WO2014058401A2 - Partie de support intermédiaire fonctionnelle utilisée parmi les pieds de sièges de passager dans des avions - Google Patents

Partie de support intermédiaire fonctionnelle utilisée parmi les pieds de sièges de passager dans des avions Download PDF

Info

Publication number
WO2014058401A2
WO2014058401A2 PCT/TR2013/000308 TR2013000308W WO2014058401A2 WO 2014058401 A2 WO2014058401 A2 WO 2014058401A2 TR 2013000308 W TR2013000308 W TR 2013000308W WO 2014058401 A2 WO2014058401 A2 WO 2014058401A2
Authority
WO
WIPO (PCT)
Prior art keywords
legs
support part
seat
intermediate support
binding groove
Prior art date
Application number
PCT/TR2013/000308
Other languages
English (en)
Other versions
WO2014058401A3 (fr
Inventor
Aykut GÜNER
Uğur AKBABA
Serkan KADAŞ
Mehmet Ali GÜZEL
Original Assignee
Assan Hani̇l Otomoti̇v Sanayi̇ Ve Ti̇caret Anoni̇m Şi̇rketi̇
Uçak Koltuk Üreti̇mi̇ Sanayi̇ Ve Ti̇caret Anoni̇m Şi̇rketi̇
United Engineering Sp. Z O. O.
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 Assan Hani̇l Otomoti̇v Sanayi̇ Ve Ti̇caret Anoni̇m Şi̇rketi̇, Uçak Koltuk Üreti̇mi̇ Sanayi̇ Ve Ti̇caret Anoni̇m Şi̇rketi̇, United Engineering Sp. Z O. O. filed Critical Assan Hani̇l Otomoti̇v Sanayi̇ Ve Ti̇caret Anoni̇m Şi̇rketi̇
Publication of WO2014058401A2 publication Critical patent/WO2014058401A2/fr
Publication of WO2014058401A3 publication Critical patent/WO2014058401A3/fr

Links

Classifications

    • 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
    • B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • B64D11/0696—Means for fastening seats to floors, e.g. to floor rails
    • 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
    • B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • 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
    • B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • B64D11/0619—Arrangements of seats, or adaptations or details specially adapted for aircraft seats with energy absorbing means specially adapted for mitigating impact loads for passenger seats, e.g. at a crash

