FR3100227B1 - SET FOR AN AIRCRAFT, LEDIT SET CONTAINING A MAST AND A WING - Google Patents

SET FOR AN AIRCRAFT, LEDIT SET CONTAINING A MAST AND A WING Download PDF

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Publication number
FR3100227B1
FR3100227B1 FR1909483A FR1909483A FR3100227B1 FR 3100227 B1 FR3100227 B1 FR 3100227B1 FR 1909483 A FR1909483 A FR 1909483A FR 1909483 A FR1909483 A FR 1909483A FR 3100227 B1 FR3100227 B1 FR 3100227B1
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FR
France
Prior art keywords
housing
spar
window
opening
mast
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
FR1909483A
Other languages
French (fr)
Other versions
FR3100227A1 (en
Inventor
Christophe Labarthe
Michael Berjot
Didier Rovatti
Thomas Candela
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 FR1909483A priority Critical patent/FR3100227B1/en
Publication of FR3100227A1 publication Critical patent/FR3100227A1/en
Application granted granted Critical
Publication of FR3100227B1 publication Critical patent/FR3100227B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/16Aircraft characterised by the type or position of power plants of jet type
    • B64D27/18Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/18Spars; Ribs; Stringers
    • B64C3/185Spars
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/32Wings specially adapted for mounting power plant
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40Arrangements for mounting power plants in aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Connection Of Plates (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

ENSEMBLE POUR UN AERONEF, LEDIT ENSEMBLE COMPORTANT UN MAT ET UNE AILE L’invention concerne un ensemble (200) comportant un mât (106) avec un longeron supérieur (202) et deux pelles latérales (230), une aile (104) avec une peau (210) et un longeron avant (208), des équerres avant/arrière bâbord/tribord, chacune avec un logement (218, 220) pour un écrou à manchon fileté (222). Le longeron avant (208) présente des plis avant/vertical (208a-b), où chaque équerre arrière (214a-b) se positionne contre le pli vertical (208b) et la peau (210), et où pour chaque logement arrière (220), l’équerre arrière (214) associée est percée d’un alésage débouchant (224) dans ledit logement (220). Pour chaque logement arrière (220), l’ensemble (200) comporte un boulon de fixation comportant l’écrou à manchon fileté (222) et une vis (226) et où chaque logement arrière (220) présente une ouverture (240) orientée vers le pli vertical (208b), le pli vertical (208b) présente une première fenêtre (242) alignée avec l’ouverture (240) et l’équerre avant (212a-b) présente une deuxième fenêtre (244) alignée avec l’ouverture (240) et la première fenêtre (242). Un tel ensemble permet d’accéder aux écrous qui sont à l’arrière du longeron avant ce qui facilite le travail des opérateurs. Fig. 3The invention relates to an assembly (200) comprising a mast (106) with an upper spar (202) and two side shovels (230), a wing (104) with a skin (210) and a forward spar (208), fore / aft port / starboard brackets, each with a housing (218, 220) for a threaded sleeve nut (222). The front spar (208) has front / vertical creases (208a-b), where each rear bracket (214a-b) fits against the vertical crease (208b) and skin (210), and where for each rear housing ( 220), the associated rear bracket (214) is pierced with a through bore (224) in said housing (220). For each rear housing (220), the assembly (200) has a mounting bolt including the threaded sleeve nut (222) and a screw (226) and where each rear housing (220) has an opening (240) oriented Towards the vertical fold (208b), the vertical fold (208b) has a first window (242) aligned with the opening (240) and the front bracket (212a-b) has a second window (244) aligned with the opening (240) and the first window (242). Such an assembly provides access to the nuts which are at the rear of the front spar, which facilitates the work of the operators. Fig. 3

FR1909483A 2019-08-28 2019-08-28 SET FOR AN AIRCRAFT, LEDIT SET CONTAINING A MAST AND A WING Active FR3100227B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1909483A FR3100227B1 (en) 2019-08-28 2019-08-28 SET FOR AN AIRCRAFT, LEDIT SET CONTAINING A MAST AND A WING

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1909483 2019-08-28
FR1909483A FR3100227B1 (en) 2019-08-28 2019-08-28 SET FOR AN AIRCRAFT, LEDIT SET CONTAINING A MAST AND A WING

Publications (2)

Publication Number Publication Date
FR3100227A1 FR3100227A1 (en) 2021-03-05
FR3100227B1 true FR3100227B1 (en) 2021-09-24

Family

ID=68807090

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1909483A Active FR3100227B1 (en) 2019-08-28 2019-08-28 SET FOR AN AIRCRAFT, LEDIT SET CONTAINING A MAST AND A WING

Country Status (1)

Country Link
FR (1) FR3100227B1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116256763B (en) * 2023-05-10 2023-08-15 武汉理工大学 Bridge disease detection device and detection method

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3065441B1 (en) * 2017-04-19 2019-07-05 Airbus Operations AIRCRAFT ASSEMBLY COMPRISING A PRIMARY STRUCTURE OF A COUPLING MAT FIXED TO A SAILBOX USING A BOLT CONNECTION
GB2569315A (en) * 2017-12-13 2019-06-19 Airbus Operations Ltd Assembly with captive nut

Also Published As

Publication number Publication date
FR3100227A1 (en) 2021-03-05

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