JP5317581B2 - 熱継手 - Google Patents

熱継手 Download PDF

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Publication number
JP5317581B2
JP5317581B2 JP2008213978A JP2008213978A JP5317581B2 JP 5317581 B2 JP5317581 B2 JP 5317581B2 JP 2008213978 A JP2008213978 A JP 2008213978A JP 2008213978 A JP2008213978 A JP 2008213978A JP 5317581 B2 JP5317581 B2 JP 5317581B2
Authority
JP
Japan
Prior art keywords
frame
thermal
thermal expansion
flange
fastener
Prior art date
Legal status (The legal status 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 status listed.)
Active
Application number
JP2008213978A
Other languages
English (en)
Japanese (ja)
Other versions
JP2009063166A5 (enExample
JP2009063166A (ja
Inventor
ウィリアム・ピィ・キース
マイケル・エル・ハンド
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boeing Co
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Publication of JP2009063166A publication Critical patent/JP2009063166A/ja
Publication of JP2009063166A5 publication Critical patent/JP2009063166A5/ja
Application granted granted Critical
Publication of JP5317581B2 publication Critical patent/JP5317581B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F01D25/24—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
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00—Components
    • F05B2240/90—Mounting on supporting structures or systems
    • F05B2240/92—Mounting on supporting structures or systems on an airbourne structure
    • 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
    • F05D2250/00—Geometry
    • F05D2250/10—Two-dimensional
    • F05D2250/18—Two-dimensional patterned
    • 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
    • F16B2200/506—Flanged connections bolted or riveted
    • 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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00—Joints and connections
    • Y10T403/21—Utilizing thermal characteristic, e.g., expansion or contraction, etc.
    • Y10T403/217—Members having different coefficients of expansion

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Connection Of Plates (AREA)
  • Flanged Joints, Insulating Joints, And Other Joints (AREA)
  • Joints Allowing Movement (AREA)
  • Clamps And Clips (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)
JP2008213978A 2007-09-07 2008-08-22 熱継手 Active JP5317581B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/851,622 2007-09-07
US11/851,622 US20090067917A1 (en) 2007-09-07 2007-09-07 Bipod Flexure Ring

Publications (3)

Publication Number Publication Date
JP2009063166A JP2009063166A (ja) 2009-03-26
JP2009063166A5 JP2009063166A5 (enExample) 2011-10-06
JP5317581B2 true JP5317581B2 (ja) 2013-10-16

Family

ID=40111025

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2008213978A Active JP5317581B2 (ja) 2007-09-07 2008-08-22 熱継手

Country Status (4)

Country Link
US (3) US20090067917A1 (enExample)
EP (1) EP2034135B1 (enExample)
JP (1) JP5317581B2 (enExample)
CA (1) CA2638187C (enExample)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8726675B2 (en) * 2007-09-07 2014-05-20 The Boeing Company Scalloped flexure ring
US20090067917A1 (en) 2007-09-07 2009-03-12 The Boeing Company Bipod Flexure Ring
US8292537B2 (en) * 2009-06-16 2012-10-23 Utah State University Research Foundation Thermal expansion compensation method and system
DE102009058504B4 (de) * 2009-12-16 2023-07-13 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Schwellerverkleidung
US9290261B2 (en) 2011-06-09 2016-03-22 United Technologies Corporation Method and assembly for attaching components
US10059431B2 (en) 2011-06-09 2018-08-28 United Technologies Corporation Method and apparatus for attaching components having dissimilar rates of thermal expansion
US9417422B2 (en) * 2011-08-23 2016-08-16 Bae Systems Information And Electronic Systems Integration Inc. Rigid adaptor ring for CTE mismatched optical device components
CA2870754C (en) 2012-04-27 2017-09-05 General Electric Company Connecting gas turbine engine annular members
GB201302125D0 (en) * 2013-02-07 2013-03-20 Rolls Royce Plc A panel mounting arrangement
US9764849B2 (en) 2014-09-18 2017-09-19 The Boeing Company Method of attaching nacelle structure to minimize fatigue loading
US10801729B2 (en) 2015-07-06 2020-10-13 General Electric Company Thermally coupled CMC combustor liner
US9856011B2 (en) * 2015-08-06 2018-01-02 The Boeing Company Method for the joining of wings or control surfaces to an airplane fuselage
US11149646B2 (en) 2015-09-02 2021-10-19 General Electric Company Piston ring assembly for a turbine engine
US9976746B2 (en) 2015-09-02 2018-05-22 General Electric Company Combustor assembly for a turbine engine
US10168051B2 (en) 2015-09-02 2019-01-01 General Electric Company Combustor assembly for a turbine engine
US10197278B2 (en) 2015-09-02 2019-02-05 General Electric Company Combustor assembly for a turbine engine
US10837640B2 (en) 2017-03-06 2020-11-17 General Electric Company Combustion section of a gas turbine engine
US11402097B2 (en) 2018-01-03 2022-08-02 General Electric Company Combustor assembly for a turbine engine
FR3084916B1 (fr) * 2018-08-10 2020-07-17 Safran Ceramics Cone d'ejection a fixation flexible
US11767770B2 (en) 2021-08-10 2023-09-26 The Boeing Company Double bipod fitting to mitigate thermal loading of engine exhaust structures
US11901619B2 (en) 2021-12-16 2024-02-13 The Boeing Company Radome with ceramic matrix composite

