GB190800282A - Improvements relating to Turbines. - Google Patents

Improvements relating to Turbines.

Info

Publication number
GB190800282A
GB190800282A GB190800282DA GB190800282A GB 190800282 A GB190800282 A GB 190800282A GB 190800282D A GB190800282D A GB 190800282DA GB 190800282 A GB190800282 A GB 190800282A
Authority
GB
United Kingdom
Prior art keywords
flanges
drum
studs
bolts
fitting
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.)
JOHN MCKENZIE NEWTON
Brush Electrical Engineering Co Ltd
Original Assignee
JOHN MCKENZIE NEWTON
Brush Electrical Engineering Co 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 JOHN MCKENZIE NEWTON, Brush Electrical Engineering Co Ltd filed Critical JOHN MCKENZIE NEWTON
Application granted granted Critical
Publication of GB190800282A publication Critical patent/GB190800282A/en
Expired legal-status Critical Current

Links

Abstract

282. Chilton, W., Newton, J. M., and Brush Electrical Engineering Co. Jan. 4. Elastic-fluid turbines.-Relates to means for attaching the end shafts to the turbine drum so as to avoid injury due to the varying thermal expansion of the connected parts. The end shaft band drum d are each provided with flanges a, d, which are connected together by bolts and nuts, or studs. Registering-devices are provided to prevent shearing-stress on the bolts or studs, and consist of a cylindrical flange extension e of the drum and a corresponding recess in the end shaft, as shown in Fig. 1, or a ring j fitting two annular grooves a, d, Fig. 2, or pins j<*> fitting corresponding holes in the flanges, as shown in Fig. 3. Shearing-stress due to torque may be avoided by inserting keys i, Fig. 1, in recesses in the flanges.
GB190800282D 1908-01-04 1908-01-04 Improvements relating to Turbines. Expired GB190800282A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB190800282T 1908-01-04

Publications (1)

Publication Number Publication Date
GB190800282A true GB190800282A (en) 1908-10-29

Family

ID=32635389

Family Applications (1)

Application Number Title Priority Date Filing Date
GB190800282D Expired GB190800282A (en) 1908-01-04 1908-01-04 Improvements relating to Turbines.

Country Status (1)

Country Link
GB (1) GB190800282A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2461242A (en) * 1944-08-23 1949-02-08 United Aircraft Corp Rotor construction for turbines

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2461242A (en) * 1944-08-23 1949-02-08 United Aircraft Corp Rotor construction for turbines

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