WO2011026598A1 - Verfahren zur herstellung einer fluchtwegmarkierung sowie eine solche - Google Patents
Verfahren zur herstellung einer fluchtwegmarkierung sowie eine solche Download PDFInfo
- Publication number
- WO2011026598A1 WO2011026598A1 PCT/EP2010/005327 EP2010005327W WO2011026598A1 WO 2011026598 A1 WO2011026598 A1 WO 2011026598A1 EP 2010005327 W EP2010005327 W EP 2010005327W WO 2011026598 A1 WO2011026598 A1 WO 2011026598A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- profile element
- profile
- luminescent layer
- mixture
- escape route
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21K—NON-ELECTRIC LIGHT SOURCES USING LUMINESCENCE; LIGHT SOURCES USING ELECTROCHEMILUMINESCENCE; LIGHT SOURCES USING CHARGES OF COMBUSTIBLE MATERIAL; LIGHT SOURCES USING SEMICONDUCTOR DEVICES AS LIGHT-GENERATING ELEMENTS; LIGHT SOURCES NOT OTHERWISE PROVIDED FOR
- F21K2/00—Non-electric light sources using luminescence; Light sources using electrochemiluminescence
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60Q—ARRANGEMENT OF SIGNALLING OR LIGHTING DEVICES, THE MOUNTING OR SUPPORTING THEREOF OR CIRCUITS THEREFOR, FOR VEHICLES IN GENERAL
- B60Q3/00—Arrangement of lighting devices for vehicle interiors; Lighting devices specially adapted for vehicle interiors
- B60Q3/40—Arrangement of lighting devices for vehicle interiors; Lighting devices specially adapted for vehicle interiors specially adapted for specific vehicle types
- B60Q3/41—Arrangement of lighting devices for vehicle interiors; Lighting devices specially adapted for vehicle interiors specially adapted for specific vehicle types for mass transit vehicles, e.g. buses
- B60Q3/46—Emergency lighting, e.g. for escape routes
-
- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09K—MATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
- C09K11/00—Luminescent, e.g. electroluminescent, chemiluminescent materials
- C09K11/02—Use of particular materials as binders, particle coatings or suspension media therefor
-
- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09K—MATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
- C09K11/00—Luminescent, e.g. electroluminescent, chemiluminescent materials
- C09K11/08—Luminescent, e.g. electroluminescent, chemiluminescent materials containing inorganic luminescent materials
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/23—Sheet including cover or casing
Definitions
- the present invention relates to a method for producing an escape route marking and an escape route marking.
- EP 0 489 561 A1 discloses a permanently fluorescent layer in which color pigments are incorporated into a polymer matrix.
- the fluorescent material may be incorporated in a carrier which imparts different optical properties to the fluorescent light through additional filters.
- CONFIRMATION COPY From WO 01/52224 AI emergency lighting for an aircraft is known, is used in the escape route markers in the form of inserts, self-adhesive tapes and color in the aircraft interior.
- EP 0 828 657 B1 discloses an emergency lighting unit for the aircraft interior, which is held in position via a cover element connected directly to the aircraft floor.
- a photoluminescent material which is prepared from a mixture of a transparent base material and photoluminescent pigments, wherein at 20 ° C, the viscosity of the transparent base material is 1 Pa s or more and photoluminescent pigments in an amount of 7 to 95 wt .-% be added.
- silicone material for the use of silicone material as a transparent base material, a viscosity of 70 Pa s and an average particle size of 150 ⁇ is proposed for the photoluminescent pigments.
- the invention has for its object to provide an escape route marking with the best possible luminance, which is designed to be robust for use in the aircraft interior.
- the object is achieved by a method having the features of claim 1.
- the escape route marking triggers with the characteristics Claim 10 this task.
- Advantageous embodiments of the invention form the subject of the dependent claims.
- the method according to the invention serves to produce an escape route marking for an aircraft having a luminescent glowing luminescent layer and a profile which has two profile elements which can be connected to each other, wherein in a first of the profile elements the luminescent layer is arranged in a recess extending in the longitudinal direction, characterized by
- the introduction of the mixture in the liquid state in the recording and curing of the mixture with the photoluminescent pigments in the recording to use silicone materials that have a low viscosity and are not suitable for insertion into a hollow profile because of their rigidity.
