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WO1993001088A1 - Cloison de separation pour cabine d'avion - Google Patents

Cloison de separation pour cabine d'avion Download PDF

Info

Publication number
WO1993001088A1
WO1993001088A1 PCT/GB1992/001228 GB9201228W WO9301088A1 WO 1993001088 A1 WO1993001088 A1 WO 1993001088A1 GB 9201228 W GB9201228 W GB 9201228W WO 9301088 A1 WO9301088 A1 WO 9301088A1
Authority
WO
WIPO (PCT)
Prior art keywords
panel section
divider
cabin
rod
panel
Prior art date
Application number
PCT/GB1992/001228
Other languages
English (en)
Inventor
Leslie James Simpson
Brian Sydney Bayliss
Original Assignee
Magerik Limited
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 Magerik Limited filed Critical Magerik Limited
Publication of WO1993001088A1 publication Critical patent/WO1993001088A1/fr
Priority to GB9400180A priority Critical patent/GB2273088A/en

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
    • B64D11/0023—Movable or removable cabin dividers, e.g. for class separation

Definitions

  • the present invention relates to aircraft cabin dividers primarily for dividing an aircraft cabin into sections catering for different classes of passenger seating.
  • Fixed dividers or bulkheads used to divide an aircraft cabin as between business and tourist class cabin areas respectively are traditionally in the form of vertical partitions anchored to the floor tracks of the cabin or between the floor tracks and some form of mounting means on the ceiling of the cabin.
  • the position of the seat aft of the cabin divider is critical as regards the need to meet certain safety regulations relating to the minimum amount of head damage permissible under dynamic testing procedures, ie HIC (Head Injury Criteria).
  • a collapsible aircraft cabin divider comprising a series of pivotally interconnected divider panel sections, ceiling mounting means for mounting an upper one of the panel sections to the ceiling of an aircraft cabin, floor mounting means for mounting a lower one of the panel sections to the floor of the cabin, an intermediate one of the panel sections being arranged with respect to the others such mat in the installed position of the divider it lies inclined to the vertical to allow the back of a passenger seat placed forward of the divider to move to a maximum recline position, and stress-critical means for forming the pivotal interconnection between at least two of the panel sections whereby under applied forces above a predetermined level the panel sections are allowed to pivot one with respect to the other and said one panel section to move to a collapsed position as it follows the movement of the back of said passenger seat placed forward of the divider.
  • the critical pan of the cabin divider is removed out of the path of travel of the descending head of a passenger strapped in the seat aft of the divider such that the position of that seat (and also the forward seat) can be arranged closer to the divider than would otherwise be possible if the divider were of the traditional fixed vertical variety.
  • the upper panel section is formed of two sub-panel sections pivotally connected to one another, with the stress-critical means in the form of a stress-critical expandable hinge between the lower one of the sub-panel sections and the inclined panel section to allow the latter to move away from the former during its movement to me collapsed position.
  • the stress-critical means in the form of a stress-critical expandable hinge between the lower one of the sub-panel sections and the inclined panel section to allow the latter to move away from the former during its movement to me collapsed position.
  • Fig 1 is a side view of an aircraft cabin illustrating a fixed vertical aircraft cabin divider according to the prior art
  • Fig 2 is a side view of an aircraft cabin divider according to an embodiment of the invention in a pre-impact position between aft and forward located passenger seats;
  • Fig 3 is a side view of the aircraft cabin divider of Fig 2 as in an impact position in relation to the aft and forward positioned passenger seats;
  • Fig 4 is a side and rear view of an aircraft cabin divider according to an another embodiment of the invention.
  • Fig 5 is a detail at location A in Fig 4 of the hinge connection between the upper and intermediate panel sections of the divider and illustrates the movement of the divider around that hinge connection in the event of crash impact.
  • a vertically mounted bulk head or cabin divider 1 according to the prior art is shown installed between the floor 2 and ceiling 3 of an aircraft cabin generally designated 4.
  • dividers of this type are introduced to separate business and tourist class areas of an aircraft cabin.
  • ⁇ ie position of a passenger seat 5 located aft of the cabin divider 1 as shown in Fig 1 is critical in relation to die injury which the head of a passenger P will sustain in a crash bv collision of his or her head H with the divider 1.
  • the passenger is shown belted to the seat in two positions, an upright position 6 corresponding to that adopted during take-off and landing and a maximum forward position 7 as would be sustained by the upper part of the body 8 being projected forward in the event of a sudden interruption in forward momentum of the aircraft occurring in a crash.
