Emergency lighting

• US 5,961,072 A
• Filed: 08/25/1995
• Issued: 10/05/1999
• Est. Priority Date: 04/20/1995
• Status: Expired due to Term

• Current Assignee: Saf-T-Glo Limited
• Original Assignee: Saf-T-Glo Limited
• Inventors: Bodle, Peter Winstanley
• Primary Examiner(s): Melius, Terry Lee
• Assistant Examiner(s): CHOP, ANDREA MARIE
• Application Number:
  US08/519,426
• Time in Patent Office: 1,502 Days
• Field of Search: 52/174, 52/177, 52/33, 40/542, 40/570, 362/153, 362/84, 116/205, 116/DIG. 16, 404/9, 404/14, 404/15, 404/16, 244/118.5, 244/118.6
• US Class Current: 244/118.5
• CPC Class Codes: A62B 3/00 Devices or single parts for facilitating escape from buildings or the like, e.g. protection shields, protection screens; Portable devices for preventing smoke penetrating into distinct parts of buildings A62B1/00 takes precedence
• CPC Class Codes: B60Q 3/46 Emergency lighting, e.g. for escape routes
• CPC Class Codes: B60Q 3/47 Circuits; Control arrangements
• CPC Class Codes: B60Q 3/68 using ultraviolet light
• CPC Class Codes: B60Q 3/78 for generating luminous strips, e.g. for marking trim component edges
• CPC Class Codes: B64D 2011/0038 Illumination systems for cabins as a whole
• CPC Class Codes: B64D 25/00 Emergency apparatus or devices, not otherwise provided for parachutes B64D17/00, B64D19/00; jettisoning of fuel tanks or fuel per se B64D37/00; specially adapted for protection against criminal attack, e.g. anti-hijacking systems B64D45/0015 ; safety belts or body harnesses in general A62B35/00; safety belts or body harnesses for land vehicles B60R22/00; jettisonable parts of fuselage facilitating emergency escape B64C
• CPC Class Codes: F21S 4/22 flexible or deformable, e.g. into a curved shape
• CPC Class Codes: G08B 7/066 guiding along a path, e.g. evacuation path lighting strip
• CPC Class Codes: G09F 13/20 with luminescent surfaces or parts luminescent compositions C09K11/00; light sources using luminescence F21K2/00
• CPC Class Codes: G09F 19/22 Advertising or display means on roads, walls or similar surfaces, e.g. illuminated

Abstract

An emergency lighting system for an aircraft has photoluminescent strips mounted on the floor rather than a string of electrical lights. This is a better fail-safe since there is no possibility of a failure in power supply. A channel extrusion is secured to the floor of the aircraft and a photoluminescent strip is held between the channel and a transparent cover member. The photoluminescent strip has two thin layers of photoluminescent material rather on a base layer, rather than being a calendered product. This increases the light output.

Claims

1. An aircraft comprising:

(a) an emergency exit door;

(b) an aisle along a floor of the aircraft leading to said door between a first group of seats disposed along one side of said aisle and a second group of seats disposed along the other side of said aisle;

(c) an emergency exit guidance system including;

(i) a first elongate guide strip fastened to said aisle floor; and

(ii) a second elongate guide strip fastened to said aisle floor;

(d) said first and second elongate guide strips each including

a plurality of sections placed longitudinally in sequence, extending end to end along each of the first and the second guide strips, each section comprising a base support section,

a photoluminescent light-emitting guide section, and

one of a transparent and a translucent cover section;

(e) wherein the cover section of each of said sections has, in an elongate direction of the guide strip, an unstepped generally flat, smooth top surface that extends the length of the section; and

(f) wherein each of said photoluminescent light-emitting guide sections of each of said sections has an upper surface formed as an elongate ribbon having a substantial elongate length in a longitudinal direction of said section and a substantial width in a direction transverse to the longitudinal direction, said photoluminescent guide sections emitting light over substantially their entire upper surface, producing a substantially continuous strip of light, so that said first and second elongate guide strips clearly indicate the sides of the aisle leading to the emergency exit door.

2. The aircraft according to claim 1, wherein each guide strip has a top surface area;

and wherein the light-emitting upper surface of said photoluminescent guide occupies substantially the entire top surface area of said guide strip.

3. The aircraft according to claim 1, wherein said light-emitting upper surfaces of said first and second guide strips extend for substantially the entire length of said guide strips.

4. The aircraft according to claim 1, wherein said cover section is releasably secured to said base support section such that said cover section may be removed from said base support section and readily replaced.

5. The aircraft according to claim 1, wherein said cover section has an upper surface that slopes towards opposite edges of said cover section so that wheeled vehicles may easily pass over the cover section.