- the second profile element is provided for connection to the ground. This means that the profile element into which the luminescent layer has been introduced, that profile element, through which the luminescent layer is visible in the installed position.
- the first profile element is at least partially transparent, so that the light the luminescent layer can be perceived.
- the silicone material has a viscosity of less than 9.5 Pa s at a temperature of 20.degree. C. and the average particle size of the pigments is less than 150 .mu.m, the proportion of the pigments being 50 to 90 wt. in the mixture amounts to.
- the use of a low-viscosity silicone material makes it possible to use pigments with a small average grain size and thus to achieve sufficient luminosity.
- the luminescent layer is introduced in liquid form in the first profile element, it is possible to work with low viscosity, low viscous silicone materials and to put them with pigments that have the smallest possible average grain size.
- the mixture is poured for introduction into the receptacle.
- the casting process can be carried out directly into the designed profile element, wherein the introduced mixture then filled evenly or with a spreading aid evenly fills the receptacle in the profile element.
- the advantage of potting the mixture in the receptacle is that a uniform thickness of the luminescent layer can be achieved. It is also ensured that a continuous luminescent layer forms and the luminescent layer bears against the profile element without bubbles or cavities.
- the mixture is continuously injected, for example via a nozzle or a screw in the designed profile element or extracted into this.
- the luminescent layer is formed by connecting the first profile covered elements with the second profile element.
- the cover of the first profile element protects the luminescent layer from moisture and mechanical stress.
- connection of the first and second profile element by gluing and / or by welding the profile elements.
- At least the inner walls in the first profile element are subjected to a surface treatment before the mixture is introduced into the recess.
- the surface treatment serves to promote the crosslinking of the silicone material with the wall material of the first profile element.
- an infrared radiation is used, which is directed after the introduction of the silicone material onto the first profile element and the silicone material.
- a flame treatment of the first profile element has been found. This can be done additionally or alternatively to the infrared radiation. Likewise, primers and / or a plasma jet treatment may be used for the first profile element to prepare the surface for better cross-linking with the liquid or curing mixture.
- the invention is also achieved by an escape route marking according to the features of claim 10.
- the escape route marking according to the invention for an aircraft has a luminescent layer which luminesces in the dark and a profile which has two profile elements which can be connected to one another, the luminescent layer being in a receptacle of the first profile element is arranged.
- the luminescent layer consists of a silicone material with photoluminescent pigments and is non-positively connected, preferably cohesively, to the first profile element.
- the non-positive and in particular the integral connection between the luminescent layer and the profile element helps to stabilize the profile element.
- the surface of the first profile element may be slightly convex, so that fluids flow away from it. For example, stress cracks in the first profile element that are induced by cleaning fluid can be avoided.
- the first profile element consists of a transparent plastic material, wherein the transparent plastic material can also be colored to obtain a color that is different from the color with which the luminescent layer luminesces.
- the first profile element has a recess extending in the longitudinal direction, which is bounded by two lateral webs running parallel to each other.
- the lateral webs border on the one hand to the lateral recess to fill the mixture in the liquid state and on the other hand, they can support a connection between the first and second profile element.
- the second profile element preferably has a recess extending in the longitudinal direction in which the luminescent layer connected to the first profile element is immersed when the first and second profile elements are connected to one another.
- the recess of the second profile element serves as a receptacle for the luminescent layer, which is fastened to a recess of the first profile element.
- Fig. 4 shows a fourth embodiment, in which the profile elements are connected to each other in their side sections and
- Fig. 5 is a schematic view of the production of the escape route marking according to the invention.
- Fig. 1 shows a first profile element 10, which has a flat base portion 12 and two laterally angled side portions 14. In the transition between base portion 12 and side portion 14, two webs 16 are provided which extend continuously in the longitudinal direction of the profile element.
- the free end of the side region 14 ends approximately at the level of the free end of the webs 16, so that the outer edge of the side region and the free end of the webs lie in one plane.
