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MX2019004853A - Componente de brida para motor de turbina de gas. - Google Patents

Componente de brida para motor de turbina de gas.

Info

Publication number
MX2019004853A
MX2019004853A MX2019004853A MX2019004853A MX2019004853A MX 2019004853 A MX2019004853 A MX 2019004853A MX 2019004853 A MX2019004853 A MX 2019004853A MX 2019004853 A MX2019004853 A MX 2019004853A MX 2019004853 A MX2019004853 A MX 2019004853A
Authority
MX
Mexico
Prior art keywords
flange
gas turbine
turbine engine
threaded
flange component
Prior art date
Application number
MX2019004853A
Other languages
English (en)
Other versions
MX395173B (es
Inventor
E Struck Bruno
Original Assignee
Solar Turbines Inc
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Solar Turbines Inc filed Critical Solar Turbines Inc
Publication of MX2019004853A publication Critical patent/MX2019004853A/es
Publication of MX395173B publication Critical patent/MX395173B/es

Links

Classifications

    • 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
    • F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D1/00—Couplings for rigidly connecting two coaxial shafts or other movable machine elements
    • F16D1/06—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end
    • F16D1/076—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end by clamping together two faces perpendicular to the axis of rotation, e.g. with bolted flanges
    • 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
    • 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
    • F01D11/003—Preventing or minimising internal leakage of working-fluid, e.g. between stages by packing rings; Mechanical 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
    • F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
    • 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
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/243—Flange connections; Bolting arrangements
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/025—Fixing blade carrying members on shafts
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
    • F01D5/066—Connecting means for joining rotor-discs or rotor-elements together, e.g. by a central bolt, by clamps
    • 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
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • 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
    • 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
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/23—Three-dimensional prismatic
    • F05D2250/232—Three-dimensional prismatic conical

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Gasket Seals (AREA)

Abstract

En la presente descripción se describe un componente de brida (70) para un motor de turbina de gas (100). El componente de brida (70) incluye un cuerpo de la brida (79) con una superficie de acoplamiento de la brida (71) y una pluralidad de elementos roscados. Cada elemento roscado (72) incluye una porción roscada (73) y una porción de liberación (74). La porción roscada (73) tiene roscas (84) y se extiende hacia dentro del cuerpo de la brida (79) desde la superficie de acoplamiento de la brida (71). La porción de liberación (74) se extiende hacia dentro del cuerpo de la brida (79) desde la superficie de acoplamiento de la brida (71) localizada hacia fuera de la porción roscada (73) que forma una porción de reborde (78) entre las mismas. La porción de reborde (78) incluye una superficie superior del reborde (63) que tiene una forma anular. La porción de liberación (74) incluye una superficie interna (75) que se extiende desde el borde y se estrecha hacia afuera desde la superficie superior del reborde (63).
MX2019004853A 2016-11-04 2017-10-31 Componente de brida para motor de turbina de gas. MX395173B (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US15/344,129 US10190641B2 (en) 2016-11-04 2016-11-04 Flanged component for a gas turbine engine
PCT/US2017/059176 WO2018085219A1 (en) 2016-11-04 2017-10-31 Flanged component for a gas turbine engine

Publications (2)

Publication Number Publication Date
MX2019004853A true MX2019004853A (es) 2019-08-05
MX395173B MX395173B (es) 2025-03-25

Family

ID=62065470

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2019004853A MX395173B (es) 2016-11-04 2017-10-31 Componente de brida para motor de turbina de gas.

Country Status (5)

Country Link
US (1) US10190641B2 (es)
CN (1) CN109937287A (es)
MX (1) MX395173B (es)
RU (1) RU2742013C2 (es)
WO (1) WO2018085219A1 (es)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NO20210178A1 (en) * 2018-08-30 2021-02-11 Dril Quip Inc Methods for decreasing stress in flange bolting
FR3115320B1 (fr) * 2020-10-19 2023-05-19 Safran Aircraft Engines Module de turbomachine comportant des plaques de verrouillage de paires de goujons
GB202210143D0 (en) * 2022-07-11 2022-08-24 Rolls Royce Plc Combustor casing component for a gas turbine engine

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3491630A (en) 1968-07-08 1970-01-27 Lloyd L Mielke Bolt,nut and washer combination
US4339217A (en) 1980-07-07 1982-07-13 Drillco Devices Limited Expanding anchor bolt assembly
RU2057949C1 (ru) * 1992-08-06 1996-04-10 Акционерное общество открытого типа "Авиадвигатель" Соединение деталей турбомашины
US6176663B1 (en) 1998-12-18 2001-01-23 Cooper Cameron Corporation Apparatus for reducing fastener bending stress in flanged connections
GB0321056D0 (en) 2003-09-09 2003-10-08 Rolls Royce Plc Joint arrangement
US7213999B2 (en) * 2004-01-30 2007-05-08 Torque-Traction Technologies, Llc. Fastener with opposite hand threads for securing two components together
US20090101328A1 (en) 2004-09-28 2009-04-23 Advanced Composite Products & Technology, Inc. Composite drill pipe and method of forming same
US8079773B2 (en) 2005-10-18 2011-12-20 General Electric Company Methods and apparatus for assembling composite structures
DE202006008721U1 (de) * 2006-06-01 2007-10-11 Profil Verbindungstechnik Gmbh & Co. Kg Nietmutter und Kombination einer Nietmutter mit einem Blechteil
FR2907497B1 (fr) * 2006-10-24 2009-01-23 Snecma Sa Systeme d'equilibrage pour rotor de turbomachine
US8033579B2 (en) 2007-10-05 2011-10-11 Ckd Corporation Fluid device connecting structure
CN201309014Y (zh) 2008-12-17 2009-09-16 桂林创源金刚石有限公司 具有夹持结构的孔类快速装卸与定心零件
CN202231518U (zh) * 2011-10-27 2012-05-23 山东齐鲁电机制造有限公司 新型汽轮发电机导风轮固定装置
US9169728B2 (en) 2011-12-08 2015-10-27 General Electric Company Dynamic load reduction system
US20140014792A1 (en) 2012-07-13 2014-01-16 General Electric Company Fastener assembly for a gas turbine
EP2733314B1 (fr) * 2012-11-15 2017-04-05 Safran Aero Boosters SA Brides radiales de fixation et de positionnement pour viroles de carter de turbomachine axiale
US20140260321A1 (en) 2013-03-15 2014-09-18 United Technologies Corporation Gas turbine engine static structure joint with undercuts
US9708912B2 (en) * 2014-10-30 2017-07-18 Siemens Energy, Inc. Turbine rotor nut and bolt arrangement with improved fatigue resistance under centrifugal load
CN205663463U (zh) * 2016-06-14 2016-10-26 中国船舶重工集团公司第七�三研究所 一种高背压汽轮机预冷却可倾瓦轴承结构

Also Published As

Publication number Publication date
MX395173B (es) 2025-03-25
RU2019114791A (ru) 2020-11-16
CN109937287A (zh) 2019-06-25
RU2742013C2 (ru) 2021-02-01
WO2018085219A1 (en) 2018-05-11
RU2019114791A3 (es) 2021-01-12
US10190641B2 (en) 2019-01-29
US20180128321A1 (en) 2018-05-10

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