PL416036A1 - Zespół złącza kołnierzowego do użycia w silniku turbospalinowym - Google Patents

Zespół złącza kołnierzowego do użycia w silniku turbospalinowym

Info

Publication number
PL416036A1
PL416036A1 PL416036A PL41603616A PL416036A1 PL 416036 A1 PL416036 A1 PL 416036A1 PL 416036 A PL416036 A PL 416036A PL 41603616 A PL41603616 A PL 41603616A PL 416036 A1 PL416036 A1 PL 416036A1
Authority
PL
Poland
Prior art keywords
flange
connection unit
turbocharged engine
flanged connection
radially outer
Prior art date
Application number
PL416036A
Other languages
English (en)
Inventor
Antoni Tyburcy
Andrzej Kakolewski
Kamil Rajter
Original Assignee
General Electric Company
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 General Electric Company filed Critical General Electric Company
Priority to PL416036A priority Critical patent/PL416036A1/pl
Priority to CA2956353A priority patent/CA2956353A1/en
Priority to GB1701629.6A priority patent/GB2547108A/en
Priority to US15/423,633 priority patent/US10718450B2/en
Publication of PL416036A1 publication Critical patent/PL416036A1/pl

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
    • F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L23/00—Flanged joints
    • F16L23/003—Auxiliary devices
    • 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
    • F01D25/08—Cooling; Heating; Heat-insulation
    • F01D25/12—Cooling
    • 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
    • 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
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
    • 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
    • F16L23/02—Flanged joints the flanges being connected by members tensioned axially
    • 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
    • F16L23/02—Flanged joints the flanges being connected by members tensioned axially
    • F16L23/036—Flanged joints the flanges being connected by members tensioned axially characterised by the tensioning members, e.g. specially adapted bolts or C-clamps
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • F05D2230/642—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins using maintaining alignment while permitting differential dilatation
    • 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
    • F05D2260/00—Function
    • F05D2260/30—Retaining components in desired mutual position
    • F05D2260/31—Retaining bolts or nuts
    • 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
    • F05D2260/30—Retaining components in desired mutual position
    • F05D2260/37—Retaining components in desired mutual position by a press fit connection
    • 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
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • F05D2300/6033—Ceramic matrix composites [CMC]
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Connection Of Plates (AREA)

Abstract

Zespół (100) złącza kołnierzowego obejmuje pierwszą konstrukcję posiadającą pierwszy kołnierz (46) oraz drugą konstrukcję posiadającą drugi kołnierz (42) połączony z pierwszym kołnierzem (46), aby utworzyć pomiędzy nimi złącze. Drugi kołnierz (42) posiada promieniowo zewnętrzną powierzchnię (112). Zespół (100) złącza kołnierzowego zawiera również pierścień ściskający (102) połączony przynajmniej z promieniowo zewnętrzną powierzchnią (112) i skonfigurowany tak, aby przykładać siłę ściskającą (114) do promieniowo zewnętrznej powierzchni (112) w celu obniżenia wielkości naprężeń rozciągających we wspomnianym drugim kołnierzu (42).
PL416036A 2016-02-04 2016-02-04 Zespół złącza kołnierzowego do użycia w silniku turbospalinowym PL416036A1 (pl)

Priority Applications (4)

Application Number Priority Date Filing Date Title
PL416036A PL416036A1 (pl) 2016-02-04 2016-02-04 Zespół złącza kołnierzowego do użycia w silniku turbospalinowym
CA2956353A CA2956353A1 (en) 2016-02-04 2017-01-26 A flange joint assembly for use in a gas turbine engine
GB1701629.6A GB2547108A (en) 2016-02-04 2017-02-01 A flange joint assembly for use in a gas turbine engine
US15/423,633 US10718450B2 (en) 2016-02-04 2017-02-03 Flange joint assembly for use in a gas turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL416036A PL416036A1 (pl) 2016-02-04 2016-02-04 Zespół złącza kołnierzowego do użycia w silniku turbospalinowym

Publications (1)

Publication Number Publication Date
PL416036A1 true PL416036A1 (pl) 2017-08-16

Family

ID=58462797

Family Applications (1)