6. The aircraft according to claim 1, wherein said photoluminescent light-emitting guide section is an elongate strip with generally parallel sides, said photoluminescent light-emitting guide section producing a substantially continuous track of light.

7. The aircraft according to claim 1, wherein an ultraviolet impermeable layer is provided to at least partially protect the photoluminescent light-emitting guide sections from damaging exposure to ultraviolet light.

8. The aircraft according to claim 1, wherein said photoluminescent light-emitting guide section emits photoluminescent light of a first color, further comprising a marking that overlies a region encompassing at least part of the upper surface of said photoluminescent light-emitting guide section, said marking being of a second color that is different than the first color and comprising a substance that changes the color of photoluminescent light emanating from the region so as to emit light of the second color.

9. The aircraft according to claim 1, further comprising a coloring disposed over said photoluminescent light-emitting guide section, said coloring being translucent to photoluminescent light emitted by said photoluminescent light-emitting guide section so that at least a portion of light emitted thereby is transmitted through said coloring, changing a wavelength spectrum of at least said portion of the light, said changed wavelength spectrum causing at least said portion to be a different color than the photoluminescent light emitted by the photoluminescent light-emitting guide section.

10. The aircraft according to claim 1, in which each of the plurality of sections comprising said first and the second guide strips includes a reflective layer disposed adjacent to the photoluminescent light-emitting guide section.

11. The aircraft according to claim 1, wherein said cover section extends laterally beyond a plan projection of said base support section.

12. The aircraft according to claim 1, wherein a colored filter is introduced between said cover section and said photoluminescent light-emitting guide section, said colored filter changing the color of the light originally emitted by said photoluminescent light-emitting guide section.

13. The aircraft according to claim 1, wherein a pair of spaced-apart branch tracks extend from said first guide strip to said emergency door, each of said branch tracks comprising an elongate base support section fastened to the floor of the aircraft, a photoluminescent light-emitting guide section supported by said base support section, and one of a transparent and a translucent cover section covering said photoluminescent light-emitting guide section.

14. The aircraft according to claim 1 wherein said cover sections are removably mounted on said base support sections.

15. The aircraft according to claim 1, wherein said photoluminescent light-emitting guide section has photoluminescent decay properties such that when charged to an extent sufficient to generate an initial light output of 1300 mcd/m² in an absence of incident light impinging on the photoluminescent light-emitting guide section, the light output of the photoluminescent light-emitting guide section is at least 445 mcd/m² after one minute, at least 30 mcd/m² after ten minutes, and at least 8 mcd/m² after thirty minutes.

16. The aircraft according to claim 1, further comprising elongate photoluminescent guide strips disposed on seats adjacent said aisle.

17. The aircraft according to claim 1, wherein said first and second guide strips include an ultraviolet impermeable layer above said photoluminescent light-emitting guide section to protect said guide section from ultraviolet light.

18. The aircraft according to claim 1, wherein said photoluminescent light-emitting guide section emits light of a first color, further comprising a marking overlying said photoluminescent guide section, said marking being of a second color different than the first color and comprising a substance that changes the color of light emitted by the photoluminescent light-emitting guide section, so that light emanating from the marking is of the second color.

19. The aircraft according to claim 1, wherein said cover sections each have a flat top surface disposed between side surfaces that slope downwardly away from said flat top surface, to facilitate the passage of wheeled trolleys over the cover sections.

20. The aircraft according to claim 1, wherein said cover section includes a flat top surface and a generally vertical side wall, one side of which defines an edge of said flat top surface.

21. The aircraft of claim 1, wherein at least a portion of said photoluminescent light-emitting guide sections are non-directional and do not indicate a preferred direction of travel relative to emergency exit door.

22. An aircraft comprising:

(a) an emergency exit door;

(b) an aisle on a floor of the aircraft leading to said exit door between a first group of seats to one side of said aisle and a second group of seats on the other side of said aisle;

(c) an emergency exit guidance system including;

(i) a first elongate guide strip fastened to said floor along the aisle adjacent said first group of seats; and

(ii) a second elongate guide strip fastened to said floor along the aisle adjacent said second group of seats, generally parallel to and spaced apart from said first elongate guide strip, thereby defining an exit path to said emergency exit door;

(d) said first and second guide strips each comprising;

(i) an elongate base support member having a central section with a flat support surface that is elongate, extending along the length of the guide strip;

(ii) an elongate photoluminescent light-emitting guide extending substantially the length of the guide strip and supported by said flat support surface, said photoluminescent light-emitting guide having a substantially flat, smooth top surface; and

(iii) a plastic cover having a smooth, flat undersurface where it covers said photoluminescent light-emitting guide, said plastic cover transmitting light emitted by the photoluminescent light-emitting guide, said plastic cover extending outwardly beyond the photoluminescent light-emitting guide and being adapted to rest upon the floor of the aircraft, said plastic cover being removably coupled to said elongate base support member; and

(e) said first and second elongate guide strips, with said respective photoluminescent light-emitting guides forming substantially continuous ribbons of light bounding said aisle along the floor and leading to said emergency exit door.

