BE900845A - Afdichting voor rotorblad-voetplaat. - Google Patents
Afdichting voor rotorblad-voetplaat.Info
- Publication number
- BE900845A BE900845A BE0/213851A BE213851A BE900845A BE 900845 A BE900845 A BE 900845A BE 0/213851 A BE0/213851 A BE 0/213851A BE 213851 A BE213851 A BE 213851A BE 900845 A BE900845 A BE 900845A
- Authority
- BE
- Belgium
- Prior art keywords
- base plate
- seal
- rotor blade
- edge
- blade base
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/28—Arrangement of seals
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/005—Sealing means between non relatively rotating elements
- F01D11/006—Sealing the gap between rotor blades or blades and rotor
- F01D11/008—Sealing the gap between rotor blades or blades and rotor by spacer elements between the blades, e.g. independent interblade platforms
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/005—Sealing means between non relatively rotating elements
- F01D11/006—Sealing the gap between rotor blades or blades and rotor
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S416/00—Fluid reaction surfaces, i.e. impellers
- Y10S416/50—Vibration damping features
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/544,933 US4505642A (en) | 1983-10-24 | 1983-10-24 | Rotor blade interplatform seal |
Publications (1)
Publication Number | Publication Date |
---|---|
BE900845A true BE900845A (nl) | 1985-02-15 |
Family
ID=24174182
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE0/213851A BE900845A (nl) | 1983-10-24 | 1984-10-18 | Afdichting voor rotorblad-voetplaat. |
Country Status (13)
Country | Link |
---|---|
US (1) | US4505642A (fr) |
JP (1) | JPS60111003A (fr) |
KR (1) | KR850003923A (fr) |
BE (1) | BE900845A (fr) |
CA (1) | CA1209483A (fr) |
CH (1) | CH665684A5 (fr) |
DE (1) | DE3436663A1 (fr) |
DK (1) | DK504784A (fr) |
GR (1) | GR80598B (fr) |
IL (1) | IL73167A (fr) |
NL (1) | NL8403110A (fr) |
TR (1) | TR22355A (fr) |
YU (1) | YU181884A (fr) |
Families Citing this family (34)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4580946A (en) * | 1984-11-26 | 1986-04-08 | General Electric Company | Fan blade platform seal |
US4743166A (en) * | 1984-12-20 | 1988-05-10 | General Electric Company | Blade root seal |
US4743164A (en) * | 1986-12-29 | 1988-05-10 | United Technologies Corporation | Interblade seal for turbomachine rotor |
US4872812A (en) * | 1987-08-05 | 1989-10-10 | General Electric Company | Turbine blade plateform sealing and vibration damping apparatus |
CA1340877C (fr) * | 1987-12-28 | 2000-01-18 | Takashi Sugiyama | Polypeptide inhibant l'elastage et procede de production par la technologie de l'adn recombinant |
GB2223277B (en) * | 1988-09-30 | 1992-08-12 | Rolls Royce Plc | Aerofoil blade damping |
US4872810A (en) * | 1988-12-14 | 1989-10-10 | United Technologies Corporation | Turbine rotor retention system |
US4936749A (en) * | 1988-12-21 | 1990-06-26 | General Electric Company | Blade-to-blade vibration damper |
EP0437977A1 (fr) * | 1990-01-18 | 1991-07-24 | United Technologies Corporation | Configuration de jante de disque de turbine |
US5201849A (en) * | 1990-12-10 | 1993-04-13 | General Electric Company | Turbine rotor seal body |
US5108261A (en) * | 1991-07-11 | 1992-04-28 | United Technologies Corporation | Compressor disk assembly |
US5302085A (en) * | 1992-02-03 | 1994-04-12 | General Electric Company | Turbine blade damper |
US5261790A (en) * | 1992-02-03 | 1993-11-16 | General Electric Company | Retention device for turbine blade damper |
US5281097A (en) * | 1992-11-20 | 1994-01-25 | General Electric Company | Thermal control damper for turbine rotors |
US5228835A (en) * | 1992-11-24 | 1993-07-20 | United Technologies Corporation | Gas turbine blade seal |
US5415526A (en) * | 1993-11-19 | 1995-05-16 | Mercadante; Anthony J. | Coolable rotor assembly |
US5573375A (en) * | 1994-12-14 | 1996-11-12 | United Technologies Corporation | Turbine engine rotor blade platform sealing and vibration damping device |
US5513955A (en) * | 1994-12-14 | 1996-05-07 | United Technologies Corporation | Turbine engine rotor blade platform seal |
US5827047A (en) * | 1996-06-27 | 1998-10-27 | United Technologies Corporation | Turbine blade damper and seal |
US5924699A (en) * | 1996-12-24 | 1999-07-20 | United Technologies Corporation | Turbine blade platform seal |
US5820338A (en) * | 1997-04-24 | 1998-10-13 | United Technologies Corporation | Fan blade interplatform seal |
US6750238B1 (en) * | 2000-05-12 | 2004-06-15 | The University Of Toledo | Aralkyl ester soft drugs |
FR2840352B1 (fr) * | 2002-05-30 | 2005-12-16 | Snecma Moteurs | Maitrise de la zone de fuite sous plate-forme d'aube |
US7121802B2 (en) * | 2004-07-13 | 2006-10-17 | General Electric Company | Selectively thinned turbine blade |
US7467924B2 (en) * | 2005-08-16 | 2008-12-23 | United Technologies Corporation | Turbine blade including revised platform |
