IT1126488B - Tenuta di turbomotore a gas e metodo per fare la medesima - Google Patents
Tenuta di turbomotore a gas e metodo per fare la medesimaInfo
- Publication number
- IT1126488B IT1126488B IT7927878A IT2787879A IT1126488B IT 1126488 B IT1126488 B IT 1126488B IT 7927878 A IT7927878 A IT 7927878A IT 2787879 A IT2787879 A IT 2787879A IT 1126488 B IT1126488 B IT 1126488B
- Authority
- IT
- Italy
- Prior art keywords
- seal
- making
- same
- turbo engine
- gas turbo
- Prior art date
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
- F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/002—Manufacture of articles essentially made from metallic fibres
-
- 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
- F16J15/44—Free-space packings
- F16J15/445—Free-space packings with means for adjusting the clearance
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
-
- 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
- Y10S277/00—Seal for a joint or juncture
- Y10S277/935—Seal made of a particular material
- Y10S277/936—Composite
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
- Gasket Seals (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/969,915 US4257735A (en) | 1978-12-15 | 1978-12-15 | Gas turbine engine seal and method for making same |
Publications (2)
Publication Number | Publication Date |
---|---|
IT7927878A0 IT7927878A0 (it) | 1979-12-07 |
IT1126488B true IT1126488B (it) | 1986-05-21 |
Family
ID=25516171
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT7927878A IT1126488B (it) | 1978-12-15 | 1979-12-07 | Tenuta di turbomotore a gas e metodo per fare la medesima |
Country Status (8)
Country | Link |
---|---|
US (1) | US4257735A (it) |
JP (1) | JPS55101733A (it) |
CA (1) | CA1128866A (it) |
DE (1) | DE2950150A1 (it) |
FR (1) | FR2444162B1 (it) |
GB (1) | GB2042928B (it) |
IL (1) | IL58400A (it) |
IT (1) | IT1126488B (it) |
Families Citing this family (44)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2087986B (en) * | 1980-11-25 | 1984-08-30 | Rolls Royce | Magnetic seal |
US4586717A (en) * | 1980-12-24 | 1986-05-06 | Conoco Inc. | Throttling bushing for shaft seal |
US4422648A (en) * | 1982-06-17 | 1983-12-27 | United Technologies Corporation | Ceramic faced outer air seal for gas turbine engines |
US4460185A (en) * | 1982-08-23 | 1984-07-17 | General Electric Company | Seal including a non-metallic abradable material |
DE3579684D1 (de) * | 1984-12-24 | 1990-10-18 | United Technologies Corp | Abschleifbare dichtung mit besonderem erosionswiderstand. |
US4754984A (en) * | 1987-01-02 | 1988-07-05 | The United States Of America As Represented By The Secretary Of The Navy | Dual-seal-ring shaft seal |
JPH01310670A (ja) * | 1988-06-08 | 1989-12-14 | Ootone Bussan:Kk | ティッシュペーパ |
US4989886A (en) * | 1988-12-30 | 1991-02-05 | Textron Inc. | Braided filamentary sealing element |
DE4130946C1 (it) * | 1991-09-18 | 1992-09-03 | Mtu Muenchen Gmbh | |
DE19750516A1 (de) * | 1997-11-14 | 1999-05-20 | Asea Brown Boveri | Abreibbare Dichtung |
DE19848104A1 (de) | 1998-10-19 | 2000-04-20 | Asea Brown Boveri | Turbinenschaufel |
US6148518A (en) * | 1998-12-22 | 2000-11-21 | United Technologies Corporation | Method of assembling a rotary machine |