23. The aircraft of claim 22, wherein the central section is generally box-shaped, having two generally parallel side walls, atop which is disposed the flat support surface, extending between top edges of the side walls, said base support section further having two elongate clips disposed outward of the central section and extending adjacent the side walls of the central section, said plastic cover having two elongate flanges extending downwardly from an under surface of the plastic cover, said elongate flanges removably coupling with said elongate clips to attach the plastic cover to said elongate base support member.

24. An aircraft comprising:

(a) an aircraft passenger cabin provided with an emergency exit door;

(b) an aisle floor leading between a first row of seats at one side of said aisle floor and a second row of seats at the other side of said aisle floor;

(c) an emergency exit guidance system comprising;

(i) an elongate guide strip fastened to said aisle floor, said elongate guide strip extending substantially continuously from a passenger holding area of said aircraft passenger cabin to said emergency exit door and comprising;

(1) an extruded elongate base strip fastened to said aisle floor, said base strip having a generally flat central support and elongate flanges disposed on opposite sides of the central support;

(2) an elongate photoluminescent layer formed as a ribbon strip overlying said base strip and supported by an upper, generally planar surface of said central support; and

(3) a cover strip that transmits light, overlying said photoluminescent layer and removably coupled to the elongate flanges, said cover strip protecting the photoluminescent layer, said cover strip being sufficiently supported by the central support, such that a passenger can tread on the cover strip without damaging the photoluminescent layer; and

(d) wherein said removable coupling of said cover strip to said base strip enables said cover strip to be removed while said base strip is still attached to said aisle floor.

25. The aircraft according to claim 24, wherein photoluminescent guide strips are provided on seats disposed adjacent said aisle floor.

26. An aircraft comprising:

(a) an aircraft passenger cabin having an emergency exit door;

(b) an aisle floor leading between a first row of seats at one side of said aisle floor and a second row of seats at the other side of said aisle floor;

(c) an emergency exit guidance system comprising an elongate guide strip fastened to said aisle floor, said elongate guide strip extending substantially continuously from a passenger holding area of said aircraft passenger cabin to said emergency exit door and comprising;

(i) an elongate base strip fastened to said aisle floor;

(ii) an elongate photoluminescent layer overlying said base strip and supported by said base strip; and

(iii) a light-transmissive cover formed of a plastic overlying said photoluminescent layer, a configuration of said base strip, said photoluminescent layer, and said cover enabling a passenger to tread on the cover without damaging the photoluminescent layer;

(d) wherein said guide strip comprises a plurality of sections, including;

(i) a plurality of base strip sections laid end to end;

(ii) a plurality of cover sections laid end to end; and

(iii) a plurality of photoluminescent layer sections extending in a line;

(e) wherein said base strip comprises a channel having side walls that contact and support the cover, and flanges that releasably engage the cover, the photoluminescent layer being held between the cover and said base strip; and

(f) wherein the guide strip has a substantial longitudinal length and a substantial transverse width, said photoluminescent layer occupying substantially the whole longitudinal length of said guide strip, emitting light substantially continuously along the whole longitudinal length of said guide strip, and extending transversely between said flanges that releasably engage the cover, across a transverse width of said guide strip.

27. An aircraft having an aisle extending longitudinally adjacent a plurality of seats, comprising:

(a) an elongate photoluminescent strip having a width, a thickness, and a length, said photoluminescent strip extending longitudinally and continually along the aisle of the aircraft, emitting visible light without being energized by an electrical current, and having a upper surface that is generally flat, continuously, along the length of the elongate photoluminescent strip; and

(b) a light-transmissive plastic material extending continuously over the elongate photoluminescent strip to protect it, said light-transmissive plastic material and said elongate photoluminescent strip forming an integral guide strip having a continuous flat, smooth top surface in the longitudinally extending direction of the elongate photoluminescent strip, an interface between a top of the elongate photoluminescent strip and light-transmissive material also being flat and smooth, said elongate photoluminescent strip emitting light in a continuous track along the aisle of the aircraft.

28. The aircraft of claim 27, further including another integral guide strip extending along the aisle of the aircraft to provide substantially parallel continuous tracks of light that define a path along the aisle of the aircraft.

29. The aircraft of claim 27, wherein the light-transmissive plastic material substantially encapsulates the elongate photoluminescent strip and is attached to the aircraft to secure said integral guide strip in place along the aisle.