FR2543079A1 - SEAT FOR VEHICLE, IN PARTICULAR FOR AN AIRCRAFT - Google Patents
SEAT FOR VEHICLE, IN PARTICULAR FOR AN AIRCRAFT Download PDFInfo
- Publication number
- FR2543079A1 FR2543079A1 FR8404371A FR8404371A FR2543079A1 FR 2543079 A1 FR2543079 A1 FR 2543079A1 FR 8404371 A FR8404371 A FR 8404371A FR 8404371 A FR8404371 A FR 8404371A FR 2543079 A1 FR2543079 A1 FR 2543079A1
- Authority
- FR
- France
- Prior art keywords
- polysiloxane
- coating
- layer
- seat
- flammable
- 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.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered 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
- B32B5/18—Layered 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
-
- A—HUMAN NECESSITIES
- A47—FURNITURE; DOMESTIC ARTICLES OR APPLIANCES; COFFEE MILLS; SPICE MILLS; SUCTION CLEANERS IN GENERAL
- A47C—CHAIRS; SOFAS; BEDS
- A47C7/00—Parts, details, or accessories of chairs or stools
- A47C7/02—Seat parts
- A47C7/18—Seat parts having foamed material included in cushioning part
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered 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
- B32B5/16—Layered 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered 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
- B32B5/22—Layered 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
- B32B5/24—Layered 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
- B32B5/245—Layered 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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; ARRANGEMENTS 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
- B64D11/0647—Seats characterised by special upholstery or cushioning features
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2264/00—Composition or properties of particles which form a particulate layer or are present as additives
- B32B2264/10—Inorganic particles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2266/00—Composition of foam
- B32B2266/02—Organic
- B32B2266/0214—Materials belonging to B32B27/00
- B32B2266/0278—Polyurethane
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/30—Properties of the layers or laminate having particular thermal properties
- B32B2307/306—Resistant to heat
- B32B2307/3065—Flame resistant or retardant, fire resistant or retardant
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2383/00—Polysiloxanes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2605/00—Vehicles
- B32B2605/18—Aircraft
Abstract
SIEGE POUR VEHICULE, NOTAMMENT POUR UN AVION. LA PARTIE INTERIEURE DU REVETEMENT12 EN MATIERE TEXTILE RECOUVRANT L'AME EN MATIERE MOUSSE16 EST MUNIE D'UNE COUCHE14 EN POLYSILOXANE ININFLAMMABLE. AVIATION.SEAT FOR VEHICLE, ESPECIALLY FOR AN AIRPLANE. THE INTERIOR PART OF THE COATING12 IN TEXTILE MATERIAL COVERING THE CORE IN FOAM MATERIAL16 IS PROVIDED WITH A LAYER14 IN FLAMMABLE POLYSILOXANE. AVIATION.
Description
Siège pour un véhicule, notamment pour un avion.Seat for a vehicle, especially for an airplane.
La présente invention concerne un siège pour The present invention relates to a seat for
un véhicule, notamment pour un avion, comprenant une- a vehicle, in particular for an airplane, comprising a
âme en matière mousse, éventuellement supportée, un revêtement en une matière textile sur l'âme en matière mousse,et unecouche en une matière ignifuge, entre foam core, optionally supported, a coating of a textile material on the foam core, and a layer of flame retardant material, between
l'âme en matière mousse et le revêtement. the foam core and the coating.
En particulier, pour concevoir des sièges pour des avions, on a fait beaucoup d'efforts pour former ces sièges de façon à ce que, en cas d'incendie, les flammes se propagent aussi lentement In particular, to design seats for aircraft, much effort has been made to form these seats so that, in case of fire, the flames propagate as slowly
que possible et qu'ainsi les passagers de l'avion dis- as possible and thus the passengers of the aircraft
posent de suffisamment de temps pour en sortir. have enough time to get out.