  • the position of the aft seat 5 has to be such that the head H of the passenger P in the maximum forward bent position 6 of the body as shown in Fig i. does not collide heavily with the vertical divider 1.
  • the invention provides an energy absorbing bulk head divider 9 as shown installed in an aircraft cabin in Figs 2 and 3.
  • the divider 9 comprises four transversely interconnected panel sections. 10. 11. 12. 13, the upper one 10 of which is pivotally mounted at M to the cabin ceiling 3 as shown, and is formed of two relatively slidable parts 10' and 10".
  • the bottom section 13 extends vertically between the seat base 14 and the floor 2 of the cabin to which it may be permanently affixed or movable on the cabin seat floor tracks (not shown).
  • ⁇ ie upper and lower panel sections 10 and 13 are offset with respect to one another, and are joined by two middle panel sections 11, 12 generally extending between d e seat base 14 and the top of the back 15 of the passenger seat 16 positioned forward of the divider 9 as shown.
  • the panel section 12 specifically extends over the end E of the arm rest 17 to the seat back 15. It will be fully appreciated that the width and configuration of the panel sections 11, 12 may be chosen to match the dimensions of any particular aircraft seat and to ensure that they maintain contact with the back parts of the seat during its forwardly propelled movement.
  • the panel section 11 is itself configured to the shape of the seat back 15 in the example shown so that the seat back 15 is able to rest snugly against the panel sec ⁇ on 1 1 in its maximum recline position as shown in dotted outline in Fig 2. It follows that the seat 16 may be positioned closer to the divider of the invention than to those dividers of the prior art.
  • panel sec ⁇ on may be padded (not shown ) in the head contact area.
  • Stress-c ⁇ ticai hinges 18 are positioned between the panel sections 10. 11. 12. 13 and the panel sec ⁇ on 10 mounting means M.
  • the stress-critical hinges 18 are designed to fail above a predetermined impact load so that to all intents and purposes in normal conditions, the partition 9 presents a rigid structure between the aft and forward passenger seats 16 and 19.
  • the partition or divider 9 Upon the occurrence of a crash, for example, the partition or divider 9 will deform or collapse as shown in Fig 3.
  • the panel sections 11 and 12 will deform around and follow the movement of the seat back 15 of the passenger seat 16 forward of the divider 9 during which the upper panel section 10 will expand and tilt or pivot around its ceiling mounting M.
  • the panel section 11 which would otherwise obstruct forward movement of the head H of the passenger seat 19 as shown in Fig 3, will move forward out of the way of the path of travel of head H under the crash impact.
  • the aircraft cabin divider shown in Fig 4 has upper and lower normally vertically disposed panel sections 20 and 21 and a straight intermediate panel section 22 in contrast to the two-part intermediate panel sections 11 and 12 shown in Figs 2 and 3.
  • the cabin divider is shown in its normally installed position in a 747 Jumbo Jet and is designed to collapse in the direction of the arrow F under crash impact conditions.
  • the upper panel section 20 is formed of two pivotally interconnected sub-panel sections 20' and 20", the sub-panel section 20' being held to the ceiling of the aircraft by means of locating pins 23.
  • the lower panel section 21 is held to the floor of the aircraft cabin by angled fixings 21'.
  • the hinge includes an expandable mechanism is in the form of a rod 24 pivotally mounted to the panel section 22 and being slidably mounted in a housing 25 attached to the sub-panel section 20" by bolts 26.
  • the rod 24 is retained within the housing 25 by means of a spring loaded pivotal locking lever or pawl 27 held, against the spring urging, by 'an inertia pin 28 in a recess 29 formed in the rod 24. With the rod 24 in the fully retracted position shown in Fig 5, the divider is held stable and effectively rigid in the normally installed position.
  • a similar friction hinge 23' to the hinge 23 is installed at the interconnection between the intermediate panel section 22 and the lower panel section 21, see particularly Fig 6. the hinge 23' is mounted within and along the lower edge of the intermediate panel section 22 as shown.
  • the hinge 23' is comprised of similar component parts to me hinge23 but in this case the rod 24 of hinge 23' is held by the pawl 27 in a partially retracted position with respect to its housing 25 so that a gap E is formed between the panel sections 22 and 21 thereby to allow for downward movement of the panel section 22 as the inertia pins 28 are released in both the hinges 23 and 23' during crash impact.
  • the pivot point of the friction hinge 23 moves from position Vj shown in Figs 5 and 6 through a lower position V2 with respect to an arc of a circle C described around the pivot point V4 of the panel section 22 to the lower panel section 21, to position V3 on that arc.
  • the rod 24 of the hinge 23 sliding out of the housing 25 to its fully retracted position and the rod 24 of the hinge 23' moving into its housing 25 so that the intermediate panel section 22 is able to move freely to its fully forward collapsed position as shown.
  • cabin dividers means that the space occupied by the aft and forward passenger seats to either side of the divider may be kept to a minimum in full compliance with relevant safetv regulations.

