FR2891804B1 - Systeme d'ecrou et mat d'accrochage de moteur d'aeronef comprenant un tel systeme - Google Patents

Systeme d'ecrou et mat d'accrochage de moteur d'aeronef comprenant un tel systeme

Info

Publication number
FR2891804B1
FR2891804B1 FR0553102A FR0553102A FR2891804B1 FR 2891804 B1 FR2891804 B1 FR 2891804B1 FR 0553102 A FR0553102 A FR 0553102A FR 0553102 A FR0553102 A FR 0553102A FR 2891804 B1 FR2891804 B1 FR 2891804B1
Authority
FR
France
Prior art keywords
aircraft engine
narrow
hitting material
hitting
narrow system
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.)
Expired - Fee Related
Application number
FR0553102A
Other languages
English (en)
Other versions
FR2891804A1 (fr
Inventor
Stephane Levert
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.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
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 FR0553102A priority Critical patent/FR2891804B1/fr
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to US12/089,312 priority patent/US8042764B2/en
Priority to RU2008118224/11A priority patent/RU2428356C2/ru
Priority to BRPI0616930-9A priority patent/BRPI0616930A2/pt
Priority to EP06807103A priority patent/EP1934093A1/fr
Priority to PCT/EP2006/067217 priority patent/WO2007042508A1/fr
Priority to CN2006800378146A priority patent/CN101282877B/zh
Priority to CA2624476A priority patent/CA2624476C/fr
Priority to JP2008535011A priority patent/JP2009511336A/ja
Publication of FR2891804A1 publication Critical patent/FR2891804A1/fr
Application granted granted Critical
Publication of FR2891804B1 publication Critical patent/FR2891804B1/fr
Expired - Fee Related 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/406—Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links
    • 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
    • F16B39/00—Locking of screws, bolts or nuts
    • F16B39/02—Locking of screws, bolts or nuts in which the locking takes place after screwing down
    • 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
    • F16B39/00—Locking of screws, bolts or nuts
    • F16B39/02—Locking of screws, bolts or nuts in which the locking takes place after screwing down
    • F16B39/10—Locking of screws, bolts or nuts in which the locking takes place after screwing down by a plate, spring, wire or ring immovable with regard to the bolt or object and mainly perpendicular to the axis of the bolt
    • 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
    • F16B39/00—Locking of screws, bolts or nuts
    • F16B39/02—Locking of screws, bolts or nuts in which the locking takes place after screwing down
    • F16B39/10—Locking of screws, bolts or nuts in which the locking takes place after screwing down by a plate, spring, wire or ring immovable with regard to the bolt or object and mainly perpendicular to the axis of the bolt
    • F16B39/103—Locking of screws, bolts or nuts in which the locking takes place after screwing down by a plate, spring, wire or ring immovable with regard to the bolt or object and mainly perpendicular to the axis of the bolt with a locking cup washer, ring or sleeve surrounding the nut or bolt head and being partially deformed on the nut or bolt head, or on the object itself
    • 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
    • F16B39/00—Locking of screws, bolts or nuts
    • F16B39/02—Locking of screws, bolts or nuts in which the locking takes place after screwing down
    • F16B39/12—Locking of screws, bolts or nuts in which the locking takes place after screwing down by means of locknuts
    • F16B39/16—Locking of screws, bolts or nuts in which the locking takes place after screwing down by means of locknuts in which the screw-thread of the locknut differs from that of the nut

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
  • Body Structure For Vehicles (AREA)
  • Transmission Devices (AREA)
  • Tires In General (AREA)
  • Pivots And Pivotal Connections (AREA)
  • Clamps And Clips (AREA)
  • Automobile Manufacture Line, Endless Track Vehicle, Trailer (AREA)
FR0553102A 2005-10-12 2005-10-12 Systeme d'ecrou et mat d'accrochage de moteur d'aeronef comprenant un tel systeme Expired - Fee Related FR2891804B1 (fr)

Priority Applications (9)

