GB190815893A - Improvements in Turbine Engines. - Google Patents

Improvements in Turbine Engines.

Info

Publication number
GB190815893A
GB190815893A GB190815893DA GB190815893A GB 190815893 A GB190815893 A GB 190815893A GB 190815893D A GB190815893D A GB 190815893DA GB 190815893 A GB190815893 A GB 190815893A
Authority
GB
United Kingdom
Prior art keywords
blades
turbine engines
enlargements
cooper
weakening
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
Arthur William Cooper
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 GB190815893A publication Critical patent/GB190815893A/en
Expired legal-status Critical Current

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  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

15,893. Cooper, A. W. July 27. Elastic-fluid turbines. -Relates to means for fastening the blades to the rotor without weakening its rim. For this purpose recesses are formed in the wheel rims alternately at a greater and less radius. Each recess has bevelled edges against which the right and left root enlargements D of a pair of blades A are secured by a key B. A shroud E made in sections is provided.
GB190815893D 1908-07-27 1908-07-27 Improvements in Turbine Engines. Expired GB190815893A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB190815893T 1908-07-27

Publications (1)

Publication Number Publication Date
GB190815893A true GB190815893A (en) 1909-01-28

Family

ID=32552432

Family Applications (1)

Application Number Title Priority Date Filing Date
GB190815893D Expired GB190815893A (en) 1908-07-27 1908-07-27 Improvements in Turbine Engines.

Country Status (1)

Country Link
GB (1) GB190815893A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2434935A (en) * 1946-02-08 1948-01-27 Westinghouse Electric Corp Turbine apparatus
US2658718A (en) * 1944-12-22 1953-11-10 Power Jets Res & Dev Ltd Manufacture and attachment of turbine and like blading
US2753149A (en) * 1951-03-30 1956-07-03 United Aircraft Corp Blade lock
US2781998A (en) * 1950-03-07 1957-02-19 Centrax Power Units Ltd Bladed rotors
US2786648A (en) * 1950-04-04 1957-03-26 United Aircraft Corp Blade locking device
US2801074A (en) * 1952-10-01 1957-07-30 United Aircraft Corp Blade retaining means
US2833515A (en) * 1953-08-20 1958-05-06 Philip P Newcomb Turbine blade
US2957675A (en) * 1956-05-07 1960-10-25 Gen Electric Damping means
US2967043A (en) * 1956-11-30 1961-01-03 Napier & Sons Ltd D Blades and blade mounting assemblies for turbines and axial flow compressors
US4084922A (en) * 1976-12-27 1978-04-18 Electric Power Research Institute, Inc. Turbine rotor with pin mounted ceramic turbine blades
USRE32042E (en) * 1979-08-31 1985-12-03 Elliott Turbomachinery Company, Inc. Stator blade assembly for turbo machines

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2658718A (en) * 1944-12-22 1953-11-10 Power Jets Res & Dev Ltd Manufacture and attachment of turbine and like blading
US2434935A (en) * 1946-02-08 1948-01-27 Westinghouse Electric Corp Turbine apparatus
US2781998A (en) * 1950-03-07 1957-02-19 Centrax Power Units Ltd Bladed rotors
US2786648A (en) * 1950-04-04 1957-03-26 United Aircraft Corp Blade locking device
US2753149A (en) * 1951-03-30 1956-07-03 United Aircraft Corp Blade lock
US2801074A (en) * 1952-10-01 1957-07-30 United Aircraft Corp Blade retaining means
US2833515A (en) * 1953-08-20 1958-05-06 Philip P Newcomb Turbine blade
US2957675A (en) * 1956-05-07 1960-10-25 Gen Electric Damping means
US2967043A (en) * 1956-11-30 1961-01-03 Napier & Sons Ltd D Blades and blade mounting assemblies for turbines and axial flow compressors
US4084922A (en) * 1976-12-27 1978-04-18 Electric Power Research Institute, Inc. Turbine rotor with pin mounted ceramic turbine blades
USRE32042E (en) * 1979-08-31 1985-12-03 Elliott Turbomachinery Company, Inc. Stator blade assembly for turbo machines

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