Landscapes

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

Abstract

L'invention concerne une cloison de séparation (9) pour cabine d'avion formée de panneaux (10, 11, 12, 13) assemblés de façon qu'ils puissent pivoter, ladite cloison se montant entre deux rangées de sièges de passager. Un panneau supérieur (10) se fixe au plafond d'une cabine d'avion et un panneau inférieur (12) se fixe au plancher de la cabine. Les panneaux supérieur et inférieur sont montés pivotants sur un panneau intermédiaire, lequel, en position normale, fait face aux passagers assis sur les sièges de la rangée arrière, d'un côté de la cloison de séparation. Au moins une des liaisons pivotantes présente un point de contrainte critique, ce qui confère à la structure, en position normale, une rigidité, cela de sorte que, en cas de crash, le panneau intermédiaire puisse suivre le mouvement des dossiers des sièges de la rangée avant, afin que les têtes des passagers de la rangée arrière ne heurtent pas le panneau intermédiaire de la cloison de séparation et ne se blessent pas. Pour donner au panneau intermédiaire plus de liberté dans son mouvement vers l'avant, la liaison présentant un point de contrainte critique, de préférence entre le panneau intermédiaire et le panneau supérieur, comprend une articulation (18) à friction, extensible, permettant au panneau intermédiaire de s'éloigner du panneau supérieur vers une position de fermeture maximum déterminée par l'extension de l'articulation.
PCT/GB1992/001228 1991-07-06 1992-07-06 Cloison de separation pour cabine d'avion WO1993001088A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9400180A GB2273088A (en) 1991-07-06 1994-01-06 Aircraft cabin divider

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB9114626.6 1991-07-06
GB919114626A GB9114626D0 (en) 1991-07-06 1991-07-06 Aircraft cabin divider

Publications (1)

Publication Number Publication Date
WO1993001088A1 true WO1993001088A1 (fr) 1993-01-21

Family

ID=10697931

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/GB1992/001228 WO1993001088A1 (fr) 1991-07-06 1992-07-06 Cloison de separation pour cabine d'avion

Country Status (3)

Country Link
AU (1) AU2231292A (fr)
GB (2) GB9114626D0 (fr)
WO (1) WO1993001088A1 (fr)

