HK1063343A1 - Flanged hollow structure - Google Patents
Flanged hollow structureInfo
- Publication number
- HK1063343A1 HK1063343A1 HK04106119.9A HK04106119A HK1063343A1 HK 1063343 A1 HK1063343 A1 HK 1063343A1 HK 04106119 A HK04106119 A HK 04106119A HK 1063343 A1 HK1063343 A1 HK 1063343A1
- Authority
- HK
- Hong Kong
- Prior art keywords
- hollow structure
- flanged hollow
- flanged
- hollow
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
-
- 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
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L23/00—Flanged joints
-
- 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
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L23/00—Flanged joints
- F16L23/16—Flanged joints characterised by the sealing means
- F16L23/24—Flanged joints characterised by the sealing means specially adapted for unequal expansion of the parts of the joint
-
- 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
- F05D2260/00—Function
- F05D2260/94—Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF]
-
- 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
- F05D2260/00—Function
- F05D2260/94—Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF]
- F05D2260/941—Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF] particularly aimed at mechanical or thermal stress reduction
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/50—Intrinsic material properties or characteristics
- F05D2300/502—Thermal properties
- F05D2300/5021—Expansivity
- F05D2300/50212—Expansivity dissimilar
-
- 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
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B2200/00—Constructional details of connections not covered for in other groups of this subclass
- F16B2200/50—Flanged connections
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/00005—Preventing fatigue failures or reducing mechanical stress in gas turbine components
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Flanged Joints, Insulating Joints, And Other Joints (AREA)
- Rod-Shaped Construction Members (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2001198916A JP4008212B2 (ja) | 2001-06-29 | 2001-06-29 | フランジ付中空構造物 |
PCT/JP2002/006641 WO2003002914A1 (fr) | 2001-06-29 | 2002-07-01 | Structure creuse a rebord |
Publications (1)
Publication Number | Publication Date |
---|---|
HK1063343A1 true HK1063343A1 (en) | 2004-12-24 |
Family
ID=19036273
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
HK04106119.9A HK1063343A1 (en) | 2001-06-29 | 2004-08-16 | Flanged hollow structure |
Country Status (8)
Country | Link |
---|---|
US (1) | US6662568B2 (de) |
EP (1) | EP1400755B1 (de) |
JP (1) | JP4008212B2 (de) |
CN (1) | CN1220845C (de) |
CA (1) | CA2421802C (de) |
DE (1) | DE60238984D1 (de) |
HK (1) | HK1063343A1 (de) |
WO (1) | WO2003002914A1 (de) |
Families Citing this family (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7178341B2 (en) * | 2004-06-17 | 2007-02-20 | Siemens Power Generation, Inc. | Multi-zone tubing assembly for a transition piece of a gas turbine |
US8015818B2 (en) * | 2005-02-22 | 2011-09-13 | Siemens Energy, Inc. | Cooled transition duct for a gas turbine engine |
JP4476152B2 (ja) * | 2005-04-01 | 2010-06-09 | 三菱重工業株式会社 | ガスタービン燃焼器 |
US7827801B2 (en) * | 2006-02-09 | 2010-11-09 | Siemens Energy, Inc. | Gas turbine engine transitions comprising closed cooled transition cooling channels |
US8141370B2 (en) * | 2006-08-08 | 2012-03-27 | General Electric Company | Methods and apparatus for radially compliant component mounting |