- the receptacle formed by the base portion 12 and the webs 16 of the first profile element 10 is filled with the luminescent layer 18.
- the luminescent layer 18 is poured continuously in the liquid state into the profile element and cures in this. With the curing of the luminescent layer in the profile element go Materials a compound that holds the luminescent layer in the profile element with a connection force. This connection force is based on a material connection. Through a surface treatment of the recording, the silicone material crosslinks during curing with the material of the profile rail. It is preferred that only one layer of the silicone material be introduced into the rail.
- the profile rail is preferably made of a polycarbonate material (PC).
- the first profile element 10 with the hardened luminescent layer 18 is connected to the second profile element 20.
- the second profile element 20 has a recess 22 which is bounded by side portions 24. The contour of the side portions 24 corresponds in its course to the curved side portions 14, so that the first profile element 10 rests flat against the second profile element 20.
- the second profile element 20 has a smooth underside and may additionally be equipped with means for connection to the ground. As a material for the second profile element 20 may also be provided a PC plastic. In contrast to the first profile element 10, it is not necessary that the second profile element 20 is transparent or translucent.
- the recess 22 in the second profile element 20 is dimensioned so that a non-positive connection between the webs 16 and the inner sides of the side portions 24 takes place.
- the side portions 16 with the side portions 24 of the other profile element cohesively, so for example glued or welded.
- the side portion 14 is additionally provided with a web 26.
- the side portion 24 of the second profile element 20 also has a recess 28 in which the web 26 is arranged. As already described in connection with FIG. 1, webs 16 can additionally be clamped in the recess 28. These can also be glued.
- FIG. 3 shows an embodiment in which a first profile element 30 is fastened to the second profile element 36 with a snap connection.
- the first profile element 30 is equipped with a receptacle delimited by webs 16, which is poured out by a luminescent layer 18.
- the side region of the first profile element 30 has a projection 32, which engages behind a snap-in nose 34 of the second profile element 36.
- FIG. 4 shows a further embodiment in which a first profile element 38 has webs 40 which laterally delimit the recess for receiving the luminescent layer 42.
- the webs 40 have on their side facing to the side portions 43 side a tapered side wall 44.
- the second profile element 46 has a second recess into which the webs 40 with the luminescent layer 42 dip.
- the second recess is bounded laterally by a side portion 48 having a beveled side wall 50.
- the air gap allows the connection of the web elements 38 and 46 with a sufficient manufacturing tolerance.
- the air gap 52, the web element 38 sufficient clearance when it is loaded from above.
- a reflection layer 54 is provided, which is formed, for example, in white color and throws the light back from the luminescent layer.
- a reflection layer can also be used in the embodiments of FIGS. 1 to 3 be provided.
- the side portions 48 and 43 are integrally connected by gluing and / or welding. For bonding, for example, a double-sided adhesive tape may be provided.
- the first profile element 60 is shown, which is unwound continuously by a drum 62.
- the first profile element 60 designed as an upper shell can be processed as an endless profile element in the production process shown in FIG.
- the profile element 60 is irradiated with laser light.
- a labeling laser with a relatively low power can be used, which serves to apply a part number or other marking.
- a subsequent step 66 there is a flame treatment of the receptacle provided for the silicone material in the first profile element. By the flame treatment, the first profile element is prepared for a subsequent recording of the silicone mixture.
- the silicone mixture is introduced into the first profile element 60.
- the silicone mixture is introduced substantially liquid, wherein by adjusting the viscosity of the silicone mixture excessive sagging or settling of the pigments is avoided.
- infrared radiation of the silicone mixture introduced into the first profile element takes place.
- the infrared radiation can, as shown in FIG. 5, take place directly on the silicone mixture.
- the second profile element 72 is unwound from a drum 74. The second Profile element 72 is applied over the first profile element 60 and closes it. If provision should be made for an additional reflector layer to be introduced between the light strip and the second profile element, then this additional reflector layer can be introduced between the work steps 70 and 72.
- a subsequent step 76 the two profile elements 60 and 72 are welded together.
- a stationary laser can be used which continuously welds the profile elements together along their edge.
- a continuous adhesive strip 80 is applied to the upper side of the second profile element 72.