US6203273B1 (en) | 1998-12-22 | 2001-03-20 | United Technologies Corporation | Rotary machine |
JP2000192173A (ja) * | 1998-12-23 | 2000-07-11 | United Technol Corp <Utc> | 摩耗性材料および摩耗性被覆を有する金属製部品 |
SG90198A1 (en) * | 1999-12-23 | 2002-07-23 | United Technologies Corp | Composite abradable material |
US6334617B1 (en) * | 2000-03-02 | 2002-01-01 | United Technologies Corporation | Composite abradable material |
EP1152124A1 (de) * | 2000-05-04 | 2001-11-07 | Siemens Aktiengesellschaft | Dichtungsanordnung |
JP4496650B2 (ja) * | 2001-01-10 | 2010-07-07 | 富士電機システムズ株式会社 | 蒸気タービン |
US6887530B2 (en) | 2002-06-07 | 2005-05-03 | Sulzer Metco (Canada) Inc. | Thermal spray compositions for abradable seals |
US6808756B2 (en) | 2003-01-17 | 2004-10-26 | Sulzer Metco (Canada) Inc. | Thermal spray composition and method of deposition for abradable seals |
WO2004113771A2 (en) * | 2003-06-20 | 2004-12-29 | Elliott Company | Hybrid abradable labyrinth damper seal |
US20060237914A1 (en) * | 2003-06-20 | 2006-10-26 | Elliott Company | Swirl-reversal abradable labyrinth seal |
US8020875B2 (en) * | 2006-02-21 | 2011-09-20 | United Technologies Corporation | Turbine friendly abradable material |
US20070197719A1 (en) * | 2006-02-21 | 2007-08-23 | United Technologies Corporation | Turbine friendly abradable material |
GB0613715D0 (en) | 2006-07-11 | 2006-08-23 | Rolls Royce Plc | A seal between relatively moveable members |
US8205335B2 (en) * | 2007-06-12 | 2012-06-26 | United Technologies Corporation | Method of repairing knife edge seals |
US8001669B2 (en) * | 2007-09-27 | 2011-08-23 | United Technologies Corporation | Pressurized cleaning of a turbine engine component |
JP4668976B2 (ja) * | 2007-12-04 | 2011-04-13 | 株式会社日立製作所 | 蒸気タービンのシール構造 |
JP5101317B2 (ja) * | 2008-01-25 | 2012-12-19 | 三菱重工業株式会社 | シール構造 |
DE102008019890A1 (de) * | 2008-04-21 | 2009-10-22 | Mtu Aero Engines Gmbh | Dichtungsanordnung |
US20100050649A1 (en) * | 2008-09-04 | 2010-03-04 | Allen David B | Combustor device and transition duct assembly |
GB0822416D0 (en) * | 2008-12-10 | 2009-01-14 | Rolls Royce Plc | A seal and a method of manufacturing a seal |
DE102009016803A1 (de) * | 2009-04-09 | 2010-10-14 | Rolls-Royce Deutschland Ltd & Co Kg | Labyrinth-Anstreifdichtung für eine Strömungsmaschine |
US20120224962A1 (en) | 2009-11-13 | 2012-09-06 | Ihi Corporation | Seal structure of fluid device |
JP5087147B2 (ja) * | 2011-01-13 | 2012-11-28 | 株式会社日立製作所 | 蒸気タービン |
US20130017070A1 (en) * | 2011-07-13 | 2013-01-17 | General Electric Company | Turbine seal, turbine, and process of fabricating a turbine seal |
US9322478B2 (en) * | 2012-07-31 | 2016-04-26 | General Electric Company | Seal system and method for rotary machine |
US20140037970A1 (en) * | 2012-08-03 | 2014-02-06 | General Electric Company | Reinforced articles and methods of making the same |
DE102013223585A1 (de) | 2013-11-19 | 2015-06-03 | MTU Aero Engines AG | Einlaufbelag auf Basis von Metallfasern |
EP2886801B1 (en) * | 2013-12-20 | 2019-04-24 | Ansaldo Energia IP UK Limited | Seal system for a gas turbine and corresponding gas turbine |
EP3037570B1 (en) * | 2014-12-15 | 2019-08-21 | United Technologies Corporation | Method of forming a seal coating |