Application Number Priority Date Filing Date Title
FR0553102A FR2891804B1 (fr) 2005-10-12 2005-10-12 Systeme d'ecrou et mat d'accrochage de moteur d'aeronef comprenant un tel systeme
RU2008118224/11A RU2428356C2 (ru) 2005-10-12 2006-10-10 Гаечная система и стойка крепления двигателя летательного аппарата, содержащая такую систему
BRPI0616930-9A BRPI0616930A2 (pt) 2005-10-12 2006-10-10 sistema de porca, montagem compreendendo um conjunto receptor assim como um sistema de porca, dispositivo de compensação dos esforços de impulso gerados por um motor de aeronave e estribo de afixação de um motor
EP06807103A EP1934093A1 (fr) 2005-10-12 2006-10-10 Systeme d'ecrou et mat d'accrochage de moteur d'aeronef comprenant un tel systeme
US12/089,312 US8042764B2 (en) 2005-10-12 2006-10-10 Nut system and aircraft engine mounting structure comprising same
PCT/EP2006/067217 WO2007042508A1 (fr) 2005-10-12 2006-10-10 Systeme d'ecrou et mat d'accrochage de moteur d'aeronef comprenant un tel systeme
CN2006800378146A CN101282877B (zh) 2005-10-12 2006-10-10 螺母***以及包含该***的、用于航空器发动机的悬挂架
CA2624476A CA2624476C (fr) 2005-10-12 2006-10-10 Systeme d'ecrou et mat d'accrochage de moteur d'aeronef comprenant un tel systeme
JP2008535011A JP2009511336A (ja) 2005-10-12 2006-10-10 ナットシステムおよび同じシステムを具備した航空機エンジンの組み付け構造

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0553102A FR2891804B1 (fr) 2005-10-12 2005-10-12 Systeme d'ecrou et mat d'accrochage de moteur d'aeronef comprenant un tel systeme

Publications (2)

Publication Number Publication Date
FR2891804A1 FR2891804A1 (fr) 2007-04-13
FR2891804B1 true FR2891804B1 (fr) 2009-05-01

Family

ID=36694341

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0553102A Expired - Fee Related FR2891804B1 (fr) 2005-10-12 2005-10-12 Systeme d'ecrou et mat d'accrochage de moteur d'aeronef comprenant un tel systeme

Country Status (9)

Country Link
US (1) US8042764B2 (fr)
EP (1) EP1934093A1 (fr)
JP (1) JP2009511336A (fr)
CN (1) CN101282877B (fr)
BR (1) BRPI0616930A2 (fr)
CA (1) CA2624476C (fr)
FR (1) FR2891804B1 (fr)
RU (1) RU2428356C2 (fr)
WO (1) WO2007042508A1 (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3000529B1 (fr) * 2012-12-28 2015-03-06 Airbus Operations Sas Dispositif de liaison souple pour ensemble propulsif d'aeronef
EP3024729B1 (fr) 2013-07-26 2022-04-27 MRA Systems, LLC Mât d'accrochage de moteur pour aéronef
FR3013678B1 (fr) * 2013-11-25 2015-11-20 Airbus Operations Sas Carenage aerodynamique
FR3014973B1 (fr) 2013-12-12 2016-01-22 Airbus Operations Sas Assemblage comprenant un axe d'articulation supporte par une chape et immobilise en translation par un dispositif de blocage integrant un double systeme d'anti-rotation
GB201417202D0 (en) * 2014-09-30 2014-11-12 Rolls Royce Plc Gas Turbine Engine Mounting Arrangement
CN107521706A (zh) * 2017-07-28 2017-12-29 中国航空工业集团公司西安飞机设计研究所 发动机辅助安装接头
CN109592056B (zh) * 2018-11-02 2022-03-15 中国航空工业集团公司西安飞机设计研究所 一种加油机吊舱悬挂方法
IT202100010319A1 (it) * 2021-04-23 2022-10-23 Leonardo Spa Gruppo per il montaggio di un pylon sub-alare ad una centina di una semiala di aeromobile
FR3125798A1 (fr) * 2021-07-28 2023-02-03 Airbus Operations Ensemble propulsif pour aéronef comportant un turboréacteur, un mât et des moyens d’accrochage du turboréacteur au mât