- the adhesive strip 80 may, for example, be in the form of a double-sided adhesive strip, by means of which, after removal of a protective film from the adhesive surface, the completed escape route marking can be glued to the substrate.
- an automatic quality control takes place.
- the automatic quality control 82 takes place continuously and continuously during production.
- quality control 82 may optically control the welds between the first and second profile members, the thickness of the incorporated silicone material, or the location of the adhesive tape 80.
- step 84 the continuously produced escape route markings are brought to a predetermined length in order to then be transported away via a carriage 86.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Inorganic Chemistry (AREA)
- Illuminated Signs And Luminous Advertising (AREA)
- Road Signs Or Road Markings (AREA)
- Application Of Or Painting With Fluid Materials (AREA)
- Paints Or Removers (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Abstract
Description
Claims
Priority Applications (8)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA2772683A CA2772683C (en) | 2009-09-01 | 2010-08-31 | Method for producing an escape route marking and an escape route marking |
BR112012004724-8A BR112012004724B1 (pt) | 2009-09-01 | 2010-08-31 | processo para a produção de uma marca de rota de escape para uma aeronave e marca de rota de escape para uma aeronave |
CN201080038760.1A CN102597601B (zh) | 2009-09-01 | 2010-08-31 | 用于制造逃生路线标志的方法以及这种逃生路线标志 |
EP10771318A EP2352949B1 (de) | 2009-09-01 | 2010-08-31 | Verfahren zur herstellung einer fluchtwegmarkierung sowie eine solche |
RU2012111207/07A RU2533667C2 (ru) | 2009-09-01 | 2010-08-31 | Способ изготовления маркировки маршрута эвакуации и маркировка маршрута эвакуации |
ES10771318T ES2400455T3 (es) | 2009-09-01 | 2010-08-31 | Procedimiento para la producción de una marca de vía de huida así como marca de vía de huida |
JP2012525939A JP5721716B2 (ja) | 2009-09-01 | 2010-08-31 | 避難経路標識の製造方法ならびに避難経路標識 |
US13/393,581 US8636867B2 (en) | 2009-09-01 | 2010-08-31 | Method for producing an escape route marking and an escape route marking |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102009040042A DE102009040042B4 (de) | 2009-09-01 | 2009-09-01 | Verfahren zur Herstellung einer Fluchtwegmarkierung sowie eine solche |
DE102009040042.7 | 2009-09-01 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2011026598A1 true WO2011026598A1 (de) | 2011-03-10 |
Family
ID=43218451
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/EP2010/005327 WO2011026598A1 (de) | 2009-09-01 | 2010-08-31 | Verfahren zur herstellung einer fluchtwegmarkierung sowie eine solche |
Country Status (10)
Country | Link |
---|---|
US (1) | US8636867B2 (de) |
EP (1) | EP2352949B1 (de) |
JP (1) | JP5721716B2 (de) |
CN (1) | CN102597601B (de) |
BR (1) | BR112012004724B1 (de) |
CA (1) | CA2772683C (de) |
DE (1) | DE102009040042B4 (de) |
ES (1) | ES2400455T3 (de) |
RU (1) | RU2533667C2 (de) |
WO (1) | WO2011026598A1 (de) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102012006902A1 (de) * | 2012-04-05 | 2013-10-10 | Lufthansa Technik Ag | Fluchtwegmarkierung mit einem Leuchtstreifen aus photolumineszentem Material |
