FR3071222B1 - SYSTEM AND METHOD FOR SUPPORT AND GUIDANCE OF AN AIRCRAFT OPENER - Google Patents

SYSTEM AND METHOD FOR SUPPORT AND GUIDANCE OF AN AIRCRAFT OPENER Download PDF

Info

Publication number
FR3071222B1
FR3071222B1 FR1758686A FR1758686A FR3071222B1 FR 3071222 B1 FR3071222 B1 FR 3071222B1 FR 1758686 A FR1758686 A FR 1758686A FR 1758686 A FR1758686 A FR 1758686A FR 3071222 B1 FR3071222 B1 FR 3071222B1
Authority
FR
France
Prior art keywords
aircraft
rotation
opener
guidance
support
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
FR1758686A
Other languages
French (fr)
Other versions
FR3071222A1 (en
Inventor
Christian Romec
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.)
Latecoere SA
Original Assignee
Latecoere 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
Application filed by Latecoere SA filed Critical Latecoere SA
Priority to FR1758686A priority Critical patent/FR3071222B1/en
Publication of FR3071222A1 publication Critical patent/FR3071222A1/en
Application granted granted Critical
Publication of FR3071222B1 publication Critical patent/FR3071222B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • 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
    • B64C1/1423—Passenger doors

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automatic Assembly (AREA)
  • Hinges (AREA)

Abstract

Ce système de support et de guidage d'un ouvrant d'aéronef comprend au moins deux bielles (5, 6) comprenant chacune une première extrémité (7) destinée à être liée à l'ouvrant et une deuxième extrémité (8) destinée à être liée au fuselage de l'aéronef, les extrémités de chaque bielle comprenant chacune une articulation (9) autour d'un premier axe de rotation (A1) par rapport à la porte et au fuselage et d'un deuxième axe de rotation (A2) par rapport aux bielles, distinct du premier axe, les premiers axes de rotation (A1) des première et deuxième extrémités étant parallèles et décalés l'un par rapport à l'autre et les deuxièmes axes de rotation (A2) des première et deuxième extrémités étant parallèles et décalés l'un par rapport à l'autre.This system for supporting and guiding an aircraft opening comprises at least two connecting rods (5, 6) each comprising a first end (7) intended to be linked to the opening and a second end (8) intended to be linked to the fuselage of the aircraft, the ends of each connecting rod each comprising an articulation (9) about a first axis of rotation (A1) relative to the door and to the fuselage and of a second axis of rotation (A2) relative to the connecting rods, distinct from the first axis, the first axes of rotation (A1) of the first and second ends being parallel and offset with respect to one another and the second axes of rotation (A2) of the first and second ends being parallel and offset from one another.

FR1758686A 2017-09-20 2017-09-20 SYSTEM AND METHOD FOR SUPPORT AND GUIDANCE OF AN AIRCRAFT OPENER Active FR3071222B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1758686A FR3071222B1 (en) 2017-09-20 2017-09-20 SYSTEM AND METHOD FOR SUPPORT AND GUIDANCE OF AN AIRCRAFT OPENER

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1758686A FR3071222B1 (en) 2017-09-20 2017-09-20 SYSTEM AND METHOD FOR SUPPORT AND GUIDANCE OF AN AIRCRAFT OPENER
FR1758686 2017-09-20

Publications (2)

Publication Number Publication Date
FR3071222A1 FR3071222A1 (en) 2019-03-22
FR3071222B1 true FR3071222B1 (en) 2020-11-27

Family

ID=60302315

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1758686A Active FR3071222B1 (en) 2017-09-20 2017-09-20 SYSTEM AND METHOD FOR SUPPORT AND GUIDANCE OF AN AIRCRAFT OPENER

Country Status (1)

Country Link
FR (1) FR3071222B1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102018130527B3 (en) * 2018-11-30 2020-01-09 Airbus Operations Gmbh Door arrangement with articulated arm, aircraft area with door arrangement and aircraft with aircraft area
FR3118941B1 (en) * 2021-01-21 2023-01-06 Latecoere Method and assembly of a connecting rod locking vehicle door stabilizer guide.
FR3140396A1 (en) * 2022-09-29 2024-04-05 Latecoere Door locking mechanism in circular translation.