US7371044B2 (en) * | 2005-10-06 | 2008-05-13 | Siemens Power Generation, Inc. | Seal plate for turbine rotor assembly between turbine blade and turbine vane |
US20090096174A1 (en) * | 2007-02-28 | 2009-04-16 | United Technologies Corporation | Blade outer air seal for a gas turbine engine |
GB201016597D0 (en) * | 2010-10-04 | 2010-11-17 | Rolls Royce Plc | Turbine disc cooling arrangement |
US8905716B2 (en) | 2012-05-31 | 2014-12-09 | United Technologies Corporation | Ladder seal system for gas turbine engines |
US9587495B2 (en) | 2012-06-29 | 2017-03-07 | United Technologies Corporation | Mistake proof damper pocket seals |
EP2900999B1 (fr) | 2012-09-28 | 2019-10-09 | United Technologies Corporation | Étouffoir doté d'une rétention améliorée |
US9920627B2 (en) | 2014-05-22 | 2018-03-20 | United Technologies Corporation | Rotor heat shield |
US10458264B2 (en) * | 2015-05-05 | 2019-10-29 | United Technologies Corporation | Seal arrangement for turbine engine component |
EP3438410B1 (fr) | 2017-08-01 | 2021-09-29 | General Electric Company | Système d'étanchéité pour machine rotative |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA697702A (en) * | 1964-11-10 | John A. Wilson, Iii | Bladed rotor and baffle assembly | |
CH335695A (de) * | 1955-12-06 | 1959-01-31 | Bbc Brown Boveri & Cie | Fuss zur Befestigung von Schaufeln in Läufern von Turbomaschinen |
US2999631A (en) * | 1958-09-05 | 1961-09-12 | Gen Electric | Dual airfoil |
US3104093A (en) * | 1961-04-11 | 1963-09-17 | United Aircraft Corp | Blade damping device |
GB996729A (en) * | 1963-12-16 | 1965-06-30 | Rolls Royce | Improvements relating to turbines and compressors |
US3309058A (en) * | 1965-06-21 | 1967-03-14 | Rolls Royce | Bladed rotor |
US3752598A (en) * | 1971-11-17 | 1973-08-14 | United Aircraft Corp | Segmented duct seal |
US3841792A (en) * | 1973-03-09 | 1974-10-15 | Westinghouse Electric Corp | Turbomachine blade lock and seal device |
US3936230A (en) * | 1974-05-09 | 1976-02-03 | The United States Of America As Represented By The Secretary Of The Air Force | Self-supported, self-locating seal for turbine engines |
US4029436A (en) * | 1975-06-17 | 1977-06-14 | United Technologies Corporation | Blade root feather seal |
DE2658345A1 (de) * | 1976-12-23 | 1978-06-29 | Motoren Turbinen Union | Rezirkulationsdichtung fuer stroemungsmaschinen, insbesondere gasturbinenstrahltriebwerke |
GB1549152A (en) * | 1977-01-11 | 1979-08-01 | Rolls Royce | Rotor stage for a gas trubine engine |
US4183720A (en) * | 1978-01-03 | 1980-01-15 | The United States Of America As Represented By The Secretary Of The Air Force | Composite fan blade platform double wedge centrifugal seal |
SU836371A1 (ru) * | 1979-04-09 | 1981-06-07 | Предприятие П/Я М-5641 | Рабочее колесо турбомашины |
US4326835A (en) * | 1979-10-29 | 1982-04-27 | General Motors Corporation | Blade platform seal for ceramic/metal rotor assembly |
FR2503247B1 (fr) * | 1981-04-07 | 1985-06-14 | Snecma | Perfectionnements aux etages de turbine a gaz de turboreacteurs munis de moyens de refroidissement par air du disque de la roue de la turbine |
US4455122A (en) * | 1981-12-14 | 1984-06-19 | United Technologies Corporation | Blade to blade vibration damper |
US4422827A (en) * | 1982-02-18 | 1983-12-27 | United Technologies Corporation | Blade root seal |
-
1983
- 1983-10-24 US US06/544,933 patent/US4505642A/en not_active Expired - Lifetime
-
1984
- 1984-09-14 CA CA000463227A patent/CA1209483A/fr not_active Expired
- 1984-10-04 IL IL73167A patent/IL73167A/xx unknown
- 1984-10-05 DE DE19843436663 patent/DE3436663A1/de not_active Withdrawn
- 1984-10-11 GR GR5980A patent/GR80598B/el unknown
- 1984-10-12 NL NL8403110A patent/NL8403110A/nl not_active Application Discontinuation
- 1984-10-16 CH CH4940/84A patent/CH665684A5/de not_active IP Right Cessation
- 1984-10-17 TR TR7663A patent/TR22355A/xx unknown
- 1984-10-18 BE BE0/213851A patent/BE900845A/fr not_active IP Right Cessation
- 1984-10-23 DK DK504784A patent/DK504784A/da not_active Application Discontinuation
- 1984-10-24 YU YU01818/84A patent/YU181884A/xx unknown
- 1984-10-24 JP JP59223824A patent/JPS60111003A/ja active Pending
- 1984-10-24 KR KR1019840006622A patent/KR850003923A/ko not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
US4505642A (en) | 1985-03-19 |
TR22355A (tr) | 1987-02-24 |
IL73167A (en) | 1989-03-31 |
JPS60111003A (ja) | 1985-06-17 |
NL8403110A (nl) | 1985-05-17 |
DK504784D0 (da) | 1984-10-23 |
CH665684A5 (de) | 1988-05-31 |
CA1209483A (fr) | 1986-08-12 |
KR850003923A (ko) | 1985-06-29 |
YU181884A (en) | 1988-06-30 |
GR80598B (en) | 1984-12-18 |
DE3436663A1 (de) | 1985-05-09 |
DK504784A (da) | 1985-04-25 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
RE | Patent lapsed |
Owner name: UNITED TECHNOLOGIES CORP. Effective date: 19891031 |