DE102012016046B3 (de) * | 2012-08-14 | 2013-12-24 | Lufthansa Technik Ag | Verfahren zum Herstellen einer Fluchtwegmarkierung für Flugzeuge sowie eine solche |
DE102014112686B3 (de) * | 2014-09-03 | 2015-04-09 | Lufthansa Technik Aktiengesellschaft | Fluchtwegmarkierung für ein Flugzeug |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2016010666A1 (en) * | 2014-07-15 | 2016-01-21 | Green Zachary L | Photoluminescent signage |
JP6568028B2 (ja) * | 2016-09-13 | 2019-08-28 | 信越化学工業株式会社 | 蓄光表示構造体の製造方法 |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0489561A1 (de) | 1990-12-06 | 1992-06-10 | Minnesota Mining And Manufacturing Company | Gegenstände, die dauerhafte Fluoreszenz zeigen |
WO1996033093A1 (en) * | 1995-04-20 | 1996-10-24 | Saf-T-Glo Aerospace Limited | Emergency lighting |
WO1998004645A1 (en) * | 1996-07-31 | 1998-02-05 | Beele Engineering B.V. | Silicone rubber-containing, afterglowing preparation, product provided therewith and use thereof |
WO2001052224A1 (en) | 2000-01-08 | 2001-07-19 | Stg Aerospace Limited | Emergency lighting |
US20020015309A1 (en) | 2000-07-25 | 2002-02-07 | Stokes Peter David | Emergency lighting |
US7074345B2 (en) | 2001-12-28 | 2006-07-11 | Availvs Corporation | Highly luminous light-emitting material and manufacturing method thereof |
EP1783000A1 (de) * | 2005-11-03 | 2007-05-09 | Saf-t-Glo Limited | Notbeleuchtung |
WO2008110344A1 (de) * | 2007-03-13 | 2008-09-18 | Lufthansa Technik Ag | Fluchtwegmarkierung für ein flugzeug |
DE202007010221U1 (de) * | 2007-07-23 | 2008-12-04 | Agor Gmbh & Co. Kg | Leuchtstreifen |
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DE29608585U1 (de) * | 1995-10-04 | 1996-10-10 | P.E.R. Flucht- und Rettungsleitsysteme GmbH, 22885 Barsbüttel | Vorrichtung zur Ausbildung nachleuchtender Signalflächen |
JPH09127891A (ja) * | 1995-11-02 | 1997-05-16 | Suzuki Sogyo Co Ltd | 反射材 |
DE19700310A1 (de) * | 1997-01-09 | 1998-07-16 | Permalight Leuchtfarben Ag | Leuchtfähige Substanz |
JP3071825U (ja) * | 2000-03-16 | 2000-09-22 | 株式会社日本テクマ | 板 材 |
JP2002285111A (ja) * | 2001-03-23 | 2002-10-03 | Dainippon Ink & Chem Inc | ケイ光粘着シートの製造方法 |
RU27024U1 (ru) * | 2002-10-08 | 2003-01-10 | Ященко Александр Владимирович | Внутрисалонный конструктивный элемент транспортного средства |
RU2323955C1 (ru) * | 2006-09-15 | 2008-05-10 | Андриевский Александр Михайлович | Водостойкий люминесцентный пигмент и люминесцентная печатная краска на его основе |
JP4969964B2 (ja) * | 2006-09-22 | 2012-07-04 | リンテック株式会社 | マーキング用粘着シート |
EP1970100B1 (de) * | 2007-03-13 | 2012-05-16 | Lufthansa Technik AG | Fluchtwegmarkierung für ein Flugzeug |
EP1987861B1 (de) * | 2007-05-04 | 2010-06-02 | Lufthansa Technik AG | Fluchtwegmarkierung für ein Flugzeug |
JP2009142998A (ja) * | 2007-12-11 | 2009-07-02 | Dic Corp | 蓄光性化粧材 |
DE102008011405A1 (de) * | 2008-02-27 | 2009-09-10 | Lufthansa Technik Ag | Fluchtwegmarkierung für ein Fahrzeug sowie Verfahren zur Herstellung einer Fluchtwegmarkierung |
-
2009
- 2009-09-01 DE DE102009040042A patent/DE102009040042B4/de active Active
-
2010
- 2010-08-31 CA CA2772683A patent/CA2772683C/en active Active
- 2010-08-31 US US13/393,581 patent/US8636867B2/en active Active
- 2010-08-31 ES ES10771318T patent/ES2400455T3/es active Active
- 2010-08-31 BR BR112012004724-8A patent/BR112012004724B1/pt active IP Right Grant
