DE3311053A1 - SEAT FOR A VEHICLE, IN PARTICULAR A PLANE - Google Patents

SEAT FOR A VEHICLE, IN PARTICULAR A PLANE

Info

Publication number
DE3311053A1
DE3311053A1 DE19833311053 DE3311053A DE3311053A1 DE 3311053 A1 DE3311053 A1 DE 3311053A1 DE 19833311053 DE19833311053 DE 19833311053 DE 3311053 A DE3311053 A DE 3311053A DE 3311053 A1 DE3311053 A1 DE 3311053A1
Authority
DE
Germany
Prior art keywords
polysiloxane
flame
retardant
layer
seat
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Withdrawn
Application number
DE19833311053
Other languages
German (de)
Inventor
Vojtech Ing. Demovic (grad.), 7000 Stuttgart
Manfred Ing.(grad.) 8998 Lindenberg Gruber
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.)
Keiper Recaro GmbH and Co
Metzeler Kautschuk AG
Original Assignee
Keiper Recaro GmbH and Co
Metzeler Kautschuk AG
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 Keiper Recaro GmbH and Co, Metzeler Kautschuk AG filed Critical Keiper Recaro GmbH and Co
Priority to DE19833311053 priority Critical patent/DE3311053A1/en
Priority to GB08406276A priority patent/GB2137492A/en
Priority to FR8404371A priority patent/FR2543079A1/en
Publication of DE3311053A1 publication Critical patent/DE3311053A1/en
Withdrawn legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/18Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by features of a layer of foamed material
    • AHUMAN NECESSITIES
    • A47FURNITURE; DOMESTIC ARTICLES OR APPLIANCES; COFFEE MILLS; SPICE MILLS; SUCTION CLEANERS IN GENERAL
    • A47CCHAIRS; SOFAS; BEDS
    • A47C7/00Parts, details, or accessories of chairs or stools
    • A47C7/02Seat parts
    • A47C7/18Seat parts having foamed material included in cushioning part
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/16Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by features of a layer formed of particles, e.g. chips, powder or granules
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/22Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • B32B5/245Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it being a foam layer
    • 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
    • B64D11/00Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/06Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • 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
    • B64D11/00Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/06Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • B64D11/0647Seats characterised by special upholstery or cushioning features
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2264/00Composition or properties of particles which form a particulate layer or are present as additives
    • B32B2264/10Inorganic particles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2266/00Composition of foam
    • B32B2266/02Organic
    • B32B2266/0214Materials belonging to B32B27/00
    • B32B2266/0278Polyurethane
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/30Properties of the layers or laminate having particular thermal properties
    • B32B2307/306Resistant to heat
    • B32B2307/3065Flame resistant or retardant, fire resistant or retardant
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2383/00Polysiloxanes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2605/00Vehicles
    • B32B2605/18Aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Wood Science & Technology (AREA)
  • Laminated Bodies (AREA)
  • Treatments For Attaching Organic Compounds To Fibrous Goods (AREA)
  • Compositions Of Macromolecular Compounds (AREA)
  • Paints Or Removers (AREA)

Description

- 2. - 2.

METZELER KAUTSCHUK GmbH "" München, 25.3.1983METZELER KAUTSCHUK GmbH "" Munich, March 25, 1983

München · Unser Zeichen:MK 253 PMunich · Our reference: MK 253 P

Sitz für ein Fahrzeug, insbesondere ein FlugzeugSeat for a vehicle, especially an airplane

Die Erfindung betrifft einen Sitz für ein Fahrzeug, insbesondere für ein Flugzeug, der im Oberbegriff des Anspruchs 1 angegebenen Gattung.The invention relates to a seat for a vehicle, in particular for an aircraft of the type specified in the preamble of claim 1.