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3791073A (en) * 1972-04-28 1974-02-12 Boeing Co Aircraft door with moving hinge line
GB2042060B (en) * 1979-02-09 1983-01-06 Boeing Co Folding plug type aircraft door
DE10258105B4 (en) * 2002-12-11 2008-12-04 Eurocopter Deutschland Gmbh Aircraft door arrangement
DE102008030696A1 (en) * 2008-07-01 2010-01-14 Eurocopter Deutschland Gmbh Airplane door with support arm arrangement
AT515354A1 (en) * 2014-01-21 2015-08-15 Facc Ag Device for opening an aircraft door
DE102015224449A1 (en) * 2015-12-07 2017-06-08 Airbus Operations Gmbh Vehicle door unit and vehicle with door unit

Also Published As

Publication number Publication date
FR3071222A1 (en) 2019-03-22

Similar Documents

Publication Publication Date Title
FR3071222B1 (en) SYSTEM AND METHOD FOR SUPPORT AND GUIDANCE OF AN AIRCRAFT OPENER
EP3324714B1 (en) Supporting device for rail member
FR3093891B1 (en) Feeding device for animals
FR3057047B1 (en) CONTROLLED ANGULAR POSITION CLAMPING SYSTEM FOR CONNECTING TWO TUBES
WO2017123166A3 (en) Movable detector and methods for inspecting elongated tube-like objects in equipment
FR2996437B1 (en) MULTI-VISION IMAGING SYSTEM FOR LAPAROSCOPIC SURGERY
EP3130918A8 (en) Apparatus for fixing of measuring device for monitoring bottom shape near bridge support to bridge structure, method for fixing such apparatus to bridge structure and sling for such fixing
EP3928929A4 (en) Auxiliary photographing device for movement disorder disease analysis, control method and apparatus
EP3864396A4 (en) Ndir sensor, sampling method and system for breath analysis
EP2626502A3 (en) Device for connection between leaf and frame in order to produce a panel with adjustable leaves and panel obtained
EP1990501A3 (en) Slat arrangement in a roller shutter for an opening in a building
ATE395280T1 (en) SWITCH DEVICE FOR A CONVEYOR
FR3061316B1 (en) TRAINING DEVICE
WO2018069462A8 (en) Position determination device for determining a position of an instrument within a tubular structure
EP3051030A3 (en) Apparatus for burying cables, pipes and the like, and operating method thereof
EP2922242A3 (en) Methods and Apparatus to Determine Network Delay with Location Independence
FR3034443A1 (en) DETECTION DEVICE, CONSTRUCTION COMPRISING SUCH A DEVICE AND METHOD FOR COATING A REFERENCE SURFACE USING SUCH AN INTERFACE DEVICE
FR3074467B1 (en) SUPPORT AND GUIDANCE DEVICE FOR A TRACTOR CABLE OF A VEHICLE TRANSPORTATION INSTALLATION AND PROCESS FOR INSPECTING SUCH A DEVICE
FR3042175B1 (en) TOOLS FOR THE HANDLING OF AN AIRCRAFT TURBOREACTOR NACELLE
FR3080360B1 (en) RECOVERY AND STORAGE DEVICE FOR A MAINSAIL AFTER FLOODING
FR3096884B1 (en) Instrument for guiding a fixation device through an intramedullary rod
EP3028916A3 (en) Gangway arrangement, intended to equip a public transport jointed vehicle, in particular a railway vehicle
FR3061130B1 (en) THERMOPHONIC INSULATION MODULE FOR AIRCRAFT COMPRISING A MATTRESS AND A BEARING STRUCTURE, AND THERMOPHONIC INSULATION METHOD OF AN AIRCRAFT BY MEANS OF SUCH A MODULE
FR3063303B1 (en) PERFECTED MOTORIZED SLIDING GATE
CN107859810A (en) Adjustable support device and its system

Legal Events

Date Code Title Description
PLSC Publication of the preliminary search report

Effective date: 20190322

PLFP Fee payment

Year of fee payment: 3

PLFP Fee payment

Year of fee payment: 4

PLFP Fee payment

Year of fee payment: 5

PLFP Fee payment

Year of fee payment: 6

PLFP Fee payment

Year of fee payment: 7