IT1260448B - Tenuta di ricircolazione per un diffusore di scarico per turbina a gas - Google Patents
Tenuta di ricircolazione per un diffusore di scarico per turbina a gasInfo
- Publication number
- IT1260448B IT1260448B ITMI920137A ITMI920137A IT1260448B IT 1260448 B IT1260448 B IT 1260448B IT MI920137 A ITMI920137 A IT MI920137A IT MI920137 A ITMI920137 A IT MI920137A IT 1260448 B IT1260448 B IT 1260448B
- Authority
- IT
- Italy
- Prior art keywords
- seal
- gas turbine
- cylinder
- fabric
- channels
- Prior art date
Links
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
- 239000011248 coating agent Substances 0.000 abstract 2
- 238000000576 coating method Methods 0.000 abstract 2
- 239000004744 fabric Substances 0.000 abstract 2
- 239000011152 fibreglass Substances 0.000 abstract 1
- 230000000717 retained effect Effects 0.000 abstract 1
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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/30—Exhaust heads, chambers, or the like
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Gasket Seals (AREA)
Abstract
E' realizzata una tenuta per impedire la ricircolazione di gas caldo attraverso una cavità anulare formata tra il rivestimento esterno di circolazione di un diffusore ed un cilindro di scarico nella sezione di scarico di una turbina a gas. La tenuta è formata da un tessuto per alta temperatura, come per esempio fibra di vetro, che è inserito tra due strati di una maglia fitta. La tenuta è costituita da una molteplicità di segmenti arcuati. Benché il tessuto abbia una forma rettangolare quando si trova nel suo stato non deformato, esso assume una forma arcuata come conseguenza del fissaggio mediante raggrinzimento entro canali arcuati interno ed esterno. La tenuta è trattenuta facendo scorrere i canali in scanalature circonferenziali nel cilindro e nel rivestimento di circolazione esterno. Un'ansa di espansione è formata nella tenuta per consentire l'espansione differenziale tra il cilindro di scarico e il rivestimento esterno.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US07/652,693 US5104286A (en) | 1991-02-08 | 1991-02-08 | Recirculation seal for a gas turbine exhaust diffuser |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| ITMI920137A0 ITMI920137A0 (it) | 1992-01-27 |
| ITMI920137A1 ITMI920137A1 (it) | 1993-07-27 |
| IT1260448B true IT1260448B (it) | 1996-04-09 |
Family
ID=24617782
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ITMI920137A IT1260448B (it) | 1991-02-08 | 1992-01-27 | Tenuta di ricircolazione per un diffusore di scarico per turbina a gas |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US5104286A (it) |
| JP (1) | JPH0814258B2 (it) |
| CA (1) | CA2060876A1 (it) |
| IT (1) | IT1260448B (it) |
Families Citing this family (51)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE4232385A1 (de) | 1992-09-26 | 1994-03-31 | Asea Brown Boveri | Gasturbine mit angeflanschtem Abgasgehäuse |
| JP3513170B2 (ja) | 1993-02-26 | 2004-03-31 | 三菱重工業株式会社 | 排気ディフューザー |
| FR2713709B1 (fr) * | 1993-12-08 | 1996-01-12 | Snecma | Paroi de turbomachine comprenant un corps d'étanchéité. |
| US5657998A (en) * | 1994-09-19 | 1997-08-19 | General Electric Company | Gas-path leakage seal for a gas turbine |
| US5509669A (en) * | 1995-06-19 | 1996-04-23 | General Electric Company | Gas-path leakage seal for a gas turbine |
| US5586773A (en) * | 1995-06-19 | 1996-12-24 | General Electric Company | Gas-path leakage seal for a gas turbine made from metallic mesh |
