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 PDFInfo
- 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
- Authority
- 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
Links
Classifications
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- 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
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/16—Aircraft characterised by the type or position of power plants of jet type
- B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
- B64C3/185—Spars
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/32—Wings specially adapted for mounting power plant
-
- 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
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
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)
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)
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 |
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2019
- 2019-08-28 FR FR1909483A patent/FR3100227B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR3100227A1 (en) | 2021-03-05 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 2 |
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PLSC | Publication of the preliminary search report |
Effective date: 20210305 |
|
PLFP | Fee payment |
Year of fee payment: 3 |
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PLFP | Fee payment |
Year of fee payment: 4 |
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PLFP | Fee payment |
Year of fee payment: 5 |