C'est ainsi, par exemple, qu'il est connu d'entourer l'âme en matière mousse d'une mince couche supplémentaire en matière mousse ignifuge Le dépôt de cette couche supplémentaire sur l'âme en matière mousse soulève, cependant, des problèmes pratiques; en outre, l'effet ignifugeant de cette matière mousse supplémentaire est relativement faible par unité de poids, c'est-à-dire qu'il faut utiliser une couche de Thus, for example, it is known to surround the foam core with a thin additional layer of flame retardant foam material. The deposition of this additional layer on the foam core raises, however, practical problems; in addition, the flame-retarding effect of this additional foam material is relatively low per unit weight, i.e. a layer of
matière mousse supplémentaire relativement épaisse. relatively thick additional foam material.
L'invention vise un siège pour un véhicule, notamment pour un avion, du type mentionné au début The invention relates to a seat for a vehicle, especially for an aircraft, of the type mentioned at the beginning
du présent mémoire, dans lequel les inconvénients in- of this specification, in which the disadvantages
diqués ci-dessus ne se produisent pas. diques above do not occur.
On propose notamment un siège dans lequel le dépôt de la couche supplémentaire en matière ignifuge In particular, a seat is proposed in which the deposition of the additional layer of flame-retardant material
ne pose pas de problèmes.does not pose any problems.
Suivant l'invention, la partie intérieure du revêtement en la matière textile est munie d'une cou- According to the invention, the inner part of the coating of the textile material is provided with a cover
che en un polysiloxane ininflammable. to a non-flammable polysiloxane.
De préférence: la couche en polysiloxane ininflammable est appliquée par enduction ou par calandrage; la couche en polysiloxane ininflammable a une épaisseur de 0,1 à 0,6 mm environ, et notamment de 0,3 à 0,4 mm; le polysiloxane ininflammable est constitué d'un diorganopolysiloxane, d'acide silicique à l'état finement divisé, de dioxyde de titane à l'état finement Preferably: the non-flammable polysiloxane layer is applied by coating or calendering; the non-flammable polysiloxane layer has a thickness of about 0.1 to 0.6 mm, and especially 0.3 to 0.4 mm; the non-flammable polysiloxane consists of a diorganopolysiloxane, silicic acid in the finely divided state, titanium dioxide in the finely divided state
divisé et d'un composé azoté.divided and a nitrogen compound.
Les avantages procurés par l'invention repo- The advantages provided by the invention
sent notamment sur le fait que le revêtement en la ma- in particular, that the coating in the
tière textile est muni d'une couche en polysiloxane fabric is equipped with a polysiloxane layer
ininflammable; on peut fabriquer ce matériau de sur- nonflammable; this material can be made from
facesans problèmes,à la dimension et/ou au dessin souhaité, le polysiloxane pouvant être appliqué sur le with no problems, in the desired size and / or pattern, the polysiloxane can be applied to the
revêtement par enduction ou par calandrage Les machi- coatings by coating or calendering
nes nécessaires à cet effet sont disponibles en les dimensions souhaitées, de sorte qu'aucun investissement necessary for this purpose are available in the desired dimensions, so that no investment
coûteux n'est nécessaire à cet effet. expensive is necessary for this purpose.
Suivant un mode de réalisation préféré, le polysiloxane est déposé en une épaisseur aussi petite According to a preferred embodiment, the polysiloxane is deposited in such a small thickness
que possible, des résultats favorables étant été obte- as possible, favorable results have been achieved
nus avec des épaisseurs de couche de 0,3 à 0,4 mm. bare with layer thicknesses of 0.3 to 0.4 mm.
Des recherches ont montré que des sièges pour Research has shown that seats for
avions suivant l'invention satisfont à toutes les exi- planes according to the invention satisfy all the requirements
gences respectives et, notamment, que l'on peut respec- respective authorities and, in particular, that it is possible
ter sans problèmes le temps d'évacuation de 90 secon- without difficulty the evacuation time of 90 seconds
des prescrit par les normes américaines. prescribed by US standards.
Suivant un mode de réalisation préféré, on utilise un polysiloxane tel que décrit dans la demande de brevet européen publiée sous le No 00 51 212 Un According to a preferred embodiment, a polysiloxane as described in European Patent Application No. 00 51 212 A is used.
tel polysiloxane est constitué d'un diorganopolysilo- such polysiloxane consists of a diorganopolysiloxane
xane, d'acide silicique à l'état finement divisé et/ou d'autres matières de charge, de Ti O 2 à l'état finement divisé, de platine, d'un agent de durcissement, ainsi xane, finely divided silicic acid and / or other fillers, finely divided TiO 2, platinum, a curing agent,
que d'un composé azoté.than a nitrogen compound.