| US5915697A (en) * | 1997-09-22 | 1999-06-29 | General Electric Company | Flexible cloth seal assembly |
| DE19848103A1 (de) * | 1998-10-19 | 2000-04-20 | Asea Brown Boveri | Dichtungsanordnung |
| IL136032A (en) * | 2000-05-09 | 2003-12-10 | Iscar Ltd | Tool joint |
| US6502825B2 (en) | 2000-12-26 | 2003-01-07 | General Electric Company | Pressure activated cloth seal |
| US6547256B2 (en) | 2000-12-26 | 2003-04-15 | General Electric Company | Cloth ring seal |
| RU2297566C2 (ru) * | 2002-07-03 | 2007-04-20 | Альстом Текнолоджи Лтд | Щелевое уплотнение для герметизации щели между двумя соседними конструкционными элементами |
| US6883807B2 (en) | 2002-09-13 | 2005-04-26 | Seimens Westinghouse Power Corporation | Multidirectional turbine shim seal |
| US6733234B2 (en) | 2002-09-13 | 2004-05-11 | Siemens Westinghouse Power Corporation | Biased wear resistant turbine seal assembly |
| US6792758B2 (en) | 2002-11-07 | 2004-09-21 | Siemens Westinghouse Power Corporation | Variable exhaust struts shields |
| GB0228748D0 (en) * | 2002-12-10 | 2003-01-15 | Alstom Switzerland Ltd | Sealing arrangement |
| US6942452B2 (en) * | 2002-12-17 | 2005-09-13 | Pratt & Whitney Canada Corp. | Grommeted bypass duct penetration |
| JP4342840B2 (ja) * | 2003-05-30 | 2009-10-14 | 株式会社東芝 | 蒸気タービン |
| DE102004016452B4 (de) | 2004-03-31 | 2020-06-10 | Ansaldo Energia Ip Uk Limited | Strömungsmaschine |
| JP4869575B2 (ja) * | 2004-09-28 | 2012-02-08 | 三菱電線工業株式会社 | シール |
| JP2006307733A (ja) * | 2005-04-28 | 2006-11-09 | Mitsubishi Heavy Ind Ltd | ガスタービン排気ディフューザ |
| US7845649B2 (en) * | 2005-09-30 | 2010-12-07 | General Electric Company | Methods and apparatus to facilitate sealing high pressure joints |
| US20070081892A1 (en) * | 2005-10-06 | 2007-04-12 | General Electric Company | Steam turbine exhaust diffuser |
| FR2892148B1 (fr) * | 2005-10-19 | 2011-07-22 | Snecma | Fourreau d'arbre de turboreacteur et turboreacteur comportant ce fourreau |
| US7793507B2 (en) | 2006-09-07 | 2010-09-14 | General Electric Company | Expansion joint for gas turbines |
| GB2449477B (en) * | 2007-05-24 | 2009-05-13 | Rolls Royce Plc | A duct installation |
| CN103557035B (zh) * | 2008-02-27 | 2015-04-29 | 三菱日立电力系统株式会社 | 排气室的连结结构、涡轮的支撑结构以及燃气轮机 |
| US8523514B2 (en) * | 2009-11-25 | 2013-09-03 | United Technologies Corporation | Composite slider seal for turbojet penetration |
| US9206705B2 (en) * | 2012-03-07 | 2015-12-08 | Mitsubishi Hitachi Power Systems, Ltd. | Sealing device and gas turbine having the same |
| IN2014DN07620A (it) | 2012-03-20 | 2015-05-15 | Alstom Technology Ltd | |
| EP2679780B8 (en) | 2012-06-28 | 2016-09-14 | General Electric Technology GmbH | Diffuser for the exhaust section of a gas turbine and gas turbine with such a diffuser |
| US20140062034A1 (en) * | 2012-08-06 | 2014-03-06 | General Electric Company | Gas path leakage seal for a turbine |
| WO2014068355A1 (en) * | 2012-10-30 | 2014-05-08 | General Electric Company | Gas turbine engine exhaust system and corresponding method for accessing turbine buckets |
| US9822664B1 (en) * | 2013-03-14 | 2017-11-21 | Calpine Corporation | Turbine exhaust cylinder baffle seal and method for installing turbine exhaust cylinder baffle seal |
| JP6125329B2 (ja) * | 2013-05-27 | 2017-05-10 | 株式会社東芝 | 静止部シール構造 |
| EP3044446B1 (en) * | 2013-09-13 | 2021-11-17 | Raytheon Technologies Corporation | Large displacement high temperature seal |
| US20150078892A1 (en) * | 2013-09-17 | 2015-03-19 | General Electric Company | Eccentric coupling device and method for coupling mating casings in a turbomachine |