Application Number Title Priority Date Filing Date
PL416036A PL416036A1 (pl) 2016-02-04 2016-02-04 Zespół złącza kołnierzowego do użycia w silniku turbospalinowym

Country Status (4)

Country Link
US (1) US10718450B2 (pl)
CA (1) CA2956353A1 (pl)
GB (1) GB2547108A (pl)
PL (1) PL416036A1 (pl)

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US10287990B2 (en) 2014-08-08 2019-05-14 Rohr, Inc. Bleed system bolted duct with recessed seals
JP6752219B2 (ja) * 2015-04-24 2020-09-09 ヌオーヴォ・ピニォーネ・テクノロジー・ソチエタ・レスポンサビリタ・リミタータＮｕｏｖｏ Ｐｉｇｎｏｎｅ Ｔｅｃｎｏｌｏｇｉｅ Ｓ．Ｒ．Ｌ． 冷却フィンを備えたケーシングを有するガスタービンエンジン
US10774685B2 (en) * 2018-04-30 2020-09-15 Ratheon Technologies Corporation Gas turbine engine exhaust component
JP7412529B2 (ja) * 2020-02-20 2024-01-12 川崎重工業株式会社 ガスタービンエンジンのフランジ冷却構造
US11542836B2 (en) 2021-06-03 2023-01-03 Pratt & Whitney Canada Corp. Bi-material joint for engine
US11732609B2 (en) * 2021-10-29 2023-08-22 Pratt & Whitney Canada Corp. Connecting arrangement between components of an aircraft engine
US12558747B2 (en) 2023-09-25 2026-02-24 Pratt & Whitney Canada Corp. Method of assembling parts with different coefficients of thermal expansion

Family Cites Families (18)

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Publication number Priority date Publication date Assignee Title
US2877623A (en) * 1956-11-27 1959-03-17 Klompas Nicholas Annular fairing structure for the rear frame housing of a gas turbine engine
JPS58119927A (ja) * 1982-01-12 1983-07-16 Mitsubishi Heavy Ind Ltd 固定式フランジ継手とその製造方法
FR2574473B1 (fr) 1984-11-22 1987-03-20 Snecma Anneau de turbine pour une turbomachine a gaz
US4951973A (en) 1988-03-17 1990-08-28 General Electric Company Joint connection for annular flanges
US5412939A (en) 1993-12-20 1995-05-09 Alliedsignal Inc. Seal compression tool for gas turbine engine
US5437482A (en) * 1994-04-07 1995-08-01 Curtis; Donald K. Pipe adapter flange
US5503490A (en) * 1994-05-13 1996-04-02 United Technologies Corporation Thermal load relief ring for engine case
US5470114A (en) * 1994-11-14 1995-11-28 General Electric Company Coupling assembly
PL181068B1 (pl) 1996-12-31 2001-05-31 Demut Stanislaw Izolacyjne złącze rurociągów
US6435820B1 (en) * 1999-08-25 2002-08-20 General Electric Company Shroud assembly having C-clip retainer
US6368054B1 (en) 1999-12-14 2002-04-09 Pratt & Whitney Canada Corp. Split ring for tip clearance control
US20050200129A1 (en) * 2004-03-15 2005-09-15 Bongiorno Louis C. Aseptic flanged joint
US7665962B1 (en) 2007-01-26 2010-02-23 Florida Turbine Technologies, Inc. Segmented ring for an industrial gas turbine
EP2107217A1 (en) 2008-03-31 2009-10-07 Siemens Aktiengesellschaft Unison ring assembly for an axial compressor casing
US8794910B2 (en) 2011-02-01 2014-08-05 United Technologies Corporation Gas turbine engine synchronizing ring bumper
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CN102563064B (zh) 2011-12-31 2015-05-20 中国船舶重工集团公司第七○二研究所 深海耐压圆口法兰对接锁死解脱装置
US9599270B2 (en) * 2012-02-06 2017-03-21 Sciteq A/S End closure device

Also Published As

Publication number Publication date
US10718450B2 (en) 2020-07-21
US20170227152A1 (en) 2017-08-10
GB2547108A (en) 2017-08-09
CA2956353A1 (en) 2017-08-04
GB201701629D0 (en) 2017-03-15

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