Definitions

  • the invention relates to a structural improvement applied on passenger seats in airplanes used in air transportation.
  • the invention particularly relates to an intermediate support part that connects seat binding grooves on the airframe with the seat frame, and connects legs to each other by getting fixed between the parts called as seat legs, and does the force transmission and force damping task along with this connection.
  • passenger seats are used in airplanes for providing a comfortable flight in air transportation.
  • Parts named as seat legs are used for connecting the seat binding grooves on the airframe with the seat frame.
  • the utility model application numbered 2009/06211 that is registered in the TPE record discloses a driver seat comprising a backrest and sitting sheets on which resistance enhancing gaps have been formed.
  • the European Patent Application numbered EP1274601 B1 relates to a seat upholstery made of leather for vehicle and airplane seats.
  • the present invention particularly relates to an intermediate support part that connects seat binding grooves on the airframe with the seat frame, and connects legs to each other by getting fixed between the parts called as seat legs, and does the force transmission and force damping task along with this connection, which all in all meets the above-mentioned requirements, removes all the disadvantages and brings some additional advantages.
  • both front and rear legs are connected to each other and the force to be exposed on the seat legs is transferred to other leg, and in addition to this allows functioning as an arch by way the bevel of its geometry.
  • some of the force exposed on the seat is damped and overall strength of the seat is improved.
  • it is required to enlarge structural section or increase wall thickness for enhancing the strength of the seat. Since the weight of the seat is of vital importance, this solution means improving the strength of the seat without increasing its weight.
  • a part that only provides a connection in terms of form is now converted into a functional part.
  • the intermediate support part that is attached between front and rear legs has an arch-like form.
  • Figure 1 is the assembled perspective view of the intermediate support part that connects the seat legs in terms of form and function.
  • the invention relates to an intermediate support part (3) that connects seat binding grooves on the airframe with the seat frame, and connects legs to each other by getting fixed between the parts called as seat legs (1 , 2), and does the force transmission and force damping task along with this connection between the legs (1 , 2).
  • the front leg (1) takes the task of connecting the front part of the seat framing to the groove on the airframe.
  • the rear leg (2) takes the task of connecting the rear part of the seat framing to the groove on the airframe.
  • the top of the binding groove on the airframe is covered by a binding groove cover sheet (4) and it is prevented that nothing enters into the groove.
  • the front leg (1) is connected to the binding groove via a front leg binding groove adapter (5).
  • the rear leg (2) is connected to the binding groove via a rear leg binding groove adapter (6).
  • the front leg (1), rear leg (2), binding groove cover sheet (4), front and rear leg binding groove adapters (5, 6) are the parts already used in the present art.
  • the intermediate support part (3) according to the invention both connects the front and rear leg (1 , 2) in terms of form and provides the transmission of force arising vertically or horizontally, and also takes the task of force damping. In 9g or 14g tests of airplane seats, an inertial force occurs due to the weight of the passenger and seat. Said force causes horizontal and vertical forces to occur on seat legs (1 , 2). As the vertical force occurring on the rear leg (2) is very strong, it strains the intermediate support part (3) to bend horizontally. Due to bending moment, the intermediate support part (3) makes deformation on vertical direction.
  • the intermediate support part (3) Due to its geometry and connection points, the intermediate support part (3) has its role in the design that acts against the exposed force on itself.
  • the intermediate support part (3) comprises an arch-like curvilinear structure, and does the task of transmitting and also damping the forces exposed thereon. Differing from present art, it provides functionality along with the connection between front and rear legs (1 , 2) in terms of form.
  • the section of the intermediate support part (3) can be replaced and so a lightening or an increase in the strength can be provided.
  • the leg connection points can be changed and its position can be optimized.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Seats For Vehicles (AREA)

Abstract

L'invention concerne une partie de support intermédiaire (3), qui relie des rainures de liaison de siège, situées sur le cadre, au cadre de siège et relie les pieds l'un à l'autre en les fixant entre les parties appelées pieds de siège (1, 2), et applique la fonction de transmission de force et d'amortissement de force avec ce raccordement entre les pieds (1, 2).
PCT/TR2013/000308 2012-10-08 2013-10-08 Partie de support intermédiaire fonctionnelle utilisée parmi les pieds de sièges de passager dans des avions WO2014058401A2 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
TR201211494 2012-10-08
TR2012/11494 2012-10-08

Publications (2)

Publication Number Publication Date
WO2014058401A2 true WO2014058401A2 (fr) 2014-04-17
WO2014058401A3 WO2014058401A3 (fr) 2014-08-28

Family

ID=49759523

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/TR2013/000308 WO2014058401A2 (fr) 2012-10-08 2013-10-08 Partie de support intermédiaire fonctionnelle utilisée parmi les pieds de sièges de passager dans des avions

Country Status (1)

Country Link
WO (1) WO2014058401A2 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3396196A1 (fr) * 2017-04-28 2018-10-31 Airbus Helicopters Mécanisme de filtrage des vibrations destiné à être agencé entre un équipement et un fuselage d'aeronef, siège equipé d'un tel mécanisme
EP4382423A1 (fr) * 2022-12-06 2024-06-12 Safran Seats USA LLC Ensemble de jambe décalée pour sièges passagers d'aéronef

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1274601B1 (fr) 2000-04-18 2005-04-13 Ernst Biermann Revetement de siege pour sieges de vehicule et d'avion de tous types
TR200906211U (tr) 2009-08-11 2009-12-21 Akkomsan Otomoti̇v Yedek Parça İmalati İnşaat Petrol Ürünleri̇ Sanayi̇ Ve Ti̇caret Li̇mi̇ted Şi̇rketi̇ Üzerinde mukavemet arttırıcı boşluklar oluşturulmuş sırtlık ve oturak saclarına haiz bir sürücü koltuğu.

