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FR1281033A - Assembly of ceramic moving blades on machines with centrifugal rotors axially traversed by currents, in particular on gas turbines - Google Patents

Assembly of ceramic moving blades on machines with centrifugal rotors axially traversed by currents, in particular on gas turbines

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Publication number
FR1281033A
FR1281033AFR852751AFR852751AFR1281033AFR 1281033 AFR1281033 AFR 1281033AFR 852751 AFR852751 AFR 852751AFR 852751 AFR852751 AFR 852751AFR 1281033 AFR1281033 AFR 1281033A
Authority
FR
France
Prior art keywords
currents
machines
assembly
gas turbines
moving 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
FR852751A
Other languages
French (fr)
Inventor
Klaus Rentzsch
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.)
Daimler Benz AG
Original Assignee
Daimler Benz AG
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 Daimler Benz AGfiledCriticalDaimler Benz AG
Priority to FR852751ApriorityCriticalpatent/FR1281033A/en
Application grantedgrantedCritical
Publication of FR1281033ApublicationCriticalpatent/FR1281033A/en
Expiredlegal-statusCriticalCurrent

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FR852751A1961-02-151961-02-15 Assembly of ceramic moving blades on machines with centrifugal rotors axially traversed by currents, in particular on gas turbinesExpiredFR1281033A (en)

Priority Applications (1)

Application NumberPriority DateFiling DateTitle
FR852751AFR1281033A (en)1961-02-151961-02-15 Assembly of ceramic moving blades on machines with centrifugal rotors axially traversed by currents, in particular on gas turbines

Applications Claiming Priority (1)

Application NumberPriority DateFiling DateTitle
FR852751AFR1281033A (en)1961-02-151961-02-15 Assembly of ceramic moving blades on machines with centrifugal rotors axially traversed by currents, in particular on gas turbines

Publications (1)

Publication NumberPublication Date
FR1281033Atrue FR1281033A (en)1962-01-08

Family

ID=8748862

Family Applications (1)

Application NumberTitlePriority DateFiling Date
FR852751AExpiredFR1281033A (en)1961-02-151961-02-15 Assembly of ceramic moving blades on machines with centrifugal rotors axially traversed by currents, in particular on gas turbines

Country Status (1)

CountryLink
FR (1)FR1281033A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
DE2240970A1 (en)*1971-12-091973-06-14United Aircraft Corp ROTOR WITH COMPOSITE SHOVELS OR BLADES
US4102602A (en)*1976-08-311978-07-25Volkswagenwerk AktiengesellschaftRotor for an axial turbine
US4169694A (en)*1977-07-201979-10-02Electric Power Research Institute, Inc.Ceramic rotor blade having root with double curvature
DE2834864A1 (en)*1978-08-091980-02-14Motoren Turbinen Union COMPOSED CERAMIC GAS TURBINE BLADE
US4802824A (en)*1986-12-171989-02-07Societe Nationale D'etude Et Moteurs D'aviation "S.N.E.C.M.A."Turbine rotor
US6102664A (en)*1995-12-142000-08-15The United States Of America As Represented By The Administrator Of The National Aeronautics And Space AdministrationBlading system and method for controlling structural vibrations
FR2890684A1 (en)*2005-09-152007-03-16Snecma CLINKING FOR TURBOREACTOR BLADE
EP2077376A3 (en)*2008-01-042012-04-25United Technologies CorporationComposite rotor blade attachment in a gas turbine

Cited By (11)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
DE2240970A1 (en)*1971-12-091973-06-14United Aircraft Corp ROTOR WITH COMPOSITE SHOVELS OR BLADES
US3752600A (en)*1971-12-091973-08-14United Aircraft CorpRoot pads for composite blades
US4102602A (en)*1976-08-311978-07-25Volkswagenwerk AktiengesellschaftRotor for an axial turbine
US4169694A (en)*1977-07-201979-10-02Electric Power Research Institute, Inc.Ceramic rotor blade having root with double curvature
DE2834864A1 (en)*1978-08-091980-02-14Motoren Turbinen Union COMPOSED CERAMIC GAS TURBINE BLADE
US4802824A (en)*1986-12-171989-02-07Societe Nationale D'etude Et Moteurs D'aviation "S.N.E.C.M.A."Turbine rotor
US6102664A (en)*1995-12-142000-08-15The United States Of America As Represented By The Administrator Of The National Aeronautics And Space AdministrationBlading system and method for controlling structural vibrations
FR2890684A1 (en)*2005-09-152007-03-16Snecma CLINKING FOR TURBOREACTOR BLADE
EP1764480A1 (en)*2005-09-152007-03-21SnecmaShim for a turbine engine blade
US7938626B2 (en)2005-09-152011-05-10SnecmaShim for a turbojet blade
EP2077376A3 (en)*2008-01-042012-04-25United Technologies CorporationComposite rotor blade attachment in a gas turbine

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