Family Cites Families (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US684928A (en) * 1900-09-25 1901-10-22 Naftaly Newman Nut-lock.
US893081A (en) * 1908-04-09 1908-07-14 Andrew Kunan Nut-lock.
US1230745A (en) * 1915-07-28 1917-06-19 Charles C Madison Nut-lock.
US1241181A (en) * 1917-07-05 1917-09-25 John Frederick Wilhelm Nut-lock.
US1413024A (en) * 1920-12-04 1922-04-18 Annie L Harrell Lock nut and bolt
CH166876A (fr) * 1933-05-23 1934-01-31 Erismann Gerard Dispositif de serrage de sûreté.
DE800512C (de) * 1948-10-02 1950-11-13 Paul Steinmetzer Schraubenmutter-Sicherung
US3964530A (en) * 1972-05-30 1976-06-22 General Motors Corporation Locking cup washer
SE363384B (fr) * 1972-06-29 1974-01-14 Aby Ab
GB2010969A (en) * 1977-12-22 1979-07-04 Rolls Royce Mounting for Gas Turbine Jet Propulsion Engine
US4266590A (en) * 1979-04-09 1981-05-12 Microdot Inc. Prevailing torque nut
US4846614A (en) * 1986-12-08 1989-07-11 Rolf Steinbock Differential thread for transfer of screw thread forces
US4781502A (en) * 1987-10-26 1988-11-01 The United States Of America As Represented By The Secretary Of The Air Force Anti-rotation locking device for fasteners
CN2103041U (zh) * 1991-08-21 1992-04-29 蒋志忠 组合式防松螺母
US5452575A (en) * 1993-09-07 1995-09-26 General Electric Company Aircraft gas turbine engine thrust mount
CN1042168C (zh) * 1993-09-28 1999-02-17 蒋志忠 组合式防松螺帽
US5391032A (en) * 1993-10-27 1995-02-21 Vassalotti; Michael Reusable positive bolt locking device
US5873547A (en) * 1997-05-20 1999-02-23 The Boeing Company Aircraft engine thrust mount
US6290442B1 (en) * 1997-09-18 2001-09-18 Okabe Corporation, Inc. Locking fastener assembly for threaded joint
JP2001027214A (ja) * 1999-07-12 2001-01-30 Nec Eng Ltd ２段式ボルトとこの２段式ボルトを用いた締結構造
DE10030280A1 (de) * 2000-06-20 2002-01-31 Zahnradfabrik Friedrichshafen Verbindungsanordnung
GB2365091B (en) * 2000-07-21 2003-10-22 Wheelsure Ltd Improved wheel nut assembly
RU2191299C2 (ru) 2000-12-08 2002-10-20 Открытое акционерное общество Таганрогский авиационный научно-технический комплекс им. Г.М.Бериева Самостопорящееся резьбовое соединение
FR2856656B1 (fr) * 2003-06-30 2006-12-01 Snecma Moteurs Suspension arriere de moteur d'avion avec bielles de reprise de poussee et palonnier en forme de boomerang
FR2891251B1 (fr) * 2005-09-28 2009-04-03 Airbus France Sas Mat d'accrochage de moteur pour aeronef
FR2893367B1 (fr) * 2005-11-17 2007-12-21 Airbus France Sas Dispositif de securisation d'un insert dans une structure
FR2903075B1 (fr) * 2006-06-29 2008-10-10 Airbus France Sas Dispositif d'articulation d'un capot de nacelle de moteur d'aeronef sur une structure portante

Also Published As

Publication number Publication date
FR2891804A1 (fr) 2007-04-13
CN101282877A (zh) 2008-10-08
JP2009511336A (ja) 2009-03-19
US8042764B2 (en) 2011-10-25
BRPI0616930A2 (pt) 2011-07-05
EP1934093A1 (fr) 2008-06-25
CA2624476A1 (fr) 2007-04-19
WO2007042508A1 (fr) 2007-04-19
CA2624476C (fr) 2014-11-04
US20080232924A1 (en) 2008-09-25
RU2428356C2 (ru) 2011-09-10
CN101282877B (zh) 2013-03-13
RU2008118224A (ru) 2009-11-20

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Legal Events

Date Code Title Description
CA Change of address

Effective date: 20110916

CD Change of name or company name

Owner name: AIRBUS HOLDING, FR

Effective date: 20110916

CJ Change in legal form

Effective date: 20110916

TP Transmission of property

Owner name: AIRBUS HOLDING, FR

Effective date: 20110913

PLFP Fee payment

Year of fee payment: 11

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Year of fee payment: 16

ST Notification of lapse

Effective date: 20220605