Family Cites Families (55)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB612532A (en) * 1946-04-08 1948-11-15 Adrian Albert Lombard Improvements in or relating to combustion chambers for internal combustion turbines
US3962843A (en) * 1970-04-30 1976-06-15 King John O Jun Resilient sleeve joint construction
US3826708A (en) * 1970-05-18 1974-07-30 Mc Donnell Douglas Corp Rocket nozzle liner construction
US3701704A (en) * 1970-05-18 1972-10-31 Mc Donnell Douglas Corp Method of fabricating a rocket nozzle liner
US4004887A (en) * 1973-03-16 1977-01-25 Tenneco Inc. Catalytic converter having a resilient thermal-variation compensating monolith-mounting arrangement
DE2453688A1 (de) * 1974-11-13 1976-05-20 Helmut Hartz Elastische kupplung
JPS5418561Y2 (enExample) * 1975-07-08 1979-07-12
US4076451A (en) * 1976-03-05 1978-02-28 United Technologies Corporation Ceramic turbine stator
US4227370A (en) * 1977-11-04 1980-10-14 Rolls-Royce Limited By-pass gas turbine engines
JPS54114823A (en) * 1978-02-27 1979-09-07 Jiyunichi Katayama Balance type expansion pipe joint
GB2112095B (en) * 1981-12-22 1985-02-06 Rolls Royce Joining components having different thermal expansion coefficients
US4552386A (en) * 1983-08-22 1985-11-12 United Technologies Corporation Joints between cylinders of different materials
US4910620A (en) * 1987-05-14 1990-03-20 Siemens Aktiengesellschaft Thermal compensation structure for a disk pack module
FR2623249A1 (fr) * 1987-11-12 1989-05-19 Snecma Ensemble constitue de deux pieces en materiaux ayant des coefficients de dilatation differents, reliees entre elles et methode d'assemblage
FR2640350B1 (fr) * 1988-12-14 1991-05-03 Europ Propulsion Dispositif de liaison demontable entre deux pieces soumises a de fortes sollicitations
US5013174A (en) * 1989-12-04 1991-05-07 Motorola, Inc. Dual function fastener
US5147151A (en) * 1991-08-23 1992-09-15 Hipkins Jr Edward C Washer insert for bearing plate
US5141393A (en) * 1991-09-03 1992-08-25 United Technologies Corporation Seal accommodating thermal expansion between adjacent casings in gas turbine engine
US5230539A (en) * 1991-12-31 1993-07-27 Dana Corporation Quick connect tube coupling
FR2699970B1 (fr) * 1992-12-30 1995-03-17 Europ Propulsion Dispositif de liaison glissante entre deux pièces soumises à de fortes sollicitations mécaniques et thermiques.
JP2710914B2 (ja) * 1993-06-18 1998-02-10 浜松ホトニクス株式会社 Ｘ線発生管
US5645363A (en) * 1994-04-15 1997-07-08 Dana Corporation Bearing cap and pump mounting flange for power take-off unit
US5503490A (en) * 1994-05-13 1996-04-02 United Technologies Corporation Thermal load relief ring for engine case
GB9510465D0 (en) * 1995-05-24 1995-07-19 Petroline Wireline Services Connector assembly
US6106184A (en) * 1997-11-12 2000-08-22 Frazier Industrial Company Bolt connector with integral burr
US6173996B1 (en) * 1997-11-25 2001-01-16 General Electric Company Compliant joint with a coupling member for interfacing dissimilar metals in X-ray tubes
US6212753B1 (en) * 1997-11-25 2001-04-10 General Electric Company Complaint joint for interfacing dissimilar metals in X-ray tubes
GB2339244B (en) * 1998-06-19 2002-12-18 Rolls Royce Plc A variable camber vane
US6158961A (en) * 1998-10-13 2000-12-12 General Electric Compnay Truncated chamfer turbine blade
US6607328B1 (en) * 1999-04-02 2003-08-19 Mark R. Treiber Fastener assembly for pivotal engagement of adjacent components
EP1604024A4 (en) * 2000-04-06 2008-04-23 Wayne P Franco METHODS OF USING GROWTH FACTORS FOR TREATING CARDIOPATHY
