FR2897041A1 - Keelson construction for e.g. beriev 200, has fuselage with lateral walls having specific length and height above floor line, where walls are made of transparent cellulose acetate of specific thickness and specific density - Google Patents
Keelson construction for e.g. beriev 200, has fuselage with lateral walls having specific length and height above floor line, where walls are made of transparent cellulose acetate of specific thickness and specific density Download PDFInfo
- Publication number
- FR2897041A1 FR2897041A1 FR0601050A FR0601050A FR2897041A1 FR 2897041 A1 FR2897041 A1 FR 2897041A1 FR 0601050 A FR0601050 A FR 0601050A FR 0601050 A FR0601050 A FR 0601050A FR 2897041 A1 FR2897041 A1 FR 2897041A1
- Authority
- FR
- France
- Prior art keywords
- fuselage
- specific
- beriev
- walls
- keelson
- 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.)
- Withdrawn
Links
- 238000010276 construction Methods 0.000 title abstract description 4
- 229920002301 cellulose acetate Polymers 0.000 title abstract 2
- 238000004519 manufacturing process Methods 0.000 claims description 4
- 230000006978 adaptation Effects 0.000 claims 3
- 238000003287 bathing Methods 0.000 claims 1
- 229910052751 metal Inorganic materials 0.000 description 5
- 239000002184 metal Substances 0.000 description 5
- 229910000838 Al alloy Inorganic materials 0.000 description 3
- UHOVQNZJYSORNB-UHFFFAOYSA-N Benzene Chemical compound C1=CC=CC=C1 UHOVQNZJYSORNB-UHFFFAOYSA-N 0.000 description 3
- 239000000463 material Substances 0.000 description 2
- 241001669679 Eleotris Species 0.000 description 1
- 240000002871 Tectona grandis Species 0.000 description 1
- 238000009835 boiling Methods 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 239000004519 grease Substances 0.000 description 1
- 230000005802 health problem Effects 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
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
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/064—Stringers; Longerons
-
- 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
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/065—Spars
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C35/00—Flying-boats; Seaplanes
-
- 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
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Body Structure For Vehicles (AREA)
Abstract
Description
DESCRIPTION -1-DESCRIPTION -1-
La présente invention consiste en la construction d'une carlingue transparente pour l'hydravion amphibie de fabrication russe BERIEV 200, aménagé intérieurement comme un navire de plaisance avec : des cabines couchettes individuelles, un carré salon et cuisine, un pont solarium, des sièges équipés de ceintures de sécurité. The present invention consists of the construction of a transparent cabin for the amphibious seaplane of Russian manufacture BERIEV 200, fitted out internally as a pleasure vessel with: individual berth cabins, a saloon and galley, a solarium deck, equipped seats seat belts.
Une version d'aménagement optimisé de la carlingue (planche 1/2) permet de déterminer, après le poste de pilotage, une première zone (I) où on trouve deux cabines simples (2) cloisonnées, de 2,OOm de long sur 0, 90m de large ; de part et d'autre d'une coursive centrale (3) de 0,70m de largeur, permettant d'accéder au cockpit (1). An optimized version of the cabin layout (board 1/2) makes it possible to determine, after the cockpit, a first zone (I) where there are two single cabins (2) partitioned, 2.0Om long by 0 , 90m wide; on either side of a central passageway (3) 0.70m wide, providing access to the cockpit (1).
Dans le prolongement de la cabine simple (2) à bâbord, un cabinet de toilettes (4) de 1,OOm de long et 0,90m de large ouvre sur la coursive (3). In the extension of the single cabin (2) on the port side, a toilet (4) 1. OOm long and 0.90m wide opens onto the passageway (3).
