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IN2014DN03062A - - Google Patents

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Publication number
IN2014DN03062A
IN2014DN03062A IN3062DEN2014A IN2014DN03062A IN 2014DN03062 A IN2014DN03062 A IN 2014DN03062A IN 3062DEN2014 A IN3062DEN2014 A IN 3062DEN2014A IN 2014DN03062 A IN2014DN03062 A IN 2014DN03062A
Authority
IN
India
Prior art keywords
bearing portion
attachment
hollow part
walls
extending
Prior art date
Application number
Inventor
Marc Andlauer
Pascal Ducrot
Original Assignee
Herakles
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 Herakles filed Critical Herakles
Publication of IN2014DN03062A publication Critical patent/IN2014DN03062A/en

Links

Classifications

    • 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
    • F02K1/04—Mounting of an exhaust cone in the jet pipe
    • 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
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • 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
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • 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
    • F02K1/78—Other construction of jet pipes
    • F02K1/80—Couplings or connections
    • 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
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
    • 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
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
    • 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
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
    • 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
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60—Support structures; Attaching or mounting means
    • 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
    • F05D2260/00—Function
    • F05D2260/30—Retaining components in desired mutual position
    • 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
    • Y10T403/33—Transverse rod to spaced plate surfaces

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Connection Of Plates (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)

Abstract

The invention relates to a attachment device (240) for attaching a hollow part consisting of two opposing walls to at least one structural part. The device includes a one piece body (241) made of a metal material and having two main surfaces (242 243) extending longitudinally between first and second ends (244 245) of said body. Each main surface (242; 243) includes a bearing portion (2420; 2430) in the vicinity of the first end (244) of said body which bearing portion is intended to be pressed against an inner surface of one of the two walls of the hollow part each bearing portion (2420; 2430) comprising an attachment opening (2421) for receiving an attachment member. The bearing portions (2420; 2430) are separated from one another by a slot (246) extending from the first end (244) of said body (241) to a predetermined depth in said body.
IN3062DEN2014 2011-10-24 2012-09-26 IN2014DN03062A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1103242A FR2981700B1 (en) 2011-10-24 2011-10-24 DEVICE FOR FIXING A HOLLOW PIECE
PCT/FR2012/052161 WO2013060956A1 (en) 2011-10-24 2012-09-26 Device for attaching a hollow part

Publications (1)

Publication Number Publication Date
IN2014DN03062A true IN2014DN03062A (en) 2015-05-15

Family

ID=47023026

Family Applications (1)

Application Number Title Priority Date Filing Date
IN3062DEN2014 IN2014DN03062A (en) 2011-10-24 2012-09-26

Country Status (10)

Country Link
US (1) US20140332604A1 (en)
EP (1) EP2771559A1 (en)
JP (1) JP6033875B2 (en)
KR (1) KR20140084119A (en)
CN (1) CN103890366B (en)
CA (1) CA2852996A1 (en)
FR (1) FR2981700B1 (en)
IN (1) IN2014DN03062A (en)
RU (1) RU2014113676A (en)
WO (1) WO2013060956A1 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2988777B1 (en) * 2012-03-29 2014-04-25 Snecma Propulsion Solide INTEGRATION OF REAR BODY PARTS OF AERONAUTICAL MOTOR
WO2013157976A1 (en) * 2012-04-19 2013-10-24 General Electric Company Combustor liner stop
GB2525197A (en) * 2014-04-15 2015-10-21 Rolls Royce Plc A panel attachment system and a method of using the same
US11572793B2 (en) * 2019-07-29 2023-02-07 Pratt & Whitney Canada Corp. Gas turbine engine exhaust case

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1440478A (en) * 1921-11-21 1923-01-02 Philip L Mckee Roof structure
US3269700A (en) * 1964-12-07 1966-08-30 United Aircraft Corp Heat shield for turbine strut
DE3110098C2 (en) * 1981-03-16 1983-03-17 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Turbine guide vane for gas turbine engines
US4594761A (en) * 1984-02-13 1986-06-17 General Electric Company Method of fabricating hollow composite airfoils
FR2586792B1 (en) * 1985-09-03 1989-06-16 Snecma CONNECTION DEVICE BETWEEN A BURNER RING OR FLAME HANGER OF COMPOSITE MATERIAL AND A POST-COMBUSTION CHAMBER CHANNEL OF A TURBOREACTOR
FR2587455B1 (en) * 1985-09-18 1987-10-30 Snecma METHOD FOR MANUFACTURING A BURNER RING IN COMPOSITE MATERIAL AND BURNER RING CARRIED OUT ACCORDING TO SAID METHOD
US4987736A (en) * 1988-12-14 1991-01-29 General Electric Company Lightweight gas turbine engine frame with free-floating heat shield
US5272869A (en) * 1992-12-10 1993-12-28 General Electric Company Turbine frame
US6189285B1 (en) * 1998-10-19 2001-02-20 The Marley Cooling Tower Company Pultruded FRP structural assembly for water cooling towers
FR2865502B1 (en) * 2004-01-23 2006-03-03 Snecma Moteurs MONOBLOC ARM-FLAMES ARM FOR A POST COMBUSTION DEVICE OF A DOUBLE FLOW TURBOREACTOR
FR2875854B1 (en) 2004-09-29 2009-04-24 Snecma Propulsion Solide Sa MIXER FOR TUYERE WITH SEPARATE FLUX
US20080159851A1 (en) * 2006-12-29 2008-07-03 Thomas Ory Moniz Guide Vane and Method of Fabricating the Same
DE102008019156A1 (en) * 2008-04-17 2009-10-22 Mtu Aero Engines Gmbh Strut for a turbine intermediate housing, turbine intermediate housing and method for producing a turbine intermediate housing
US8512808B2 (en) * 2008-04-28 2013-08-20 The Boeing Company Built-up composite structures with a graded coefficient of thermal expansion for extreme environment applications
FR2935464B1 (en) * 2008-09-01 2018-10-26 Safran Aircraft Engines DEVICE FOR FASTENING AN ARM ATTACHED FLAME ON A POST-COMBUSTION HOUSING.
FR2935753B1 (en) * 2008-09-08 2011-07-01 Snecma Propulsion Solide FASTENING, FASTENING CONNECTIONS FOR MOUNTING CMC PIECES

Also Published As

Publication number Publication date
WO2013060956A1 (en) 2013-05-02
JP6033875B2 (en) 2016-11-30
FR2981700A1 (en) 2013-04-26
CA2852996A1 (en) 2013-05-02
RU2014113676A (en) 2015-12-10
CN103890366A (en) 2014-06-25
US20140332604A1 (en) 2014-11-13
KR20140084119A (en) 2014-07-04
EP2771559A1 (en) 2014-09-03
JP2014530991A (en) 2014-11-20
CN103890366B (en) 2017-02-15
FR2981700B1 (en) 2016-08-26

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