JP3600911B2 (ja) * 2001-01-25 2004-12-15 川崎重工業株式会社 環状燃焼器のライナ支持構造
US6540899B2 (en) * 2001-04-05 2003-04-01 All Wet Technologies, Inc. Method of and apparatus for fluid sealing, while electrically contacting, wet-processed workpieces
FR2825783B1 (fr) * 2001-06-06 2003-11-07 Snecma Moteurs Accrochage de chambre de combustion cmc de turbomachine par pattes brasees
FR2825781B1 (fr) * 2001-06-06 2004-02-06 Snecma Moteurs Montage elastique de chambre ce combustion cmc de turbomachine dans un carter metallique
FR2825784B1 (fr) * 2001-06-06 2003-08-29 Snecma Moteurs Accrochage de chambre de combustion cmc de turbomachine utilisant les trous de dilution
JP3600912B2 (ja) * 2001-09-12 2004-12-15 川崎重工業株式会社 燃焼器ライナのシール構造
AUPR880901A0 (en) * 2001-11-12 2001-12-06 Nique Enterprises Pty Ltd Furniture joint
FR2840974B1 (fr) * 2002-06-13 2005-12-30 Snecma Propulsion Solide Anneau d'etancheite pour cahmbre de combustion et chambre de combustion comportant un tel anneau
US6904757B2 (en) * 2002-12-20 2005-06-14 General Electric Company Mounting assembly for the forward end of a ceramic matrix composite liner in a gas turbine engine combustor
US6775985B2 (en) * 2003-01-14 2004-08-17 General Electric Company Support assembly for a gas turbine engine combustor
FR2855249B1 (fr) * 2003-05-20 2005-07-08 Snecma Moteurs Chambre de combustion ayant une liaison souple entre un fond de chambre et une paroi de chambre
FR2857409B1 (fr) * 2003-07-11 2006-07-28 Snecma Moteurs Dispositif pour piloter passivement la dilatation thermique du carter d'extension d'un turboreacteur
FR2871846B1 (fr) * 2004-06-17 2006-09-29 Snecma Moteurs Sa Chambre de combustion en cmc de turbine a gaz supportee dans un carter metallique par des organes de liaison en cmc
FR2871845B1 (fr) 2004-06-17 2009-06-26 Snecma Moteurs Sa Montage de chambre de combustion de turbine a gaz avec distributeur integre de turbine haute pression
FR2871847B1 (fr) * 2004-06-17 2006-09-29 Snecma Moteurs Sa Montage d'un distributeur de turbine sur une chambre de combustion a parois en cmc dans une turbine a gaz
FR2871844B1 (fr) * 2004-06-17 2006-09-29 Snecma Moteurs Sa Montage etanche d'un distributeur de turbine haute pression sur une extremite d'une chambre de combustion dans une turbine a gaz
FR2875854B1 (fr) * 2004-09-29 2009-04-24 Snecma Propulsion Solide Sa Melangeur pour tuyere a flux separes
US7546743B2 (en) 2005-10-12 2009-06-16 General Electric Company Bolting configuration for joining ceramic combustor liner to metal mounting attachments
US8141370B2 (en) 2006-08-08 2012-03-27 General Electric Company Methods and apparatus for radially compliant component mounting
FR2916018B1 (fr) * 2007-05-10 2009-08-21 Snecma Propulsion Solide Sa Systeme d'echappement pour turbine a gaz
US8726675B2 (en) * 2007-09-07 2014-05-20 The Boeing Company Scalloped flexure ring
US20090067917A1 (en) * 2007-09-07 2009-03-12 The Boeing Company Bipod Flexure Ring
US8459941B2 (en) * 2009-06-15 2013-06-11 General Electric Company Mechanical joint for a gas turbine engine
US9284969B2 (en) * 2012-02-24 2016-03-15 Pratt & Whitney Canada Corp. Thermal expansion joint connection for sheet metal assembly

Also Published As

Publication number Publication date
US20130034378A1 (en) 2013-02-07
EP2034135B1 (en) 2014-08-13
CA2638187A1 (en) 2009-03-07
US8328453B2 (en) 2012-12-11
JP2009063166A (ja) 2009-03-26
CA2638187C (en) 2011-10-11
US20100227698A1 (en) 2010-09-09
US20090067917A1 (en) 2009-03-12
EP2034135A2 (en) 2009-03-11
US8834056B2 (en) 2014-09-16
EP2034135A3 (en) 2012-04-18

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