- 2010-08-31 JP JP2012525939A patent/JP5721716B2/ja active Active
- 2010-08-31 WO PCT/EP2010/005327 patent/WO2011026598A1/de active Application Filing
- 2010-08-31 EP EP10771318A patent/EP2352949B1/de active Active
- 2010-08-31 RU RU2012111207/07A patent/RU2533667C2/ru active
- 2010-08-31 CN CN201080038760.1A patent/CN102597601B/zh active Active
Patent Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
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EP0489561A1 (de) | 1990-12-06 | 1992-06-10 | Minnesota Mining And Manufacturing Company | Gegenstände, die dauerhafte Fluoreszenz zeigen |
WO1996033093A1 (en) * | 1995-04-20 | 1996-10-24 | Saf-T-Glo Aerospace Limited | Emergency lighting |
EP0828657A1 (de) | 1995-04-20 | 1998-03-18 | Saf-t-Glo Aerospace Limited | Notbeleuchtungseinheit |
WO1998004645A1 (en) * | 1996-07-31 | 1998-02-05 | Beele Engineering B.V. | Silicone rubber-containing, afterglowing preparation, product provided therewith and use thereof |
WO2001052224A1 (en) | 2000-01-08 | 2001-07-19 | Stg Aerospace Limited | Emergency lighting |
US20020015309A1 (en) | 2000-07-25 | 2002-02-07 | Stokes Peter David | Emergency lighting |
US7074345B2 (en) | 2001-12-28 | 2006-07-11 | Availvs Corporation | Highly luminous light-emitting material and manufacturing method thereof |
EP1783000A1 (de) * | 2005-11-03 | 2007-05-09 | Saf-t-Glo Limited | Notbeleuchtung |
WO2008110344A1 (de) * | 2007-03-13 | 2008-09-18 | Lufthansa Technik Ag | Fluchtwegmarkierung für ein flugzeug |
DE202007010221U1 (de) * | 2007-07-23 | 2008-12-04 | Agor Gmbh & Co. Kg | Leuchtstreifen |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102012006902A1 (de) * | 2012-04-05 | 2013-10-10 | Lufthansa Technik Ag | Fluchtwegmarkierung mit einem Leuchtstreifen aus photolumineszentem Material |
CN104303222A (zh) * | 2012-04-05 | 2015-01-21 | 汉莎航空技术股份公司 | 包括由光致发光的材料制成的发光条的撤离路线标记 |
US9269284B2 (en) | 2012-04-05 | 2016-02-23 | Lufthansa Technik Ag | Escape route marking with a luminous strip made of photoluminescent material |
DE102012016046B3 (de) * | 2012-08-14 | 2013-12-24 | Lufthansa Technik Ag | Verfahren zum Herstellen einer Fluchtwegmarkierung für Flugzeuge sowie eine solche |
US9702509B2 (en) | 2012-08-14 | 2017-07-11 | Lufthansa Technik Ag | Method for producing an escape route marking for airplanes, and said escape route marking |
DE102014112686B3 (de) * | 2014-09-03 | 2015-04-09 | Lufthansa Technik Aktiengesellschaft | Fluchtwegmarkierung für ein Flugzeug |
WO2016034532A1 (de) | 2014-09-03 | 2016-03-10 | Lufthansa Technik Ag | Fluchtwegmarkierung für ein flugzeug |
Also Published As
Publication number | Publication date |
---|---|
DE102009040042B4 (de) | 2013-08-29 |
CA2772683A1 (en) | 2011-03-10 |
CA2772683C (en) | 2018-02-27 |
BR112012004724B1 (pt) | 2020-06-30 |
EP2352949B1 (de) | 2012-11-28 |
DE102009040042A8 (de) | 2011-06-01 |
CN102597601A (zh) | 2012-07-18 |
ES2400455T3 (es) | 2013-04-10 |
JP5721716B2 (ja) | 2015-05-20 |
JP2013504079A (ja) | 2013-02-04 |
EP2352949A1 (de) | 2011-08-10 |
RU2012111207A (ru) | 2013-10-27 |
US8636867B2 (en) | 2014-01-28 |
US20120282428A1 (en) | 2012-11-08 |
RU2533667C2 (ru) | 2014-11-20 |
BR112012004724A2 (pt) | 2016-03-15 |
DE102009040042A1 (de) | 2011-03-03 |
CN102597601B (zh) | 2016-06-01 |
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