Critical Belliss and Morcom Ltd
Application granted granted Critical
Publication of GB190517373A publication Critical patent/GB190517373A/en
Expired legal-status Critical Current

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Abstract

17,373. Belliss & Morcom, and Jude, A. Aug. 28. Making turbines.-Relates to methods of constructing and assembling blades for the fixed and moving parts of turbines such as are described in Specification No. 24,570, A.D. 1904. Wheel blades b, Fig. 5, have shanks b<1> which are bent over and inserted in notches formed in the wheel or in a ring C, so that the intervening pieces of metal c<1> form distancepieces and may be upset to secure the blades in position. The shanks may be either doubled over or single, and they may be dovetailed and the blades secured by squeezing the sides of the groove. Blades b, Fig. 12, of very oblique arrangement, have their shanks b<1> twisted and inserted in a narrow groove B<1>, where they are gripped by the sides of the groove. Or the blades may be secured in a wide groove without twisting their shanks by means of two stepped filling-pieces.
GB190517373D 1905-08-28 1905-08-28 Improvements in Turbine Motors. Expired GB190517373A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB190517373T 1905-08-28

Publications (1)

Publication Number Publication Date
GB190517373A true GB190517373A (en) 1906-08-23

Family

ID=32198898

Family Applications (1)

Application Number Title Priority Date Filing Date
GB190517373D Expired GB190517373A (en) 1905-08-28 1905-08-28 Improvements in Turbine Motors.

Country Status (1)

Country Link
GB (1) GB190517373A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE758097C (en) * 1940-06-08 1954-02-22 Versuchsanstalt Fuer Luftfahrt Blade attachment for gas or exhaust turbine blades

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE758097C (en) * 1940-06-08 1954-02-22 Versuchsanstalt Fuer Luftfahrt Blade attachment for gas or exhaust turbine blades

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