Ce polysiloxane doit être durci à des tempéra- This polysiloxane must be cured at temperatures
tures supérieures à 60 C, sous la pression normale ou sous une pression supérieure à la pression normale, en une durée déterminée, de manière à obtenir le stade dit A de la vulcanisation On peut effectuer ensuite une post-vulcanisation qui dure de 1 à 24 heures, et above 60 ° C, under normal pressure or at a pressure higher than the normal pressure, in a determined time, so as to obtain the so-called stage of vulcanization Can be carried out a post-vulcanization which lasts from 1 to 24 hours, and
qui conduit au stade B de la vulcanisation. which leads to stage B vulcanization.
Lorsque l'on applique le polysiloxane par enduction, on effectue les deux stades de durcissement l'un après l'autre Si l'on applique -le polysilôxane par calandrage, on effectue la vulcanisation pour aller jusqu'au stade A, lors du calandrage, que l'on fait suivre ensuite de la vulcanisation pour aller au stade B. When the polysiloxane is applied by coating, the two stages of curing are carried out one after the other. If the polysiloxane is applied by calendering, the vulcanization is carried out to go to stage A, during calendering. , which is then followed by vulcanization to go to stage B.
Le revêtement en la matière textile se pré- The coating of the textile material is
sentant sous la forme d'une structure superficielle feeling in the form of a superficial structure
d'un seul tenant, et la couche déposée en le poly- in one piece, and the layer deposited in the poly-
siloxane ininflammable, sont fixés de la façon habi- non-flammable siloxane, are fixed in the usual way
tuelle sur l'âme en matière mousse, de sorte que l'on peut se dispenser des stades de fabrication qui étaient nécessaires jusqu'ici au dépôt d'une couche supplémentaire entre l'âme en matière mousse et le revêtement. L'invention est explicitée, d'une manière plus précise, dans ce qui suit, au moyen d'un exemple de réalisation en se référant au dessin schématique annexé, dont la figure unique est une vue en coupe a It is possible to dispense with the stages of manufacture which have hitherto been necessary for the deposition of an additional layer between the foam core and the coating. The invention is explained, in a more precise manner, in the following, by means of an embodiment with reference to the attached schematic drawing, the single figure of which is a sectional view.
25430 0925430 09
échelle agrandie d'une partie d'un siège pour mm avion. Le siège pour avion représenté à la fiumre est désigné, d'une manière générale, par 1 e sigme de référence 10, et présente une âme en matière musse enlarged scale of part of a seat for mm plane. The aircraft seat shown in black is generally designated by the reference sigma 10, and has a soul in musse material.
16 qui est, par exemple, en mousse de polyurétmanne. 16 which is, for example, polyurethane foam.
En cas de besoin, on peut maintenir cette lm en ma- If needed, this lm can be maintained by
tière mousse 16 en la forme et en la position somba- foam 16 in the shape and in the somba-
tées par un support, qui n'est pas représenté. by a support, which is not represented.
Cette âme en matière mousse 16, qui a déjà la forme du siège 10 pour avion, est munie, sur sa face extérieure, d'un revêtement qui est constitui d'un revêtement habituel 12 en matière textile et d'une couche 14 en polysiloxane ininflammable relle This foam core 16, which already has the shape of the seat 10 for aircraft, is provided on its outer face, a coating which is constituted by a usual coating 12 of textile material and a layer 14 of polysiloxane not flammable real
rigidement au revêtement 12.rigidly to the skin 12.
La couche 14 en polysiloxane ininfl Emmable a été appliquée sur la partie intérieure du rev temmt The layer 14 in polysiloxane uninflammable Emmable was applied to the inner part of the rev temmt
12 en la matière textile, par enduction ou par caam- 12 in the textile field, by coating or
drage, la vulcanisation du polysiloxane jusqu'au the vulcanization of the polysiloxane
stade A et jusqu'au stade B se déroulant en deux sta- stage A and up to stage B taking place in two stages
des successifs.successive ones.