Insbesondere bei der Entwicklung von Flugzeugsitzen werden große Anstrengungen unternommen, um diese Sitze so auszugestalten, daß sich bei einem Brand die Flammen möglichst langsam ausbreiten und dadurch den Insassen des Flugzeugs ausreichende Zeit zur Evakuierung zur Verfügung steht. .In particular in the development of aircraft seats, great efforts are made to make these seats that way to design that in a fire the flames spread as slowly as possible and thereby the occupants the aircraft has sufficient time to evacuate. .

So ist es beispielsweise bekannt, den Schaumstoffkern mit einer zusätzlichen, dünnen Schicht aus einem flammhemmenden Schaumstoff zu umgeben. Die Aufbringung dieser zusätzlichen Schicht auf den Schaumstoffkern bereitet jedoch in der Praxis Probleme; außerdem ist die flammhemmende Wirkung dieses zusätzlichen Schaumstoffes pro Gewichtseinheit relativ gering, d.h., es muß eine relativ dicke, zusätzliche Schaumstoffschicht eingesetzt werden.So it is known, for example, the foam core with an additional, thin layer of a flame retardant Surrounding foam. However, the application of this additional layer to the foam core prepares problems in practice; in addition, the flame-retardant effect of this additional foam is per unit weight relatively small, i.e. a relatively thick, additional foam layer must be used.

Der Erfindung liegt deshalb die Aufgabe zugrunde, einen Sitz für ein Fahrzeug, insbesondere ein Flugzeug, der angegebenen Gattung zu schaffen, bei dem die oben erwähnten Nachteile nicht auftreten.The invention is therefore based on the object To create a seat for a vehicle, in particular an airplane, of the specified type, in which the above-mentioned Disadvantages do not occur.

Insbesondere soll ein Sitz vorgeschlagen werden, bei dem die Aufbringung der zusätzlichen Schicht aus dem flammhemmenden Material keine Probleme bereitet.In particular, a seat is to be proposed in which the application of the additional layer of the flame-retardant Material does not cause any problems.

(MK 261 E 82)(MK 261 E 82)

Dies wird erfindungsgemäß durch die im kennzeichnenden Teil des Anspruchs 1 angegebenen Merkmale erreicht.This is according to the invention by the in the characterizing Part of claim 1 specified features achieved.

Zweckmäßige Ausführungsformen sind in den Unteransprüchen zusammengestellt.Appropriate embodiments are compiled in the subclaims.

Die mit der Erfindung erzielten'Vorteile beruhen insbesondere darauf, daß der Bezug aus dem textlien Material mit einer Schicht aus einem flammwidrigen Polysiloxan versehen ist; dieses Flächenmaterial läßt sich ohne Probleme in den gewünschten Größen und/oder Designs herstellen, wobei das Polysiloxan auf den Bezug aufgestrichen oder aufkalandriert wird. Die dazu erforderlichen Maschinen stehen in den gewünschten Ausmaßen zur Verfügung, so daß hierzu keine aufwendigen Investitionen erforderlich sind.The advantages achieved with the invention are based in particular ensure that the cover made of the textile material is provided with a layer made of a flame-retardant polysiloxane is; this sheet material can be produced in the desired sizes and / or designs without any problems, wherein the polysiloxane is painted or calendered onto the cover. The machines required for this are available in the desired dimensions, so that no costly investments are required for this.

Nach einer bevorzugten Ausführungsform wird das Polysiloxan mit möglichst geringer Dicke aufgebracht, wobei günstige Ergebnisse mit Schichtdicken von 0,3 bis 0,4 mm erreicht wurden.According to a preferred embodiment, the polysiloxane is applied with the smallest possible thickness, which is favorable Results with layer thicknesses of 0.3 to 0.4 mm were achieved.

Untersuchungen haben ergeben, daß entsprechende Flugzeugsitze alle einschlägigen Anforderungen erfüllen und insbesondere die von den amerikanischen Vorschriften vorgeschriebene Evakuierungszeit von 90 sek. ohne Probleme eingehalten werden kann.Investigations have shown that corresponding aircraft seats meet all the relevant requirements and in particular the evacuation time of 90 seconds prescribed by American regulations. adhered to without problems can be.