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0708018A1 (fr) 1994-10-18 1996-04-24 DaimlerChrysler Aerospace Airbus Gesellschaft mit beschränkter Haftung Cloison mobile pour la cabine d'un avion de passager
EP0847917A1 (fr) * 1996-12-16 1998-06-17 The Boeing Company Siège comportant un dispositif pour réduire un impact de la tête
EP1698552A1 (fr) 2005-03-03 2006-09-06 Airbus Deutschland GmbH Disposition d'un premier et d'un deuxième élément
WO2010084048A1 (fr) * 2009-01-23 2010-07-29 Airbus Operations Gmbh Protection visuelle pour cabine passagers
JP2011511739A (ja) * 2008-02-11 2011-04-14 ビーイー・エアロスペース・インコーポレーテッド 航空機客室用クラス仕切り
DE102012021430A1 (de) * 2012-10-30 2014-04-30 Airbus Operations Gmbh Vorrichtung zur Trennung zweier Zonen einer Passagierkabine
JP2015527240A (ja) * 2012-07-11 2015-09-17 ビーイー・エアロスペース・インコーポレーテッドＢ／Ｅ Ａｅｒｏｓｐａｃｅ， Ｉｎｃ． 座席クラスを分割する乗客席のバルクヘッド
WO2016004096A3 (fr) * 2014-06-30 2016-02-18 C&D Zodiac, Inc. Ensemble panneau avec section d'écrasement
EP3219601A1 (fr) * 2016-03-18 2017-09-20 The Boeing Company Système de panneau de jeu déployable, procédé et ensemble pour une boîte de raccordement au solà l'intérieur d'une cabine d'un aéronef
EP3219555A1 (fr) * 2016-03-15 2017-09-20 Airbus Operations GmbH Module de paroi de séparation d'une cabine de véhicule pour une séparation mécanique et optique de différentes zones de cabine
WO2017176298A1 (fr) * 2016-04-04 2017-10-12 B/E Aerospace, Inc. Séparateur de classe profilé
WO2018187334A1 (fr) * 2017-04-04 2018-10-11 B/E Aerospace, Inc. Séparateur de classe profilé
WO2019068028A1 (fr) * 2017-09-29 2019-04-04 B/E Aerospace, Inc. Séparateur de classe profilé
CN110049922A (zh) * 2016-10-12 2019-07-23 Be航天公司 波形舱位分隔器
CN110481797A (zh) * 2019-08-20 2019-11-22 湖北航宇嘉泰飞机设备有限公司 一种飞机隔板碰撞吸能装置
US10676194B2 (en) 2016-04-04 2020-06-09 B/E Aerospace, Inc. Contoured class divider
US10843799B2 (en) 2016-04-04 2020-11-24 B/E Aerospace, Inc. Contoured class divider
US11066171B2 (en) 2016-04-04 2021-07-20 B/E Aerospace, Inc. Contoured class divider
JP2022126940A (ja) * 2021-02-19 2022-08-31 株式会社豊田自動織機 車室仕切装置
EP4292931A1 (fr) * 2022-06-17 2023-12-20 B/E Aerospace, Inc. Cloison de séparation de zone mobile

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US10230257B1 (en) 2017-09-12 2019-03-12 Video Gaming Technologies, Inc. Electronic gaming machine including a wireless charging apparatus
US11847885B2 (en) 2018-10-05 2023-12-19 Aristocrt Technologies Australia Pty Limited System and method for cashless exchange at smart tables
US11972659B2 (en) 2018-10-05 2024-04-30 Aristocrat Technologies, Inc. System and method for changing beacon identifiers for secure mobile communications
AU2019240623A1 (en) 2018-10-05 2020-04-23 Aristocrat Technologies Australia Pty Limited System and method for managing digital wallets
US11132862B2 (en) 2018-10-05 2021-09-28 Aristocrat Technologies Australia Pty Limited System and method for ticketing at a gaming table
WO2020072362A1 (fr) 2018-10-05 2020-04-09 Aristocrat Technologies Australia Pty Limited Système et procédé pour changer des identifiants de balise pour des communications mobiles sécurisées
US11227466B2 (en) 2019-08-30 2022-01-18 Aristocrat Technologies, Inc. Multi-currency digital wallets and gaming architectures
US11544994B2 (en) 2020-03-27 2023-01-03 Aristocrat Technologies, Inc. Beacon to patron communications for electronic gaming devices
US11276271B2 (en) 2020-04-03 2022-03-15 Aristocrat Technologies, Inc. Systems and methods for securely connecting an electronic gaming machine to an end user device
US12208171B2 (en) 2020-04-30 2025-01-28 Aristocrat Technologies, Inc. Ultraviolet disinfection and sanitizing systems and methods for electronic gaming devices and other gaming equipment
USD968513S1 (en) 2020-05-15 2022-11-01 Aristocrat Technologies, Inc. (ATI) Gaming machine divider

Citations (4)