FR3085180B1 (fr) * | 2018-08-24 | 2020-11-27 | Safran Aircraft Engines | Ensemble aubage pour stator de turbine de turbomachine comprenant des nervures d'etancheite inclinees |
US11555410B2 (en) * | 2020-02-17 | 2023-01-17 | Pratt & Whitney Canada Corp. | Labyrinth seal with variable seal clearance |
KR20240055095A (ko) * | 2022-05-17 | 2024-04-26 | 미츠비시 파워 가부시키가이샤 | 축 시일 장치 및 회전 기계 |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2840343A (en) * | 1955-10-14 | 1958-06-24 | Jr David E Brandt | Reduction of rotating tip clearance using segmented wear strips |
GB851267A (en) * | 1958-04-28 | 1960-10-12 | Gen Motors Corp | Improvements relating to axial-flow compressors |
US3053694A (en) * | 1961-02-20 | 1962-09-11 | Gen Electric | Abradable material |
FR1546474A (fr) * | 1966-03-11 | 1968-11-22 | Gen Electric | Matrice d'étanchéité |
US3346175A (en) * | 1966-04-01 | 1967-10-10 | Gen Motors Corp | Plastic coating for compressors |
US3547455A (en) * | 1969-05-02 | 1970-12-15 | Gen Electric | Rotary seal including organic abradable material |
US3575427A (en) * | 1969-11-03 | 1971-04-20 | United Aircraft Corp | Composite abradable seal |
US3701536A (en) * | 1970-05-19 | 1972-10-31 | Garrett Corp | Labyrinth seal |
US3836156A (en) * | 1971-07-19 | 1974-09-17 | United Aircraft Canada | Ablative seal |
US3825364A (en) * | 1972-06-09 | 1974-07-23 | Gen Electric | Porous abradable turbine shroud |
CH589221A5 (it) * | 1973-06-29 | 1977-06-30 | Bbc Brown Boveri & Cie | |
US4149823A (en) * | 1973-06-29 | 1979-04-17 | Bbc Brown, Boveri & Company Limited | Method of maintaining optimum minimum operating clearance between rotor and stator components of fluid-flow machines |
GB1512811A (en) * | 1974-02-28 | 1978-06-01 | Brunswick Corp | Abradable seal material and composition thereof |
US4139376A (en) * | 1974-02-28 | 1979-02-13 | Brunswick Corporation | Abradable seal material and composition thereof |
US4135851A (en) * | 1977-05-27 | 1979-01-23 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Composite seal for turbomachinery |
-
1978
- 1978-12-15 US US05/969,915 patent/US4257735A/en not_active Expired - Lifetime
-
1979
- 1979-10-05 IL IL58400A patent/IL58400A/xx unknown
- 1979-11-30 CA CA340,964A patent/CA1128866A/en not_active Expired
- 1979-12-07 IT IT7927878A patent/IT1126488B/it active
- 1979-12-12 GB GB7942899A patent/GB2042928B/en not_active Expired
- 1979-12-13 DE DE19792950150 patent/DE2950150A1/de active Granted
- 1979-12-14 FR FR7930669A patent/FR2444162B1/fr not_active Expired
- 1979-12-14 JP JP16168979A patent/JPS55101733A/ja active Granted
Also Published As
Publication number | Publication date |
---|---|
JPS55101733A (en) | 1980-08-04 |
IL58400A (en) | 1981-09-13 |
DE2950150C2 (it) | 1990-01-11 |
JPS6250654B2 (it) | 1987-10-26 |
DE2950150A1 (de) | 1980-06-26 |
US4257735A (en) | 1981-03-24 |
IL58400A0 (en) | 1980-01-31 |
CA1128866A (en) | 1982-08-03 |
IT7927878A0 (it) | 1979-12-07 |
FR2444162B1 (fr) | 1986-06-27 |
FR2444162A1 (fr) | 1980-07-11 |
GB2042928B (en) | 1983-02-23 |
GB2042928A (en) | 1980-10-01 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
TA | Fee payment date (situation as of event date), data collected since 19931001 |
Effective date: 19921216 |