La composition du polysiloxane utilisée de préférence peut être celle décrite dans la demande de brevet européen de la Société Bayer AG, publiée ous le No 00 51 212 Ce polysiloxane ininflammable est The composition of the polysiloxane preferably used can be that described in the European patent application of Bayer AG, published under No. 00 51 212 This non-flammable polysiloxane is
constitué d'un diorganopolysiloxane, d'acide siólci- consisting of a diorganopolysiloxane, SiO
que à l'état finement divisé et/ou d'autres matières de charge, de dioxyde de titane à l'état fime ut divisé, de platine, d'un agent de durcissement, almsi in the finely divided state and / or other filler materials, split titanium dioxide, platinum, a hardening agent, almsi
que d'un composé azoté.than a nitrogen compound.
Si l'on enduit le revêtement du polysi Loxame à l'état non vulcanisé, il faut effectuer esmite les deux étapes de vulcanisation menant au stade A et au stade B Lorsque l'on applique le polysiloxame par If the coating is coated with the unvulcanized polysiloxane, the two vulcanization steps leading to stage A and stage B are to be carried out. When the polysiloxam is applied by
calandrage, la vulcanisation jusqu'au stade A s"effec- calendering, vulcanization to stage A is carried out
tue pendant le calandrage; la vulcanisation jusqu'au kills during calendering; vulcanization up to
stade B doit alors être effectuée ensuite de la fa- stage B must then be carried out from the
çon habituelle.usual lesson.
2543079 -2543079 -
Claims (4)
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 |
---|---|
FR2543079A1 true FR2543079A1 (en) | 1984-09-28 |
Family
ID=6194742
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8404371A Pending FR2543079A1 (en) | 1983-03-25 | 1984-03-21 | SEAT FOR VEHICLE, IN PARTICULAR FOR AN AIRCRAFT |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE3311053A1 (en) |
FR (1) | FR2543079A1 (en) |
GB (1) | GB2137492A (en) |
Families Citing this family (5)
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 |
DE3507085A1 (en) * | 1985-02-28 | 1986-08-28 | Metzeler Schaum Gmbh, 8940 Memmingen | AIRCRAFT SEAT IN FLAME-RETARDANT DESIGN |
CH670995A5 (en) * | 1986-05-09 | 1989-07-31 | Greiner Schaumstoffwerk | |
EP0281694A1 (en) * | 1987-03-11 | 1988-09-14 | Magerik Ltd | A seat |
AT399488B (en) * | 1991-04-22 | 1995-05-26 | Greiner & Soehne C A | Seat cushion, in particular an aircraft seat |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
EP0051212A1 (en) * | 1980-11-04 | 1982-05-12 | Bayer Ag | Flame-proof polyorganosiloxane compositions |
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 |
EP0070701A1 (en) * | 1981-07-17 | 1983-01-26 | Courtaulds Plc | Fire-resistant support for the human body |
Family Cites Families (9)
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 |
SE381272B (en) * | 1969-07-16 | 1975-12-01 | Dow Corning | FLAME RESISTANT SILICONE LOAD 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 |
GB2105584B (en) * | 1981-07-17 | 1985-08-21 | Courtaulds Plc | Fire resistant support for the human body |
GB2116838A (en) * | 1982-03-22 | 1983-10-05 | British Vita Company Limited | Upholstery component |
-
1983
- 1983-03-25 DE DE19833311053 patent/DE3311053A1/en not_active Withdrawn
-
1984
- 1984-03-09 GB GB08406276A patent/GB2137492A/en not_active Withdrawn
- 1984-03-21 FR FR8404371A patent/FR2543079A1/en active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
EP0051212A1 (en) * | 1980-11-04 | 1982-05-12 | Bayer Ag | Flame-proof polyorganosiloxane compositions |
EP0070701A1 (en) * | 1981-07-17 | 1983-01-26 | Courtaulds Plc | Fire-resistant support for the human body |
Also Published As
Publication number | Publication date |
---|---|
GB2137492A (en) | 1984-10-10 |
DE3311053A1 (en) | 1984-09-27 |
GB8406276D0 (en) | 1984-04-11 |
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