Nach einer bevorzugten Ausführungsform wird ein Polysiloxan verwendet, wie es in der unter Nummer 0051212 veröffentlichten europäischen Patentanmeldung beschrieben ist. Ein solches Polysiloxan besteht aus einem Diorganopolysiloxan, feinverteilter Kieselsäure und/oder anderen Füllstoffen, feinverteiltem TiO2, Platin, einem Härtungsmittel sowie einer Stickstoffverbindung.According to a preferred embodiment, a polysiloxane is used as it is described in the European patent application published under number 0051212. Such a polysiloxane consists of a diorganopolysiloxane, finely divided silica and / or other fillers, finely divided TiO 2 , platinum, a hardening agent and a nitrogen compound.

Dieses Polysiloxan muß bei Temperaturen von mehr als 600C unter normalem oder Überdruck in einer bestimmten Zeitspanne gehärtet werden/ wodurch man die sogenannte A-Stufe
der Vulkanisation erhält. Anschließend kann eine Nachvulkanisation erfolgen, die 1 . bis 24 Stunden dauert und
zu der B-Stufe der Vulkanisation führt.
This polysiloxane has to be cured at temperatures of more than 60 ° C. under normal or overpressure in a certain period of time / which means what is known as the A stage
the vulcanization. Post-vulcanization can then take place, the 1. takes up to 24 hours and
leads to the B stage of vulcanization.

Beim Aufstreichen des Polysiloxans werden die beiden Aushärtungsstufen nacheinander durchgeführt. Wird das PoIysilocan aufkalandriert, so erfolgt die Vulkanisation zur
Stufe A beim Kalandrieren, dem dann die Vulkanisation zur Stufe B nachgeschaltet wird.
When the polysiloxane is spread on, the two curing stages are carried out one after the other. If the polysilocane is calendered, the vulcanization takes place
Stage A in calendering, which is followed by vulcanization to stage B.

Der als einstückiges Flächengebilde vorliegende Bezug aus dem textlien Material und der aufgebrachten Schicht aus
dem flammwidrigen Polysiloxan wird in der üblichen Weise
auf dem Schaumstoffkern angebracht, so daß die bisher erforderlichen Fertigungs-Schritte für die Aufbringung
The cover made of the textile material and the applied layer, which is present as a one-piece flat structure
the flame retardant polysiloxane is used in the usual way
attached to the foam core, so that the manufacturing steps previously required for the application

einer zusätzlichen Schicht zwischen Schaumstoffkern und
Bezug entfallen können.
an additional layer between the foam core and
Reference can be omitted.

Die Erfindung wird im folgenden anhand eines Ausführungsbeispiels unter Bezugnahme auf die beiliegende, schematisehe Zeichnung näher erläutert, deren einzige Figur imThe invention is described below using an exemplary embodiment with reference to the accompanying schematic Drawing explained in more detail, the only figure in

vergrößerten Maßstab einen Schnitt durch einen Teil eines Flugzeugsitzes zeigt.shows a section through part of an aircraft seat on an enlarged scale.

Der in der Figur dargestellte, allgemein durch das Bezugszeichen 10 angedeutete Flugzeugsitz weist einen Schaumstoff kern 16 auf, der beispielsweise aus einem Polyurethan-Schaum besteht. Bei Bedarf kann dieser Schaumstoffkern 16 durch eine nicht dargestellte Abstützung in der gewünschten Form und Lage gehalten werden.The aircraft seat shown in the figure, indicated generally by the reference numeral 10, has a foam core 16, which consists for example of a polyurethane foam. If necessary, this foam core 16 be held in the desired shape and position by a support, not shown.