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2409316A (en) * 1942-10-12 1946-10-15 Douglas Aircraft Co Inc Removable and collapsible seating fixture
FR2671838B1 (fr) * 1991-01-22 1995-01-13 Sicma Aero Seat Dispositif d'absorption d'energie, structure formant pietement pour siege d'appareil de transport aerien comportant un tel dispositif, et siege comportant une telle structure.
FR2769191B1 (fr) * 1997-10-03 2000-02-25 Simair Pied de siege et siege d'aeronef incorporant un tel pied
JP5165592B2 (ja) * 2006-01-30 2013-03-21 ビー イー エアロスペイス，インク． 振動防止式軌道固定具
US7785053B2 (en) * 2006-03-31 2010-08-31 The Boeing Company Single tough locking seat fittings and methods

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1274601B1 (fr) 2000-04-18 2005-04-13 Ernst Biermann Revetement de siege pour sieges de vehicule et d'avion de tous types
TR200906211U (tr) 2009-08-11 2009-12-21 Akkomsan Otomoti̇v Yedek Parça İmalati İnşaat Petrol Ürünleri̇ Sanayi̇ Ve Ti̇caret Li̇mi̇ted Şi̇rketi̇ Üzerinde mukavemet arttırıcı boşluklar oluşturulmuş sırtlık ve oturak saclarına haiz bir sürücü koltuğu.

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3396196A1 (fr) * 2017-04-28 2018-10-31 Airbus Helicopters Mécanisme de filtrage des vibrations destiné à être agencé entre un équipement et un fuselage d'aeronef, siège equipé d'un tel mécanisme
FR3065771A1 (fr) * 2017-04-28 2018-11-02 Airbus Helicopters Mecanisme de filtrage des vibrations destine a etre agence entre un equipement et un fuselage d'aeronef, siege equipe d'un tel mecanisme
US10787264B2 (en) 2017-04-28 2020-09-29 Airbus Helicopters Vibration filter mechanism for arranging between a piece of equipment and an aircraft fuselage, and a seat fitted with such a mechanism
EP4382423A1 (fr) * 2022-12-06 2024-06-12 Safran Seats USA LLC Ensemble de jambe décalée pour sièges passagers d'aéronef

Also Published As

Publication number Publication date
WO2014058401A3 (fr) 2014-08-28

Similar Documents

Publication Publication Date Title
EP3010376B1 (fr) Siège compact d'équipage de cabine
US9604725B2 (en) Aircraft seat with a single-beam structure and aircraft comprising such a seat
JP6297472B2 (ja) 乗物用シート
WO2012086803A1 (fr) Siège de véhicule
JP6133146B2 (ja) 乗物用シート
JP5799838B2 (ja) 車両用シートクッションフレーム
JP6130327B2 (ja) 航空機の乗客用シート
JP2016013824A (ja) 車両用シート
JP5669567B2 (ja) 乗物用シート
CN105291923A (zh) 椅背框架和用于在椅背框架中使用的树脂
JP5915603B2 (ja) シートバックフレーム構造
WO2014058401A2 (fr) Partie de support intermédiaire fonctionnelle utilisée parmi les pieds de sièges de passager dans des avions
CN105459857A (zh) 集成三点式安全带的单边调角器座椅骨架
CN201729084U (zh) 可调式防乘客下潜机构
EP2769916B1 (fr) Dispositif d'absorption d'énergie de siège d'aéronef pour retenue d'occupant
US9150128B2 (en) Vehicle seat cushion frame
JP2018199362A (ja) 乗物用シート
JP2018131159A (ja) 乗物シート用クッションフレーム
WO2011088999A3 (fr) Dispositif de siège
JP5989856B2 (ja) 乗物用シート
CN203902695U (zh) 一种防后排乘员前碰撞下潜结构
CN204055472U (zh) 卷缩器放置侧边的座椅骨架
JP2020111286A (ja) クッションフレーム
JP6004185B2 (ja) 車両用シート構造
JP5629204B2 (ja) 乗物用シート

Legal Events

Date Code Title Description
122 Ep: pct application non-entry in european phase

Ref document number: 13845377

Country of ref document: EP

Kind code of ref document: A2