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Publication number Priority date Publication date Assignee Title
FR2458461A1 (fr) * 1979-06-12 1981-01-02 Carnieres Pol De Cloison mobile pour separation de classes dans des avions commerciaux
US4597549A (en) * 1984-09-28 1986-07-01 Falcon Jet Corporation Aircraft mid-cabin divider
EP0361717A1 (fr) * 1988-09-08 1990-04-04 Magerik Ltd Séparateur pour cabine d'avion
DE3917206C1 (en) * 1989-05-26 1990-05-17 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De Safety fire trap partition system for aircraft - has composite folding door in region above through aperture, pivoting about horizontal axis

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2458461A1 (fr) * 1979-06-12 1981-01-02 Carnieres Pol De Cloison mobile pour separation de classes dans des avions commerciaux
US4597549A (en) * 1984-09-28 1986-07-01 Falcon Jet Corporation Aircraft mid-cabin divider
EP0361717A1 (fr) * 1988-09-08 1990-04-04 Magerik Ltd Séparateur pour cabine d'avion
DE3917206C1 (en) * 1989-05-26 1990-05-17 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De Safety fire trap partition system for aircraft - has composite folding door in region above through aperture, pivoting about horizontal axis

Cited By (46)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0708018A1 (fr) 1994-10-18 1996-04-24 DaimlerChrysler Aerospace Airbus Gesellschaft mit beschränkter Haftung Cloison mobile pour la cabine d'un avion de passager
DE4437133A1 (de) * 1994-10-18 1996-04-25 Daimler Benz Aerospace Airbus Trennwand für die Kabine eines Passagierflugzeuges
US5577358A (en) * 1994-10-18 1996-11-26 Daimler-Benz Aerospace Airbus Gmbh Separation wall for dividing a cabin in a passenger aircraft
EP0847917A1 (fr) * 1996-12-16 1998-06-17 The Boeing Company Siège comportant un dispositif pour réduire un impact de la tête
US7905451B2 (en) 2005-03-03 2011-03-15 Airbus Deutschland Gmbh Arrangement of a first and a second furnishing
EP1698552A1 (fr) 2005-03-03 2006-09-06 Airbus Deutschland GmbH Disposition d'un premier et d'un deuxième élément
US8297554B2 (en) 2005-03-03 2012-10-30 Airbus Operations Gmbh Arrangement of a first and a second furnishing
JP2011511739A (ja) * 2008-02-11 2011-04-14 ビーイー・エアロスペース・インコーポレーテッド 航空機客室用クラス仕切り
EP2240367A4 (fr) * 2008-02-11 2013-08-21 Be Aerospace Inc Séparation de classe pour cabine d'avion
WO2010084048A1 (fr) * 2009-01-23 2010-07-29 Airbus Operations Gmbh Protection visuelle pour cabine passagers
US9027880B2 (en) 2009-01-23 2015-05-12 Airbus Operations Gmbh Screen for a passenger cabin
JP2015527240A (ja) * 2012-07-11 2015-09-17 ビーイー・エアロスペース・インコーポレーテッドＢ／Ｅ Ａｅｒｏｓｐａｃｅ， Ｉｎｃ． 座席クラスを分割する乗客席のバルクヘッド
DE102012021430A1 (de) * 2012-10-30 2014-04-30 Airbus Operations Gmbh Vorrichtung zur Trennung zweier Zonen einer Passagierkabine
DE102012021430B4 (de) 2012-10-30 2023-01-12 Airbus Operations Gmbh Vorrichtung zur Trennung zweier Zonen einer Passagierkabine
US9550572B2 (en) 2012-10-30 2017-01-24 Airbus Operations Gmbh Device for separating two zones of a passenger cabin
US10059423B2 (en) 2014-06-30 2018-08-28 Zodiac Seats Us Llc Panel assembly with crush section