Dans le prolongement de la cabine simple (2) tribord, une cabine de douche (5) de 1,OOm/0,90m, équipée d'un lavabo, ouvre entièrement vers l'arrière sur le pont (II)qui constitue la deuxième zone (II)... Surface de la zone I : 7,50m2. Le pont (II) garni sur toute sa surface de lattes de teck, est composé par : le plancher (6) de la partie centrale de la carlingue, soit une surface de 4,OOm x 2,50m = 10m2 ; deux portes (7), de 25 4,OOm x 1,70m = 6,80m2 chacune, pivotant autour de trois charnières attachées à leur partie inférieure, et maintenues horizontalement de part et d'autre du fuselage, grâce à des vérins hydrauliques servant également à les actionner pour assurer leur ouverture et leur fermeture. Les portes (7) déployées (seulement lorsque l'avion est à l'arrêt), le pont (II) offre une surface totale de 23,60m2. As an extension of the starboard single cabin (2), a 1. OOm / 0.90m shower cabin (5), equipped with a washbasin, opens entirely to the rear onto the deck (II) which constitutes the second zone (II) ... Area of zone I: 7.50m2. Deck (II), lined over its entire surface with teak slats, is made up of: the floor (6) of the central part of the cabin, ie a surface area of 4.0m x 2.50m = 10m2; two doors (7), 25 4. OOm x 1.70m = 6.80m2 each, pivoting around three hinges attached to their lower part, and held horizontally on either side of the fuselage, thanks to hydraulic jacks serving also to actuate them to ensure their opening and closing. With the doors (7) deployed (only when the aircraft is stationary), the deck (II) offers a total surface area of 23.60m2.
Elles sont sécurisées et confirmées en position fermées/verrouillées mécaniquement, avant le décollage. They are secured and confirmed in the closed / mechanically locked position, before take-off.
Toute la partie avant du fuselage, depuis le nez (soit environ 15,OOm) englobant le poste de pilotage, et les zones I et II sont entièrement en alliage d'aluminium. 2897041 -2- The entire front part of the fuselage, from the nose (approximately 15,000 m) including the cockpit, and zones I and II are entirely in aluminum alloy. 2897041 -2-
La paroi du fuselage, au niveau de chacune des deux cabines 45 simples de la zone I est ajourée d'un hublot circulaire de 0,60m de diamètre. The wall of the fuselage, at the level of each of the two single cabins 45 of zone I, is perforated with a circular porthole 0.60 m in diameter.
Cette partie du fuselage se termine à l'extrémité arrière du pont 9 à une cinquantaine de centimètres du bord d'attaque 50 (15) de la voilure. This part of the fuselage ends at the rear end of deck 9 about fifty centimeters from the leading edge 50 (15) of the airfoil.
La zone III (planche 1/2) ouvre, sur toute la largeur (2,50m) de la carlingue (sans aucune séparation), sur le pont de la zone II, pour constituer le carré (III). 55 Il s'agit d'un confortable salon séjour bar, meublé : d'une banquette (8), de fauteuils (9), d'une table basse (10) ; de tabourets (11) devant le comptoir (12) d'une cuisine à l'américaine. La zone III s'étend sur une longueur de 3,50m. 60 Elle couvre donc une surface de 3,50m x 2,50m = 8,75m2 Zone III (plank 1/2) opens, over the entire width (2.50m) of the cabin (without any separation), onto the deck of zone II, to constitute the saloon (III). 55 This is a comfortable lounge / bar, furnished with: a bench (8), armchairs (9), a coffee table (10); stools (11) in front of the counter (12) of an American kitchen. Zone III extends over a length of 3.50m. 60 It therefore covers an area of 3.50m x 2.50m = 8.75m2
La quatrième zone (IV) est aménagée avec neuf sièges (13) très confortables (catégorie 1ere classe ), sur trois rangées. Une allée décentrée (14), de 0,50m de large, laisse trois sièges 65 à bâbord, et un à tribord dans chaque travée. La zone IV avec 3,00m de long pour 2,50m de large, s'étend sur 7,50m2. The fourth zone (IV) is fitted out with nine very comfortable seats (13) (1st class category), in three rows. An off-center aisle (14), 0.50m wide, leaves three seats 65 to port, and one to starboard in each bay. Zone IV, 3.00m long and 2.50m wide, covers 7.50m2.
