BR112017012551A2 - sistema de reparo de uma ligação que equipa uma parede de reator - Google Patents

sistema de reparo de uma ligação que equipa uma parede de reator

Info

Publication number
BR112017012551A2
BR112017012551A2 BR112017012551-0A BR112017012551A BR112017012551A2 BR 112017012551 A2 BR112017012551 A2 BR 112017012551A2 BR 112017012551 A BR112017012551 A BR 112017012551A BR 112017012551 A2 BR112017012551 A2 BR 112017012551A2
Authority
BR
Brazil
Prior art keywords
wall
bushing
repair system
link repair
system equipping
Prior art date
Application number
BR112017012551-0A
Other languages
English (en)
Other versions
BR112017012551B1 (pt
Inventor
Christophe Maurice Sarazin Yann
Pierre Claude Charbonnier Simon
Jean-Louis Reghezza Patrick
Roset Julien
Original Assignee
Safran Aircraft Engines
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 Safran Aircraft Engines filed Critical Safran Aircraft Engines
Publication of BR112017012551A2 publication Critical patent/BR112017012551A2/pt
Publication of BR112017012551B1 publication Critical patent/BR112017012551B1/pt

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
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B37/00—Nuts or like thread-engaging members
    • F16B37/04—Devices for fastening nuts to surfaces, e.g. sheets, plates
    • F16B37/041—Releasable devices
    • F16B37/042—Releasable devices locking by rotation
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/06—Attaching of nacelles, fairings or cowlings
    • 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
    • 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
    • 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
    • F16B19/00—Bolts without screw-thread; Pins, including deformable elements; Rivets
    • F16B19/02—Bolts or sleeves for positioning of machine parts, e.g. notched taper pins, fitting pins, sleeves, eccentric positioning rings
    • 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
    • F16B33/00—Features common to bolt and nut
    • F16B33/002—Means for preventing rotation of screw-threaded elements
    • 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
    • F16B37/00—Nuts or like thread-engaging members
    • F16B37/04—Devices for fastening nuts to surfaces, e.g. sheets, plates
    • F16B37/044—Nut cages
    • 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
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/06—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of clamps or clips
    • F16B5/0607—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of clamps or clips joining sheets or plates to each other
    • F16B5/0621—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of clamps or clips joining sheets or plates to each other in parallel relationship
    • F16B5/065—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of clamps or clips joining sheets or plates to each other in parallel relationship the plates being one on top of the other and distanced from each other, e.g. by using protrusions to keep contact and distance
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0266—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
    • B64D2033/0273—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for jet engines
    • 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
    • F05D2230/80—Repairing, retrofitting or upgrading methods
    • 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
    • F05D2260/33—Retaining components in desired mutual position with a bayonet coupling
    • 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
    • F05D2260/36—Retaining components in desired mutual position by a form fit connection, e.g. by interlocking
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
  • Snaps, Bayonet Connections, Set Pins, And Snap Rings (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)

Abstract

sistema de fixação destinado a equipar uma parede (17), esse sistema incluindo uma porca destinada a receber um parafuso (31) de orientação normal à parede (17), esse parafuso (31) atravessando um efluente, tal como um painel externo (32) para fixar esse elemento na parede (17). o sistema de fixação compreende uma bucha (26) que tem uma face externa cilíndrica filetada (34) destinada a ser parafusada no orifício (29) que atravessa a parede (17) e tendo dimensões superiores às dimensões da ligação que essa bucha de reparo (26) substitui, essa bucha (26) portando em sua região central uma porca (28) que recebe o parafuso de fixação (32).
BR112017012551-0A 2014-12-15 2015-12-14 Sistema de fixação destinado a ser instalado em uma parede de turbomáquina, motor de aeronave de tipo turborreator e processo de reparo de uma ligação instalada em uma parede de turbomáquina BR112017012551B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1462434A FR3029980B1 (fr) 2014-12-15 2014-12-15 Systeme de reparation d'une attache equipant une paroi de reacteur
FR1462434 2014-12-15
PCT/FR2015/053463 WO2016097552A1 (fr) 2014-12-15 2015-12-14 Systeme de reparation d'une attache equipant une paroi de reacteur

Publications (2)

Publication Number Publication Date
BR112017012551A2 true BR112017012551A2 (pt) 2018-01-02
BR112017012551B1 BR112017012551B1 (pt) 2022-12-27

Family

ID=52477940

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112017012551-0A BR112017012551B1 (pt) 2014-12-15 2015-12-14 Sistema de fixação destinado a ser instalado em uma parede de turbomáquina, motor de aeronave de tipo turborreator e processo de reparo de uma ligação instalada em uma parede de turbomáquina

Country Status (9)