Dieser Schaumstoffkern 16, der bereits die Form des Flug-This foam core 16, which already has the shape of the flight

zeugsitzes 10 hatr ist auf seiner Außenfläche mit einem Überzug versehen, der aus einem üblichen Bezug 12 aus einem Textilmaterial und einer fest mit dem überzug 12 verbundenen Schicht 14 aus einem flammwidrigen Polysiloxan besteht.Zeugsitzes 10 has r is provided on its outer surface with a coating which consists of a conventional cover 12 made of a textile material and a layer 14 made of a flame-retardant polysiloxane that is firmly connected to the cover 12.

Die Schicht 14 aus dem flammwidrigen Polysiloxan ist auf die Innenseite des Bezuges 12 aus dem Textilmaterial auf- IQ gestrichen oder aufkalandriert worden, wobei die Vulkanisation des Polysiloxans zur Stufe A und zur Stufe B in zwei aufeinanderfolgenden Schritten abläuft.The layer 14 of the flame-retardant polysiloxane is coated on the inside of the cover 12 from the textile material up IQ or calendered, wherein the vulcanization of the polysiloxane to step A and step B in two successive steps expires.

Die Zusammensetzung des bevorzugt verwendeten Polysiloxans kann der unter der Nummer 0 051 212 veröffentlichten europäischen Patentanmeldung der Bayer AG entnommen werden. Dieses flammwidrige Polysiloxan besteht aus einem Diorganopolysiloxan, feinzerteilter Kieselsäure und/oder anderen Füllstoffen, feinzerteiltem Titandioxids, Platin, einem Härtungsmittel sowie einer Stickstoffverbindung.The composition of the polysiloxane preferably used can be that of the European published under the number 0 051 212 Patent application from Bayer AG. This flame-retardant polysiloxane consists of a diorganopolysiloxane, finely divided silica and / or other fillers, finely divided titanium dioxide, platinum, a curing agent and a nitrogen compound.

Wird das Polysiloxan in der unvulkanisierten Form auf den Bezug aufgestrichen, so müssen die beiden Vulkanisationsschritte zur Stufe A.bzw. B anschließend durchgeführt wer-2g den. Beim Aufkalandrieren des Polysiloxans erfolgt die Vulkanisation zur Stufe A während des Kalandrierens? die Vulkanisation zur Stufe B muß dann in der üblichen Weise nachgeschaltet werden.If the polysiloxane is brushed onto the cover in the unvulcanized form, the two vulcanization steps must be carried out to level A. or B then carried out wer-2g the. When the polysiloxane is calendered, does vulcanization to stage A take place during calendering? the Vulcanization to stage B must then follow in the usual way.

- Leerseite -- blank page -

Claims (4)