60 La cinquième zone (V) constitue la zone nuit . En effet, elle s'étend sur la portion restante de la carlingue pressurisée (jusqu'à la paroi du fond), soit sur une longueur de 10,50m, et une surface de 22,75m2. Cette zone contient trois cabines couchettes simples à tribord (16), 70 deux doubles avec cabines de toilettes et douche à bâbord (17). En face d'un cabinet de toilettes à bâbord (18), une porte d'accès (19) à l'avion s'ouvre à tribord. Une cabine couchette double (20) occupe le fond de la carlingue. 60 The fifth zone (V) constitutes the night zone. Indeed, it extends over the remaining portion of the pressurized cabin (up to the back wall), i.e. over a length of 10.50m, and a surface area of 22.75m2. This area contains three single berth cabins to starboard (16), 70 two doubles with toilet and shower cabins to port (17). In front of a toilet on the port side (18), an access door (19) to the aircraft opens on the starboard side. A double sleeper cabin (20) occupies the bottom of the cabin.
75 Des coffres à bagages de cabine sont fixés sur la partie supérieure des cloisons. Une trappe peut être prévue dans le plancher de la zone I, pour accéder à une soute dans laquelle seront stockés les objets lourds et encombrants, ainsi que du ravitaillement de toute sorte. 80 2897041 -3 75 Cabin baggage compartments are attached to the upper part of the partitions. A hatch can be provided in the floor of zone I, to access a hold in which heavy and bulky objects will be stored, as well as supplies of all kinds. 80 2897041 -3
La section de la carlingue aménagée est semi circulaire. La hauteur du plafond dans l'axe central est de 2,10m pour une 85 surface de plancher de 56m2 ; ce qui offre un volume d'environ 95m! The section of the fitted cabin is semi-circular. The height of the ceiling in the central axis is 2.10m for a floor area of 56m2; which offers a volume of about 95m!
Seules les parois latérales (21) et (22) du fuselage, le long des zones III, IV et V sont en acétocellulose (CA) transparent, sur 17,00m de 90 longueur, et 1,70m de hauteur au dessus de la ligne du plancher. Une épaisseur de 1 cm assurerait une bonne solidité. Tout le reste de l'enveloppe est en alliage d'aluminium de 3mm. Only the side walls (21) and (22) of the fuselage, along zones III, IV and V are in transparent acetocellulose (CA), on 17.00m of 90 length, and 1.70m of height above the line from the floor. A thickness of 1 cm would ensure good strength. All the rest of the casing is 3mm aluminum alloy.
L'acétocellulose (CA) présente une structure amorphe. 95 Sa densité de 1.2 - 1.3 g/cnt en fait un revêtement plus léger que l'alliage d'aluminium utilisé dans la construction aéronautique, de densité supérieure à 2.7 g/cn? Résilient, résistant à l'eau bouillante, il casse difficilement présente une bonne résistance aux éraflures. 100 Il est de faible charge électrique. Cette matière plastique, convient bien à l'insertion de pièces en métal. Elle ne pose aucun problème pour la santé. Acetocellulose (CA) has an amorphous structure. 95 Its density of 1.2 - 1.3 g / cnt makes it a lighter coating than the aluminum alloy used in aircraft construction, with a density greater than 2.7 g / cn? Resilient, resistant to boiling water, it is difficult to break and has good scratch resistance. 100 It has a low electrical charge. This plastic material is suitable for inserting metal parts. It does not pose any health problem.
105 Ce matériaux résiste aux graisses, essences, et autre benzène. Il est difficilement inflammable, et s'éteint à l'extérieur de la flamme. 105 This material is resistant to grease, gasoline, and other benzene. It is hardly flammable, and goes out outside the flame.