FR2942515B1 (fr) * | 2009-02-24 | 2015-07-03 | Saint Gobain Ct Recherches | Dispositif d'assemblage. |
US9234431B2 (en) * | 2010-07-20 | 2016-01-12 | Siemens Energy, Inc. | Seal assembly for controlling fluid flow |
US8721278B2 (en) | 2010-08-02 | 2014-05-13 | Siemens Energy, Inc. | Exhaust manifold flange connection |
WO2014158600A1 (en) | 2013-03-14 | 2014-10-02 | United Technologies Corporation | Compressor case snap assembly |
CN106922157B (zh) * | 2014-11-18 | 2018-12-18 | 西门子公司 | 具有插入件的过渡件导管出口框架 |
US10392950B2 (en) | 2015-05-07 | 2019-08-27 | General Electric Company | Turbine band anti-chording flanges |
US11149646B2 (en) * | 2015-09-02 | 2021-10-19 | General Electric Company | Piston ring assembly for a turbine engine |
US10584880B2 (en) | 2016-03-25 | 2020-03-10 | General Electric Company | Mounting of integrated combustor nozzles in a segmented annular combustion system |
US10605459B2 (en) | 2016-03-25 | 2020-03-31 | General Electric Company | Integrated combustor nozzle for a segmented annular combustion system |
US10563869B2 (en) | 2016-03-25 | 2020-02-18 | General Electric Company | Operation and turndown of a segmented annular combustion system |
US10641491B2 (en) | 2016-03-25 | 2020-05-05 | General Electric Company | Cooling of integrated combustor nozzle of segmented annular combustion system |
US10520194B2 (en) | 2016-03-25 | 2019-12-31 | General Electric Company | Radially stacked fuel injection module for a segmented annular combustion system |
US11428413B2 (en) | 2016-03-25 | 2022-08-30 | General Electric Company | Fuel injection module for segmented annular combustion system |
US10584876B2 (en) | 2016-03-25 | 2020-03-10 | General Electric Company | Micro-channel cooling of integrated combustor nozzle of a segmented annular combustion system |
US10830442B2 (en) | 2016-03-25 | 2020-11-10 | General Electric Company | Segmented annular combustion system with dual fuel capability |
US10641176B2 (en) | 2016-03-25 | 2020-05-05 | General Electric Company | Combustion system with panel fuel injector |
US10690350B2 (en) | 2016-11-28 | 2020-06-23 | General Electric Company | Combustor with axially staged fuel injection |
US11156362B2 (en) | 2016-11-28 | 2021-10-26 | General Electric Company | Combustor with axially staged fuel injection |
US11371702B2 (en) | 2020-08-31 | 2022-06-28 | General Electric Company | Impingement panel for a turbomachine |
US11460191B2 (en) | 2020-08-31 | 2022-10-04 | General Electric Company | Cooling insert for a turbomachine |
US11614233B2 (en) | 2020-08-31 | 2023-03-28 | General Electric Company | Impingement panel support structure and method of manufacture |
US11994293B2 (en) | 2020-08-31 | 2024-05-28 | General Electric Company | Impingement cooling apparatus support structure and method of manufacture |
US11994292B2 (en) | 2020-08-31 | 2024-05-28 | General Electric Company | Impingement cooling apparatus for turbomachine |
US11255545B1 (en) | 2020-10-26 | 2022-02-22 | General Electric Company | Integrated combustion nozzle having a unified head end |
US11767766B1 (en) | 2022-07-29 | 2023-09-26 | General Electric Company | Turbomachine airfoil having impingement cooling passages |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1362281A (en) * | 1970-08-17 | 1974-08-07 | Lausch H | Reinforced glass tubes |
JPH063267Y2 (ja) * | 1987-03-26 | 1994-01-26 | 日本碍子株式会社 | セラミックス製筒体の接合構造 |
