FR3084704B1 - PIVOTING CONNECTION DEVICE BETWEEN AT LEAST TWO PARTS, AIRCRAFT INCLUDING A HOOD EQUIPPED WITH THE SAID PIVOTING CONNECTION DEVICE - Google Patents

PIVOTING CONNECTION DEVICE BETWEEN AT LEAST TWO PARTS, AIRCRAFT INCLUDING A HOOD EQUIPPED WITH THE SAID PIVOTING CONNECTION DEVICE Download PDF

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Publication number
FR3084704B1
FR3084704B1 FR1857330A FR1857330A FR3084704B1 FR 3084704 B1 FR3084704 B1 FR 3084704B1 FR 1857330 A FR1857330 A FR 1857330A FR 1857330 A FR1857330 A FR 1857330A FR 3084704 B1 FR3084704 B1 FR 3084704B1
Authority
FR
France
Prior art keywords
connection device
pivoting connection
parts
branches
orifice
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
FR1857330A
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French (fr)
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FR3084704A1 (en
Inventor
Paolo Messina
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
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR1857330A priority Critical patent/FR3084704B1/en
Publication of FR3084704A1 publication Critical patent/FR3084704A1/en
Application granted granted Critical
Publication of FR3084704B1 publication Critical patent/FR3084704B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C11/00—Pivots; Pivotal connections
    • F16C11/04—Pivotal connections
    • F16C11/045—Pivotal connections with at least a pair of arms pivoting relatively to at least one other arm, all arms being mounted on one pin
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
    • 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
    • B64D29/08—Inspection panels for power plants
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
    • B64C1/1407—Doors; surrounding frames
    • B64C1/1446—Inspection hatches
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C7/00—Structures or fairings not otherwise provided for
    • B64C7/02—Nacelles

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Pivots And Pivotal Connections (AREA)

Abstract

L'invention a pour objet un dispositif de liaison pivotante reliant au moins deux pièces (52, 54) et comprenant : - une chape (56) présentant des première et deuxième branches (58, 60) présentant chacune un orifice traversant (66, 68), - un bras (62), positionné entre les première et deuxième branches (58, 60) de la chape (56), présentant un orifice traversant (70), - un axe cylindrique (64) reliant la chape (56) et le bras (62), présentant une nervure (78) en saillie qui a une longueur inférieure ou égale à la distance séparant les première et deuxième branches (58, 60), l'orifice (70) du bras (62) présentant une première rainure, configurée pour loger au moins partiellement la nervure (78) de l'axe cylindrique (64), qui s'étend d'une face latérale (F62, F62') à l'autre du bras (62), - au moins un orifice (66, 68) des première et deuxième branches (58, 60) présentant une deuxième rainure configurée pour permettre un passage de la nervure (78) de l'axe cylindrique (64).The subject of the invention is a pivoting connection device connecting at least two parts (52, 54) and comprising: - a yoke (56) having first and second branches (58, 60) each having a through orifice (66, 68 ), - an arm (62), positioned between the first and second branches (58, 60) of the yoke (56), having a through orifice (70), - a cylindrical axis (64) connecting the yoke (56) and the arm (62), having a projecting rib (78) which has a length less than or equal to the distance between the first and second branches (58, 60), the orifice (70) of the arm (62) having a first groove, configured to at least partially accommodate the rib (78) of the cylindrical axis (64), which extends from one side face (F62, F62 ') to the other of the arm (62), - at least an orifice (66, 68) of the first and second branches (58, 60) having a second groove configured to allow passage of the rib (78) of the cylindrical axis (64).

FR1857330A 2018-08-06 2018-08-06 PIVOTING CONNECTION DEVICE BETWEEN AT LEAST TWO PARTS, AIRCRAFT INCLUDING A HOOD EQUIPPED WITH THE SAID PIVOTING CONNECTION DEVICE Active FR3084704B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1857330A FR3084704B1 (en) 2018-08-06 2018-08-06 PIVOTING CONNECTION DEVICE BETWEEN AT LEAST TWO PARTS, AIRCRAFT INCLUDING A HOOD EQUIPPED WITH THE SAID PIVOTING CONNECTION DEVICE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1857330A FR3084704B1 (en) 2018-08-06 2018-08-06 PIVOTING CONNECTION DEVICE BETWEEN AT LEAST TWO PARTS, AIRCRAFT INCLUDING A HOOD EQUIPPED WITH THE SAID PIVOTING CONNECTION DEVICE

Publications (2)

Publication Number Publication Date
FR3084704A1 FR3084704A1 (en) 2020-02-07
FR3084704B1 true FR3084704B1 (en) 2020-12-18

Family

ID=63722634

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1857330A Active FR3084704B1 (en) 2018-08-06 2018-08-06 PIVOTING CONNECTION DEVICE BETWEEN AT LEAST TWO PARTS, AIRCRAFT INCLUDING A HOOD EQUIPPED WITH THE SAID PIVOTING CONNECTION DEVICE

Country Status (1)

Country Link
FR (1) FR3084704B1 (en)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US737360A (en) * 1903-07-01 1903-08-25 Frank M Daly Knuckle-joint.
US1030801A (en) * 1912-02-27 1912-06-25 Edwin J Berault Hinge.
CA2237976A1 (en) * 1998-06-15 1999-12-15 Christian Guillemette Lockable hinge device
FR2887854B1 (en) * 2005-06-30 2008-08-08 Airbus France Sas PLATFORM FOR AN AIRCRAFT AND AN AIRCRAFT PROVIDED WITH AT LEAST ONE SUCH NACELLE

Also Published As

Publication number Publication date
FR3084704A1 (en) 2020-02-07

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