La transparence de l'Acétocellulose (CA) permettra des vues 110 panoramiques exceptionnelles, tel qu'appliqué à un appareil comme le BERIEV 200, dans sa version yacht volant , à vocation exclusivement touristique. The transparency of Acetocellulose (CA) will allow exceptional 110 panoramic views, as applied to a device like the BERIEV 200, in its flying yacht version, exclusively for tourism.
L'acceptabilité de l'acétocellulose à l'insertion de pièces 115 métallique facilitera le rivetage des panneaux de parois transparents sur les couples, les longerons (23, 24) et autres supports métalliques (planche 2/2). Les raccordements entre plaques métalliques et plaques d'acétocellulose (1cm d'épaisseur) devront se faire par 120 chevauchement (25) des premières (plus minces) sur les secondes, pour garantir une jonction homogène surface externe. Intérieurement, un capitonnage discret sera apposé sur la structure métallique apparente. The acceptability of the acetocellulose to the insertion of metal parts 115 will facilitate the riveting of the transparent wall panels on the pairs, the spars (23, 24) and other metal supports (plate 2/2). The connections between metal plates and acetocellulose plates (1cm thick) must be made by 120 overlaps (25) of the first (thinner) on the second, to guarantee a homogeneous external surface junction. Internally, a discreet padding will be affixed to the visible metal structure.
Claims (3)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0601050A FR2897041A1 (en) | 2006-02-07 | 2006-02-07 | Keelson construction for e.g. beriev 200, has fuselage with lateral walls having specific length and height above floor line, where walls are made of transparent cellulose acetate of specific thickness and specific density |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0601050A FR2897041A1 (en) | 2006-02-07 | 2006-02-07 | Keelson construction for e.g. beriev 200, has fuselage with lateral walls having specific length and height above floor line, where walls are made of transparent cellulose acetate of specific thickness and specific density |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2897041A1 true FR2897041A1 (en) | 2007-08-10 |
Family
ID=37000118
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0601050A Withdrawn FR2897041A1 (en) | 2006-02-07 | 2006-02-07 | Keelson construction for e.g. beriev 200, has fuselage with lateral walls having specific length and height above floor line, where walls are made of transparent cellulose acetate of specific thickness and specific density |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2897041A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2724937A1 (en) * | 2012-10-26 | 2014-04-30 | The Boeing Company | Single aisle aircraft lavatory with optimized use of floor space for wheelchair accessibility |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2314949A (en) * | 1940-07-12 | 1943-03-30 | Vultee Aircraft Inc | Airplane |
US3643899A (en) * | 1969-03-07 | 1972-02-22 | Floyd A Firestone | Airplane with spatial panorama |
FR2848525A1 (en) * | 2002-12-11 | 2004-06-18 | Jean Ederique | Interior conversion of Beriev BE 200 seaplane of section from pilot partition to rear of pressurized zone consists of double and single cabins isolated by partitions, sleeper berths, dressing tables, storage cabinets and toilets |
-
2006
- 2006-02-07 FR FR0601050A patent/FR2897041A1/en not_active Withdrawn
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2314949A (en) * | 1940-07-12 | 1943-03-30 | Vultee Aircraft Inc | Airplane |
US3643899A (en) * | 1969-03-07 | 1972-02-22 | Floyd A Firestone | Airplane with spatial panorama |
FR2848525A1 (en) * | 2002-12-11 | 2004-06-18 | Jean Ederique | Interior conversion of Beriev BE 200 seaplane of section from pilot partition to rear of pressurized zone consists of double and single cabins isolated by partitions, sleeper berths, dressing tables, storage cabinets and toilets |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2724937A1 (en) * | 2012-10-26 | 2014-04-30 | The Boeing Company | Single aisle aircraft lavatory with optimized use of floor space for wheelchair accessibility |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |
Effective date: 20081031 |