JPH03141847A (ja) * | 1989-10-27 | 1991-06-17 | Nissan Motor Co Ltd | 内燃機関のシリンダブロック |
JPH063267A (ja) | 1992-06-20 | 1994-01-11 | Horiba Ltd | 有機化合物の検出方法およびその装置 |
JPH05215584A (ja) * | 1991-11-20 | 1993-08-24 | Tokico Ltd | 振動式測定装置 |
JPH06241363A (ja) * | 1993-02-10 | 1994-08-30 | Toshiomi Hayashi | フランジ継手組とその結合方法 |
GB2300909B (en) * | 1995-05-18 | 1998-09-30 | Europ Gas Turbines Ltd | A gas turbine gas duct arrangement |
US5906093A (en) * | 1997-02-21 | 1999-05-25 | Siemens Westinghouse Power Corporation | Gas turbine combustor transition |
US6018950A (en) * | 1997-06-13 | 2000-02-01 | Siemens Westinghouse Power Corporation | Combustion turbine modular cooling panel |
JP4031590B2 (ja) * | 1999-03-08 | 2008-01-09 | 三菱重工業株式会社 | 燃焼器の尾筒シール構造及びその構造を用いたガスタービン |
JP2001050448A (ja) * | 1999-08-02 | 2001-02-23 | Ishikawajima Harima Heavy Ind Co Ltd | 筒状部材の継手構造 |
US6397603B1 (en) * | 2000-05-05 | 2002-06-04 | The United States Of America As Represented By The Secretary Of The Air Force | Conbustor having a ceramic matrix composite liner |
JP2002243154A (ja) * | 2001-02-16 | 2002-08-28 | Mitsubishi Heavy Ind Ltd | ガスタービン燃焼器尾筒出口構造及びガスタービン燃焼器 |
-
2001
- 2001-06-29 JP JP2001198916A patent/JP4008212B2/ja not_active Expired - Fee Related
-
2002
- 2002-07-01 CN CNB028023994A patent/CN1220845C/zh not_active Expired - Fee Related
- 2002-07-01 WO PCT/JP2002/006641 patent/WO2003002914A1/ja active Application Filing
- 2002-07-01 CA CA002421802A patent/CA2421802C/en not_active Expired - Fee Related
- 2002-07-01 DE DE60238984T patent/DE60238984D1/de not_active Expired - Lifetime
- 2002-07-01 EP EP02738898A patent/EP1400755B1/de not_active Expired - Lifetime
-
2003
- 2003-03-05 US US10/378,602 patent/US6662568B2/en not_active Expired - Lifetime
-
2004
- 2004-08-16 HK HK04106119.9A patent/HK1063343A1/xx unknown
Also Published As
Publication number | Publication date |
---|---|
EP1400755B1 (de) | 2011-01-19 |
JP4008212B2 (ja) | 2007-11-14 |
US6662568B2 (en) | 2003-12-16 |
WO2003002914A1 (fr) | 2003-01-09 |
EP1400755A1 (de) | 2004-03-24 |
CA2421802A1 (en) | 2003-03-07 |
CA2421802C (en) | 2007-08-21 |
JP2003014237A (ja) | 2003-01-15 |
CN1464960A (zh) | 2003-12-31 |
CN1220845C (zh) | 2005-09-28 |
US20030140633A1 (en) | 2003-07-31 |
EP1400755A4 (de) | 2007-05-09 |
DE60238984D1 (de) | 2011-03-03 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
HK1063343A1 (en) | Flanged hollow structure | |
EP1394038A4 (de) | Luftschiff | |
TW580228U (en) | Carrying structure | |
GB0117667D0 (en) | Support structure | |
GB2376729B (en) | Structural assembly | |
GB2378821B (en) | Daughter-card structural support | |
GB0106567D0 (en) | Mutuagenesis Technique | |
GB0103498D0 (en) | Support structure | |
GB0203683D0 (en) | PAK-GFP Construct | |
TW493677U (en) | Doorstopper structure | |
GB2382477B (en) | Crossing-wire fixing structure | |
TW428699U (en) | Lampstand structure | |
TW574995U (en) | Structure for mini-bicycle | |
TW522798U (en) | Simple lunch-box structure | |
PL112617U1 (en) | Hollow shape | |
GB2382359B (en) | Structural elongate elements | |
TW485770U (en) | Improved umbrella-opening structure | |
TW532415U (en) | Improved door-removal structure | |
GB0129207D0 (en) | Rigidible construction supports | |
EG23586A (en) | Haemagel solution | |
TW481424U (en) | Case structure | |
TW512949U (en) | Rolling-wheel positioning structure | |
GB0114412D0 (en) | Paydispense shoe-replaceable technology/applicatiocs | |
TW585333U (en) | Improved billboard structure | |
GB0120500D0 (en) | Support structure |