Country Link
US (1) US10253800B2 (pt)
EP (1) EP3234311B1 (pt)
JP (1) JP6717848B2 (pt)
CN (1) CN107002508B (pt)
BR (1) BR112017012551B1 (pt)
CA (1) CA2970251C (pt)
FR (1) FR3029980B1 (pt)
RU (1) RU2717187C2 (pt)
WO (1) WO2016097552A1 (pt)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102015122744A1 (de) * 2015-12-23 2017-06-29 Böllhoff Verbindungstechnik GmbH Verstellbare Distanzhülse
US10695984B2 (en) * 2017-10-25 2020-06-30 Ford Global Technologies, Llc Housing for a fastener of a vehicle component
USD976754S1 (en) * 2018-03-12 2023-01-31 Transportation Ip Holdings, Llc Rail vehicle traction pin
FR3085435B1 (fr) * 2018-09-05 2021-06-18 Safran Aircraft Engines Turbomachine a double flux
CN108980184B (zh) * 2018-09-10 2024-01-23 一汽-大众汽车有限公司 一种固定装置及汽车
FR3084731B1 (fr) * 2019-02-19 2020-07-03 Safran Aircraft Engines Chambre de combustion pour une turbomachine
FR3093537B1 (fr) 2019-03-08 2021-06-11 Safran Aircraft Engines Sous ensemble de montage d'un palier de guidage d'un arbre de compresseur
JP6854866B1 (ja) * 2019-11-20 2021-04-07 三菱電機株式会社 電力変換装置
USD1008795S1 (en) * 2021-04-26 2023-12-26 Mark David Rowley Threaded insert with a replaceable nut element
US11933341B2 (en) * 2021-04-26 2024-03-19 Mark David Rowley Threaded insert with a replaceable nut element
CN114083476A (zh) * 2021-11-12 2022-02-25 中国航发贵州黎阳航空动力有限公司 一种用于航空发动机低压涡轮转子装配的工装
TWI806242B (zh) * 2021-11-16 2023-06-21 恒昌行精密工業有限公司 浮動式定位裝置及應用該浮動式定位裝置之散熱模組
CN114179582A (zh) * 2021-11-22 2022-03-15 梁山众兴机械制造有限公司 空气悬架提升结构及组装方法

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US4981735A (en) * 1989-09-05 1991-01-01 The United States Of America As Represented By The Secretary Of The Army Two piece threaded mounting insert with adhesive for use with honeycomb composite
US5037259A (en) * 1989-10-25 1991-08-06 Avibank Mfg., Inc. Nut with sleeve lock
JPH0480917U (pt) * 1990-11-27 1992-07-14
US5468104A (en) * 1994-08-10 1995-11-21 Fatigue Technology, Inc. Wall nut assembly
JP3237429B2 (ja) * 1995-01-13 2001-12-10 三菱自動車工業株式会社 装着部材の取付け構造
DE20021221U1 (de) * 2000-12-15 2001-03-22 Ejot Verbindungstech Gmbh & Co Befestigungsvorrichtung für an einer Platte zu befestigendes Bauteil
RU2217629C1 (ru) * 2002-04-17 2003-11-27 Открытое акционерное общество "ОКБ Сухого" Крепежное устройство
US7591622B2 (en) * 2005-07-22 2009-09-22 The Boeing Company Nutmount apparatus
US20070297869A1 (en) * 2006-06-26 2007-12-27 Kunda James J Through insert with floating capability
US7588386B2 (en) * 2006-08-30 2009-09-15 Silicon Valley Automation Leveling and aligning device
FR2915217B1 (fr) * 2007-04-20 2009-07-10 Imphy Alloys Sa Structure pour le montage dans une paroi d'un batiment de batis destines a supporter des panneaux tels que des panneaux photovoltaiques
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Also Published As

Publication number Publication date
WO2016097552A1 (fr) 2016-06-23
FR3029980A1 (fr) 2016-06-17
EP3234311B1 (fr) 2021-01-27
BR112017012551B1 (pt) 2022-12-27
RU2017124939A3 (pt) 2019-07-17
CA2970251A1 (fr) 2016-06-23
RU2717187C2 (ru) 2020-03-18
FR3029980B1 (fr) 2017-01-13
US10253800B2 (en) 2019-04-09
US20170343033A1 (en) 2017-11-30
EP3234311A1 (fr) 2017-10-25
RU2017124939A (ru) 2019-01-17
CN107002508A (zh) 2017-08-01
JP6717848B2 (ja) 2020-07-08
CN107002508B (zh) 2019-06-14
CA2970251C (fr) 2022-05-03
JP2018505365A (ja) 2018-02-22

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Legal Events

Date Code Title Description
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 14/12/2015, OBSERVADAS AS CONDICOES LEGAIS