FR2994468B1 - Chape en composite de liaison entre deux pieces - Google Patents

Chape en composite de liaison entre deux pieces

Info

Publication number
FR2994468B1
FR2994468B1 FR1257651A FR1257651A FR2994468B1 FR 2994468 B1 FR2994468 B1 FR 2994468B1 FR 1257651 A FR1257651 A FR 1257651A FR 1257651 A FR1257651 A FR 1257651A FR 2994468 B1 FR2994468 B1 FR 2994468B1
Authority
FR
France
Prior art keywords
composite joint
piece composite
piece
joint
composite
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
FR1257651A
Other languages
English (en)
Other versions
FR2994468A1 (fr
Inventor
Boulicaut Loic Le
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.)
Safran Nacelles SAS
Original Assignee
Aircelle SA
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
Priority to FR1257651A priority Critical patent/FR2994468B1/fr
Application filed by Aircelle SA filed Critical Aircelle SA
Priority to EP13756605.5A priority patent/EP2882583A1/fr
Priority to RU2015107170A priority patent/RU2015107170A/ru
Priority to BR112015001981A priority patent/BR112015001981A2/pt
Priority to CA2879679A priority patent/CA2879679A1/fr
Priority to PCT/FR2013/051808 priority patent/WO2014023890A1/fr
Priority to CN201380041552.0A priority patent/CN104520094A/zh
Publication of FR2994468A1 publication Critical patent/FR2994468A1/fr
Priority to US14/609,739 priority patent/US20150197342A1/en
Application granted granted Critical
Publication of FR2994468B1 publication Critical patent/FR2994468B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • 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
    • 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
    • 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
    • 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
    • Y10T403/32—Articulated members
    • Y10T403/32606—Pivoted

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Connection Of Plates (AREA)
FR1257651A 2012-08-07 2012-08-07 Chape en composite de liaison entre deux pieces Active FR2994468B1 (fr)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR1257651A FR2994468B1 (fr) 2012-08-07 2012-08-07 Chape en composite de liaison entre deux pieces
RU2015107170A RU2015107170A (ru) 2012-08-07 2013-07-26 Композитная скоба для обеспечения соединения между двумя деталями
BR112015001981A BR112015001981A2 (pt) 2012-08-07 2013-07-26 conector em u compósito para a conexão entre duas partes, compreendendo um arranjo de camadas de conector em u compósito e um orifício que permite dita conexão e parte equipada com um conector em u
CA2879679A CA2879679A1 (fr) 2012-08-07 2013-07-26 Chape en composite de liaison entre deux pieces
EP13756605.5A EP2882583A1 (fr) 2012-08-07 2013-07-26 Chape en composite de liaison entre deux pièces
PCT/FR2013/051808 WO2014023890A1 (fr) 2012-08-07 2013-07-26 Chape en composite de liaison entre deux pièces
CN201380041552.0A CN104520094A (zh) 2012-08-07 2013-07-26 用于连接两个部件的复合材料连接叉
US14/609,739 US20150197342A1 (en) 2012-08-07 2015-01-30 Composite strap for connection between two parts

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1257651A FR2994468B1 (fr) 2012-08-07 2012-08-07 Chape en composite de liaison entre deux pieces

Publications (2)

Publication Number Publication Date
FR2994468A1 FR2994468A1 (fr) 2014-02-14
FR2994468B1 true FR2994468B1 (fr) 2017-10-13

Family

ID=47088924

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1257651A Active FR2994468B1 (fr) 2012-08-07 2012-08-07 Chape en composite de liaison entre deux pieces

Country Status (8)

Country Link
US (1) US20150197342A1 (fr)
EP (1) EP2882583A1 (fr)
CN (1) CN104520094A (fr)
BR (1) BR112015001981A2 (fr)
CA (1) CA2879679A1 (fr)
FR (1) FR2994468B1 (fr)
RU (1) RU2015107170A (fr)
WO (1) WO2014023890A1 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2988407B1 (fr) * 2012-03-22 2014-10-31 Aircelle Sa Procede de fabrication d'une preforme monobloc pour structure composite
DE102012224340A1 (de) * 2012-12-21 2014-06-26 Putzmeister Engineering Gmbh Mastarm für einen Betonverteilermast und Verfahren zu dessen Herstellung
CN116968339A (zh) * 2016-12-31 2023-10-31 郑州泽正技术服务有限公司 一种纤维织物复合材料结构件及其制备方法
DE102017203477A1 (de) 2017-03-03 2018-09-06 Aktiebolaget Skf Kompositformstück

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3388615A (en) * 1967-04-06 1968-06-18 Bendix Corp Bushings for tie-bars
US3475988A (en) * 1968-02-08 1969-11-04 Bendix Corp End fitting for tie bar
US3484174A (en) * 1968-04-08 1969-12-16 Kaman Corp Rotary wing system
US3923422A (en) * 1974-10-17 1975-12-02 United Technologies Corp Taper lining for composite blade root attachment
GB1526815A (en) * 1974-11-26 1978-10-04 Messerschmitt Boelkow Blohm Stress-reducing connecting assembly
US4300410A (en) * 1980-01-04 1981-11-17 Ford Motor Company Tension-compression member
DE3004575A1 (de) * 1980-02-08 1981-08-13 Sigri Elektrographit Gmbh, 8901 Meitingen Pleuelstange aus verbundwerkstoff
US4555961A (en) * 1982-07-07 1985-12-03 Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschraenkter Haftung Connecting rod made of fiber reinforced synthetic material
US4469730A (en) * 1982-12-30 1984-09-04 The Boeing Company Composite base structure and end fitting joint and method
US4973372A (en) * 1984-08-29 1990-11-27 Allied-Signal Inc. Method of making a tie-bar with internal lubrication
JPS61271167A (ja) * 1985-05-25 1986-12-01 Toyota Motor Corp 繊維強化樹脂製ステアリングホイ−ル芯材及びその製造方法
US4986949A (en) * 1986-05-12 1991-01-22 Trimble Brent J Method of making composite bicycle frames
US4841801A (en) * 1987-03-25 1989-06-27 Trw Inc. Connecting rod
US5279892A (en) * 1992-06-26 1994-01-18 General Electric Company Composite airfoil with woven insert
US5376199A (en) * 1993-08-24 1994-12-27 Brunswick Corporation Method of making a composite filament reinforced clevis
FR2740378B1 (fr) * 1995-10-30 1998-01-02 Eurocopter France Procede de fabrication d'une pale a pas variable en materiau composite pour rotor d'helicoptere, et pale a pas variable pouvant etre obtenue par un tel procede
US6513753B1 (en) * 2001-08-14 2003-02-04 Sikorsky Aircraft Corporation Transmission support structure for a rotary wing aircraft
JP2003200531A (ja) * 2002-01-09 2003-07-15 Tokai Rubber Ind Ltd ゴム・樹脂複合製品及びそれからなる防振装置
JP2008155581A (ja) * 2006-12-26 2008-07-10 Tokai Rubber Ind Ltd 構造部材およびそれを用いた防振装置
DE102007015909A1 (de) * 2007-04-02 2008-10-09 Mt Aerospace Ag Verfahren zur Herstellung faserverstärkter Hohlkörper

Also Published As

Publication number Publication date
FR2994468A1 (fr) 2014-02-14
BR112015001981A2 (pt) 2017-07-04
CN104520094A (zh) 2015-04-15
US20150197342A1 (en) 2015-07-16
RU2015107170A (ru) 2016-09-27
WO2014023890A1 (fr) 2014-02-13
EP2882583A1 (fr) 2015-06-17
CA2879679A1 (fr) 2014-02-13

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