METZELER KAUTSCHUK GmbH MK 2 53 P 83METZELER KAUTSCHUK GmbH MK 2 53 P 83 MünchenMunich PatentansprücheClaims (iV)Sitz für ein Fahrzeug, insbesondere ein Flugzeug, a) mit einem gegebenenfalls abgestützten Schaumstoffkern,
b) mit einem Bezug aus einem Textilmaterial auf dem
(iV) Seat for a vehicle, in particular an airplane, a) with a possibly supported foam core,
b) with a cover made of a textile material on the
Schaumstoffkern, und
c) mit einer .Schicht aus einem flammhemmenden Material
Foam core, and
c) with a .Schicht made of a flame-retardant material
zwischen dem Schaustoffkern und dem Bezug, dadurch gekennzeichnet, daß d) die Innenseite des Bezuges (12) aus dem Textilmaterial mit einer Schicht (14) aus einem flammwidrigen Polysiloxan versehen ist.between the foam core and the cover, characterized in that d) the inside of the cover (12) made of the textile material with a layer (14) made of a flame-retardant polysiloxane is provided.
2. Sitz nach Anspruch 1, dadurch gekennzeichnet, daß2. Seat according to claim 1, characterized in that die- Schicht (14) aus dem flammwidrigen Polysiloxan aufgestrichen oder aufkalandriert ist.the layer (14) made of the flame-retardant polysiloxane is painted on or is calendered. 3. Sitz nach einem der Ansprüche 1 oder 2, dadurch gekennzeichnet, daß die Schicht (14) aus dem flammwidrigen Polysiloxan eine Dicke von etwa 0,1 bis 0,6 mm, insbesondere 0,3 bis 0,4 mm, hat.3. Seat according to one of claims 1 or 2, characterized in that that the layer (14) made of the flame-retardant polysiloxane has a thickness of about 0.1 to 0.6 mm, in particular 0.3 to 0.4 mm. 4. Sitz nach einem der Ansprüche 1 bis 3, dadurch gekennzeichnet, daß das flammwidrige Polysiloxan aus einem Diorgano-Polysiloxan, feinverteilter Kieselsäure, feinverteiltem Titandioxid und einer Stickstoffverbindung besteht.4. Seat according to one of claims 1 to 3, characterized in that the flame-retardant polysiloxane consists of a diorgano-polysiloxane, finely divided silica, finely divided titanium dioxide and a nitrogen compound consists.
DE19833311053 1983-03-25 1983-03-25 SEAT FOR A VEHICLE, IN PARTICULAR A PLANE Withdrawn DE3311053A1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
DE19833311053 DE3311053A1 (en) 1983-03-25 1983-03-25 SEAT FOR A VEHICLE, IN PARTICULAR A PLANE
GB08406276A GB2137492A (en) 1983-03-25 1984-03-09 A seat for a vehicle in particular for an aircraft
FR8404371A FR2543079A1 (en) 1983-03-25 1984-03-21 SEAT FOR VEHICLE, IN PARTICULAR FOR AN AIRCRAFT

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19833311053 DE3311053A1 (en) 1983-03-25 1983-03-25 SEAT FOR A VEHICLE, IN PARTICULAR A PLANE

Publications (1)

Publication Number Publication Date
DE3311053A1 true DE3311053A1 (en) 1984-09-27

Family

ID=6194742

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19833311053 Withdrawn DE3311053A1 (en) 1983-03-25 1983-03-25 SEAT FOR A VEHICLE, IN PARTICULAR A PLANE

Country Status (3)

Country Link
DE (1) DE3311053A1 (en)
FR (1) FR2543079A1 (en)
GB (1) GB2137492A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3443103A1 (en) * 1984-11-27 1986-05-28 Paul Stoessel GmbH + Co KG, 4005 Meerbusch Vehicle seat with upholstery protection
US5477572A (en) * 1991-04-22 1995-12-26 C.A. Greiner & Sohne Gesellschaft M.B.H. Vehicle seat cushion

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3507085A1 (en) * 1985-02-28 1986-08-28 Metzeler Schaum Gmbh, 8940 Memmingen AIRCRAFT SEAT IN FLAME-RETARDANT DESIGN
DE3767156D1 (en) * 1986-05-09 1991-02-07 Greiner Schaumstoffwerk SEAT, ESPECIALLY FOR PUBLIC TRANSPORT.
EP0281694A1 (en) * 1987-03-11 1988-09-14 Magerik Ltd A seat

