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FR2990415B1 - Ferrure d'un dispositif d'etayage d'un aeronef - Google Patents

Ferrure d'un dispositif d'etayage d'un aeronef

Info

Publication number
FR2990415B1
FR2990415B1 FR1254321A FR1254321A FR2990415B1 FR 2990415 B1 FR2990415 B1 FR 2990415B1 FR 1254321 A FR1254321 A FR 1254321A FR 1254321 A FR1254321 A FR 1254321A FR 2990415 B1 FR2990415 B1 FR 2990415B1
Authority
FR
France
Prior art keywords
aircraft
shaping
fastening
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
FR1254321A
Other languages
English (en)
Other versions
FR2990415A1 (fr
Inventor
Mickael Matignon
Francis Ramond
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 SAS
Original Assignee
Airbus 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
Application filed by Airbus SAS filed Critical Airbus SAS
Priority to FR1254321A priority Critical patent/FR2990415B1/fr
Priority to US13/891,305 priority patent/US9587670B2/en
Publication of FR2990415A1 publication Critical patent/FR2990415A1/fr
Application granted granted Critical
Publication of FR2990415B1 publication Critical patent/FR2990415B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
    • 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
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C11/00—Pivots; Pivotal connections
    • F16C11/04—Pivotal connections
    • F16C11/06—Ball-joints; Other joints having more than one degree of angular freedom, i.e. universal joints
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/50—Handling or transporting aircraft components
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B66—HOISTING; LIFTING; HAULING
    • B66C—CRANES; LOAD-ENGAGING ELEMENTS OR DEVICES FOR CRANES, CAPSTANS, WINCHES, OR TACKLES
    • B66C1/00—Load-engaging elements or devices attached to lifting or lowering gear of cranes or adapted for connection therewith for transmitting lifting forces to articles or groups of articles
    • B66C1/10—Load-engaging elements or devices attached to lifting or lowering gear of cranes or adapted for connection therewith for transmitting lifting forces to articles or groups of articles by mechanical means
    • 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
    • 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
    • Y10T403/32631—Universal ball and socket

Landscapes

  • Engineering & Computer Science (AREA)
  • Transportation (AREA)
  • Manufacturing & Machinery (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Connection Of Plates (AREA)
FR1254321A 2012-05-11 2012-05-11 Ferrure d'un dispositif d'etayage d'un aeronef Active FR2990415B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1254321A FR2990415B1 (fr) 2012-05-11 2012-05-11 Ferrure d'un dispositif d'etayage d'un aeronef
US13/891,305 US9587670B2 (en) 2012-05-11 2013-05-10 Fitting for an aircraft bracing device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1254321A FR2990415B1 (fr) 2012-05-11 2012-05-11 Ferrure d'un dispositif d'etayage d'un aeronef

Publications (2)

Publication Number Publication Date
FR2990415A1 FR2990415A1 (fr) 2013-11-15
FR2990415B1 true FR2990415B1 (fr) 2014-06-13

Family

ID=46579078

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1254321A Active FR2990415B1 (fr) 2012-05-11 2012-05-11 Ferrure d'un dispositif d'etayage d'un aeronef

Country Status (2)

Country Link
US (1) US9587670B2 (fr)
FR (1) FR2990415B1 (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9682429B2 (en) * 2015-04-22 2017-06-20 The Boeing Company Reaction tool and method for forming openings in an aircraft fuselage joint
US10577774B2 (en) * 2016-05-31 2020-03-03 Caterpillar Inc. Trunnion and socket assembly
JP7029416B2 (ja) * 2016-06-23 2022-03-03 ヘキサゴン テクノロジー アーエス 内部軸受を有するボス
DE102018112783A1 (de) * 2018-05-29 2019-12-05 Airbus Operations Gmbh System zum Verspannen eines Einbauelements in einem Innenraum eines Fahrzeugs
FR3096597B1 (fr) * 2019-05-29 2021-05-07 Safran Nacelles Dispositif pour la fixation d’un outillage de levage sur porte d’inverseur de poussée de nacelle d’aéronef
US11260954B2 (en) * 2019-10-09 2022-03-01 The Boeing Company Apparatus for attaching aircraft wing structural components
US11105375B2 (en) * 2020-01-09 2021-08-31 Caterpillar Inc. Retention system for bearing member
DE102021205352A1 (de) * 2020-08-03 2022-02-03 Sacs Aerospace Gmbh Beschlagteil
US12344402B1 (en) * 2024-05-22 2025-07-01 The Boeing Company Angularly adjustable support tool indexes and related methods

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5141357A (en) * 1991-01-09 1992-08-25 Sundstrand Corp. Misalignment compensating fastener insert
US5326206A (en) * 1993-04-19 1994-07-05 Northrop Corporation Method for compensating for bolt hole misalignment and bolt assemblies therefor
US5823588A (en) * 1995-11-13 1998-10-20 Morghen; Manfred A. Universal hoist assembly
US8083175B2 (en) * 2007-11-09 2011-12-27 The Boeing Company Loading fitting having intersecting holes in the web side and end

Also Published As

Publication number Publication date
FR2990415A1 (fr) 2013-11-15
US20130302083A1 (en) 2013-11-14
US9587670B2 (en) 2017-03-07

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