WO2016004096A3 (fr) * 2014-06-30 2016-02-18 C&D Zodiac, Inc. Ensemble panneau avec section d'écrasement
JP2017521307A (ja) * 2014-06-30 2017-08-03 ゾディアック シーツ ユーエス エルエルシィ クラッシュセクションを有するパネル組立体
EP3219555A1 (fr) * 2016-03-15 2017-09-20 Airbus Operations GmbH Module de paroi de séparation d'une cabine de véhicule pour une séparation mécanique et optique de différentes zones de cabine
DE102016104794A1 (de) * 2016-03-15 2017-09-21 Airbus Operations Gmbh Trennwandmodul für eine Kabine eines Fahrzeugs zur optischen und mechanischen Abtrennung unterschiedlicher Kabinenbereiche
US10836491B2 (en) 2016-03-15 2020-11-17 Airbus Operations Gmbh Partition wall module for a cabin of a vehicle for an optical and mechanical separation of different cabin regions
CN107200132A (zh) * 2016-03-18 2017-09-26 波音公司 飞行器内舱内隔间的可展开的净空面板系统、方法及组件
JP2017171278A (ja) * 2016-03-18 2017-09-28 ザ・ボーイング・カンパニーＴｈｅ Ｂｏｅｉｎｇ Ｃｏｍｐａｎｙ 航空機の内部客室内のモニュメント用の展開可能な隙間パネルシステム、方法および組立体
CN107200132B (zh) * 2016-03-18 2021-12-03 波音公司 飞行器内舱内隔间的可展开的净空面板系统、方法及组件
EP3219601A1 (fr) * 2016-03-18 2017-09-20 The Boeing Company Système de panneau de jeu déployable, procédé et ensemble pour une boîte de raccordement au solà l'intérieur d'une cabine d'un aéronef
US10112719B2 (en) 2016-03-18 2018-10-30 The Boeing Company Deployable clearance panel system, method, and assembly for a monument within an internal cabin of an aircraft
US11787544B2 (en) 2016-04-04 2023-10-17 B/E Aerospace, Inc. Contour class divider
US10370106B2 (en) * 2016-04-04 2019-08-06 B/E Aerospace, Inc. Contoured class divider
CN109071022B (zh) * 2016-04-04 2022-06-03 B/E航空公司 波状外形舱分隔器
US10676194B2 (en) 2016-04-04 2020-06-09 B/E Aerospace, Inc. Contoured class divider
CN109071022A (zh) * 2016-04-04 2018-12-21 B/E航空公司 波状外形舱分隔器
US10843799B2 (en) 2016-04-04 2020-11-24 B/E Aerospace, Inc. Contoured class divider
US11066171B2 (en) 2016-04-04 2021-07-20 B/E Aerospace, Inc. Contoured class divider
WO2017176298A1 (fr) * 2016-04-04 2017-10-12 B/E Aerospace, Inc. Séparateur de classe profilé
CN110049922A (zh) * 2016-10-12 2019-07-23 Be航天公司 波形舱位分隔器
EP3939886A1 (fr) * 2016-10-12 2022-01-19 B/E Aerospace Inc. Séparateur de classe profilé
EP3526120B1 (fr) * 2016-10-12 2021-12-01 B/E Aerospace, Inc. Séparateur de classe profilé
WO2018187334A1 (fr) * 2017-04-04 2018-10-11 B/E Aerospace, Inc. Séparateur de classe profilé
CN111212786A (zh) * 2017-09-29 2020-05-29 Be航天公司 波形舱位分隔器
EP4194337A1 (fr) * 2017-09-29 2023-06-14 B/E Aerospace, Inc. Diviseur de classe profilé
WO2019068028A1 (fr) * 2017-09-29 2019-04-04 B/E Aerospace, Inc. Séparateur de classe profilé
CN111212786B (zh) * 2017-09-29 2024-04-19 Be航天公司 波形舱位分隔器
CN110481797A (zh) * 2019-08-20 2019-11-22 湖北航宇嘉泰飞机设备有限公司 一种飞机隔板碰撞吸能装置
JP2022126940A (ja) * 2021-02-19 2022-08-31 株式会社豊田自動織機 車室仕切装置
EP4292931A1 (fr) * 2022-06-17 2023-12-20 B/E Aerospace, Inc. Cloison de séparation de zone mobile
US12103686B2 (en) 2022-06-17 2024-10-01 B/E Aerospace, Inc. Movable area partition

Also Published As

Publication number Publication date
GB2273088A (en) 1994-06-08
GB9400180D0 (en) 1994-03-16
AU2231292A (en) 1993-02-11
GB9114626D0 (en) 1991-08-21

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