FR379209A - Improvements to elastic fluid turbines - Google Patents
Improvements to elastic fluid turbinesInfo
- Publication number
- FR379209A FR379209A FR379209A FR379209DA FR379209A FR 379209 A FR379209 A FR 379209A FR 379209 A FR379209 A FR 379209A FR 379209D A FR379209D A FR 379209DA FR 379209 A FR379209 A FR 379209A
- Authority
- FR
- France
- Prior art keywords
- elastic fluid
- fluid turbines
- turbines
- elastic
- fluid
- 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
Links
Classifications
-
- 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
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
-
- 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
- F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/16—Sealings between relatively-moving surfaces
- F16J15/32—Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings
- F16J15/3284—Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings characterised by their structure; Selection of materials
- F16J15/3288—Filamentary structures, e.g. brush seals
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/55—Seals
- F05D2240/56—Brush seals
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB379209X | 1906-07-03 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR379209A true FR379209A (en) | 1907-10-29 |
Family
ID=1425518
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR379209A Expired FR379209A (en) | 1906-07-03 | 1907-06-25 | Improvements to elastic fluid turbines |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR379209A (en) |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1057827B (en) * | 1955-08-18 | 1959-05-21 | Stroemungsmasch Anst | Fixed impeller rim for gas turbines |
FR2545537A1 (en) * | 1983-05-06 | 1984-11-09 | Mtu Muenchen Gmbh | TURBOCHARGER COMPRISING A RUNNING TRIM |
FR2551130A1 (en) * | 1983-08-26 | 1985-03-01 | Gen Electric | FRICTION INSENSITIVE TURBINE ENVELOPE |
FR2660371A1 (en) * | 1990-04-03 | 1991-10-04 | Gen Electric | INTER-FLOOR SEALING ARRANGEMENT FOR BLADES OF ROTOR BLADES TURNING IN A TURBINE ENGINE. |
EP0572312A1 (en) * | 1992-05-27 | 1993-12-01 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Sealing arrangement between stator blade rows and a rotating rotor drum |
FR2724412A1 (en) * | 1994-09-14 | 1996-03-15 | Snecma | TURBOMACHINE DAWN IN COMPOSITE MATERIAL WITH SEAL AND METHOD OF MAKING SAME |
EP0905421A1 (en) * | 1997-09-25 | 1999-03-31 | Asea Brown Boveri AG | Brush seal |
WO2000045070A1 (en) * | 1999-01-27 | 2000-08-03 | General Electric Company | Method and apparatus for eliminating thermal bowing of steam turbine rotors |
WO2002012759A3 (en) * | 2000-08-09 | 2002-08-01 | Advanced Component & Materials | Brush seal assembly, method of manufacture and use |
US6536773B2 (en) | 2000-11-06 | 2003-03-25 | Advanced Components & Materials, Inc. | Compliant brush shroud assembly for gas turbine engine compressors |
US6880829B1 (en) | 2000-11-06 | 2005-04-19 | Advanced Components & Materials, Inc. | Compliant brush shroud assembly for gas turbine engine compressors |
US6913265B2 (en) | 2000-08-09 | 2005-07-05 | Advanced Components & Materials, Inc. | Brush seal assembly, method of manufacture and use |
-
1907
- 1907-06-25 FR FR379209A patent/FR379209A/en not_active Expired
Cited By (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1057827B (en) * | 1955-08-18 | 1959-05-21 | Stroemungsmasch Anst | Fixed impeller rim for gas turbines |
FR2545537A1 (en) * | 1983-05-06 | 1984-11-09 | Mtu Muenchen Gmbh | TURBOCHARGER COMPRISING A RUNNING TRIM |
FR2551130A1 (en) * | 1983-08-26 | 1985-03-01 | Gen Electric | FRICTION INSENSITIVE TURBINE ENVELOPE |
FR2660371A1 (en) * | 1990-04-03 | 1991-10-04 | Gen Electric | INTER-FLOOR SEALING ARRANGEMENT FOR BLADES OF ROTOR BLADES TURNING IN A TURBINE ENGINE. |
EP0572312A1 (en) * | 1992-05-27 | 1993-12-01 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Sealing arrangement between stator blade rows and a rotating rotor drum |
FR2691749A1 (en) * | 1992-05-27 | 1993-12-03 | Snecma | Sealing device between stages of blades and a rotating drum in particular to avoid leaks around stages of stator blades. |
US5328328A (en) * | 1992-05-27 | 1994-07-12 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Sealing device between blade stages and a rotary drum, particularly for preventing leaks around the stages of straightener blades |
FR2724412A1 (en) * | 1994-09-14 | 1996-03-15 | Snecma | TURBOMACHINE DAWN IN COMPOSITE MATERIAL WITH SEAL AND METHOD OF MAKING SAME |
EP0708227A1 (en) | 1994-09-14 | 1996-04-24 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Composite turbomachine blade with integrated brush seal and manufacturing method therefor |
US5628622A (en) * | 1994-09-14 | 1997-05-13 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Composite material turbine engine blade equipped with a seal and its production process |
EP0905421A1 (en) * | 1997-09-25 | 1999-03-31 | Asea Brown Boveri AG | Brush seal |
US6471212B1 (en) | 1997-09-25 | 2002-10-29 | Alstom | Brush seal |
WO2000045070A1 (en) * | 1999-01-27 | 2000-08-03 | General Electric Company | Method and apparatus for eliminating thermal bowing of steam turbine rotors |
US6168377B1 (en) | 1999-01-27 | 2001-01-02 | General Electric Co. | Method and apparatus for eliminating thermal bowing of steam turbine rotors |
WO2002012759A3 (en) * | 2000-08-09 | 2002-08-01 | Advanced Component & Materials | Brush seal assembly, method of manufacture and use |
GB2380774A (en) * | 2000-08-09 | 2003-04-16 | Advanced Components & Material | Brush seal assembly, method of manufacture and use |
GB2380774B (en) * | 2000-08-09 | 2004-04-14 | Advanced Components & Material | Brush seal assembly, method of manufacture and use |
US6913265B2 (en) | 2000-08-09 | 2005-07-05 | Advanced Components & Materials, Inc. | Brush seal assembly, method of manufacture and use |
US6536773B2 (en) | 2000-11-06 | 2003-03-25 | Advanced Components & Materials, Inc. | Compliant brush shroud assembly for gas turbine engine compressors |
US6880829B1 (en) | 2000-11-06 | 2005-04-19 | Advanced Components & Materials, Inc. | Compliant brush shroud assembly for gas turbine engine compressors |
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