| WO2015084460A2 (en) * | 2013-10-02 | 2015-06-11 | United Technologies Corporation | Recirculation seal for use in a gas turbine engine |
| EP2863019B1 (de) * | 2013-10-18 | 2017-03-29 | Siemens Aktiengesellschaft | Dichtungsanordnung |
| DE102013223690A1 (de) * | 2013-11-20 | 2015-05-21 | Siemens Aktiengesellschaft | Dichtungsanordnung einer Turbine |
| US9598981B2 (en) * | 2013-11-22 | 2017-03-21 | Siemens Energy, Inc. | Industrial gas turbine exhaust system diffuser inlet lip |
| WO2015116399A1 (en) * | 2014-01-28 | 2015-08-06 | United Technologies Corporation | Flexible cavity seal for gas turbine engines |
| JP6203090B2 (ja) | 2014-03-14 | 2017-09-27 | 三菱日立パワーシステムズ株式会社 | 排気室入口側部材、排気室、ガスタービンおよび最終段タービン動翼取出方法 |
| EP2947283B1 (fr) | 2014-05-23 | 2017-01-11 | GE Energy Products France SNC | Structure d'isolation thermo-acoustique pour échappement de machine tournante |
| US10047622B2 (en) | 2014-07-22 | 2018-08-14 | General Electric Company | Flexible layered seal for turbomachinery |
| US9650919B2 (en) | 2014-08-04 | 2017-05-16 | Siemens Energy, Inc. | Moveable sealing arrangement for a gas turbine diffuser gap |
| EP3073056B1 (en) * | 2015-03-25 | 2018-01-03 | Ansaldo Energia IP UK Limited | Wire seal |
| US20160312633A1 (en) * | 2015-04-24 | 2016-10-27 | General Electric Company | Composite seals for turbomachinery |
| US10041377B2 (en) * | 2015-11-24 | 2018-08-07 | General Electric Company | System and method for turbine diffuser |
| EP3441578B1 (en) * | 2017-08-11 | 2021-03-03 | General Electric Company | Turbine exhaust diffuser |
| KR102475240B1 (ko) * | 2018-05-21 | 2022-12-07 | 이구루코교 가부시기가이샤 | 시일 장치 |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB190901724A (en) * | 1909-01-25 | 1909-09-30 | James Walker | Improvements relating to Packing. |
| US2314289A (en) * | 1941-05-24 | 1943-03-16 | Gen Electric | Elastic fluid turbine |
| US2766055A (en) * | 1952-12-30 | 1956-10-09 | Johns Manville | Gaskets |
| US3020185A (en) * | 1958-07-28 | 1962-02-06 | Connecticut Hard Rubber Co | Wire reinforced polytetrafluoroethylene seal |
| JPS5270212A (en) * | 1975-12-10 | 1977-06-11 | Hitachi Ltd | Dashboard equipment |
| GB2070700B (en) * | 1980-03-01 | 1983-10-05 | Rolls Royce | Gas turbine seals |
| GB2075614B (en) * | 1980-05-10 | 1984-11-28 | Rolls Royce | Annular seal |
| US4462603A (en) * | 1983-03-16 | 1984-07-31 | Metex Corporation | Knitted wire mesh exhaust coupling seal with refractory metallic oxide impregnant |
| US4747750A (en) * | 1986-01-17 | 1988-05-31 | United Technologies Corporation | Transition duct seal |
| US4932207A (en) * | 1988-12-28 | 1990-06-12 | Sundstrand Corporation | Segmented seal plate for a turbine engine |
-
1991
- 1991-02-08 US US07/652,693 patent/US5104286A/en not_active Expired - Lifetime
-
1992
- 1992-01-27 IT ITMI920137A patent/IT1260448B/it active IP Right Grant
- 1992-02-06 JP JP4021034A patent/JPH0814258B2/ja not_active Expired - Fee Related
- 1992-02-07 CA CA002060876A patent/CA2060876A1/en not_active Abandoned
Also Published As
| Publication number | Publication date |
|---|---|
| ITMI920137A0 (it) | 1992-01-27 |
| US5104286A (en) | 1992-04-14 |
| CA2060876A1 (en) | 1992-08-09 |
| ITMI920137A1 (it) | 1993-07-27 |
| JPH0814258B2 (ja) | 1996-02-14 |
| JPH0552122A (ja) | 1993-03-02 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 0001 | Granted | ||
| TA | Fee payment date (situation as of event date), data collected since 19931001 |
Effective date: 19960130 |