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2891033A (en) * 1956-02-07 1959-06-16 Gen Electric Process for the preparation of flameretardant silicone rubber and composition thereof
GB833141A (en) * 1957-06-07 1960-04-21 Midland Silicones Ltd Organosiloxane compositions
GB869565A (en) * 1958-10-01 1961-05-31 Midland Silicones Ltd Insulating material
GB1274839A (en) * 1969-07-16 1972-05-17 Dow Corning Improved flame resistant silicone composition
GB1446013A (en) * 1973-07-14 1976-08-11 Dunlop Ltd Flame-retardant composite articles
GB1477145A (en) * 1974-07-12 1977-06-22 Norman N Flame retardant means
US4174420A (en) * 1975-04-29 1979-11-13 E. I. Du Pont De Nemours And Company Upholstered furniture having improved flame resistance
US4031579A (en) * 1975-12-19 1977-06-28 The United States Of America As Represented By The Secretary Of The Air Force Aircraft seat cushion
US4246313A (en) * 1979-01-12 1981-01-20 Owens-Illinois, Inc. Heat-resistant composite material and method of making same
US4349494A (en) * 1979-05-07 1982-09-14 W. R. Grace & Co. Method of making a fire-retardant product having a foamed lore and a fire-retardant protective layer
DE3041588A1 (en) * 1980-11-04 1982-06-09 Bayer Ag, 5090 Leverkusen FLAME-RESISTANT POLYSILOXANE MOLDS
GB2105584B (en) * 1981-07-17 1985-08-21 Courtaulds Plc Fire resistant support for the human body
FI822525L (en) * 1981-07-17 1983-01-18 Courtaulds Plc ELDHAERDIGT STOED FOER MAENNISKOKROPPEN
GB2116838A (en) * 1982-03-22 1983-10-05 British Vita Company Limited Upholstery component

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3443103A1 (en) * 1984-11-27 1986-05-28 Paul Stoessel GmbH + Co KG, 4005 Meerbusch Vehicle seat with upholstery protection
US5477572A (en) * 1991-04-22 1995-12-26 C.A. Greiner & Sohne Gesellschaft M.B.H. Vehicle seat cushion
US5632053A (en) * 1991-04-22 1997-05-27 C.A. Greiner & Sohne Gesellschaft M.B.H. Vehicle seat cushion

Also Published As

Publication number Publication date
GB2137492A (en) 1984-10-10
GB8406276D0 (en) 1984-04-11
FR2543079A1 (en) 1984-09-28

Similar Documents

Publication Publication Date Title
DE69428377T2 (en) METHOD AND SPRAY MOLDING DEVICE FOR PRODUCING AN ELASTOMERIC SKIN FROM AT LEAST TWO MATERIALS AND MANUFACTURED ELASTOMERIC SKIN
DE69323190T2 (en) Process for the production of a thermoplastic composite panel
DE102018127597A1 (en) Planar heater and manufacturing method therefor
DE2758581B1 (en) Windshield, especially for motor vehicles, with an inner pane made of chemically toughened silicate glass
EP0387400A2 (en) Bulkhead
EP1128988B1 (en) Vehicle rooflining and method for producing the same
DE29517468U1 (en) Handle device for the interior of a vehicle
DE3311053A1 (en) SEAT FOR A VEHICLE, IN PARTICULAR A PLANE
DE69006891T2 (en) Radial pneumatic tire.
EP0193165A2 (en) Flame-resistant air line passenger seat
DE2703785B2 (en) Composite safety pane, in which the inner pane breaks into pieces that are as small as possible and largely exclude cuts due to impact
EP0298987B1 (en) Seat, especially for public transport vehicles
EP0115869B1 (en) Floor covering, especially for aeroplanes
DE2603325A1 (en) TIRE
EP0230952A2 (en) Back upholstery for an aircraft passenger seat
WO2009074876A2 (en) Wound glass fiber-reinforced plastic pipes, and method for the production thereof
DE60102307T2 (en) Method for improving the breaking strength of an aircraft
EP1110859B1 (en) Cabin window for passenger aircraft
DE3725146A1 (en) Seat, in particular for motor vehicles
DE3113246C2 (en) Process for the production of a laminate
DE9217352U1 (en) Multi-layered bellows casing for a flexible transition
EP0078424B1 (en) Layer structure, and method for the continuous manufacture of a layer structure
DE60315768T2 (en) Window pane, window with such a window pane, method for producing such a window pane and its use
DE102022122363A1 (en) ENERGY ABSORBING MATERIAL FOR A VEHICLE
DE102007017467A1 (en) Steering wheel with foam surround and method for producing a steering wheel

Legal Events

Date Code Title Description
8110 Request for examination paragraph 44
8139 Disposal/non-payment of the annual fee