Emergency lighting arrangement with decentralized emergency power supply for an aircraft

• US 7,378,989 B2
• Filed: 12/30/2004
• Issued: 05/27/2008
• Est. Priority Date: 12/30/2003
• Status: Active Grant

• Current Assignee: Airbus Operations GmbH (Airbus SE)
• Original Assignee: Airbus Deutschland GmbH (Airbus SE)
• Inventors: Rowold, Lars, Wisch, Bodo
• Primary Examiner(s): NGUYEN, HUNG T
• Application Number:
  US11/027,562
• Publication Number:
  US 20050141226A1
• Time in Patent Office: 1,244 Days
• Field of Search: 340/981, 340/693.1, 340/635, 340/636.1, 340/636.12, 340/636.13, 340/687, 340/425.5, 340/815.4, 340/815.45, 340/815.69, 340/332, 362/470, 362/153
• US Class Current: 340/981
• 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: B64D 11/00 Passenger or crew accommodation; Flight-deck installations not otherwise provided for
• 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: B64D 47/02 Arrangements or adaptations of signal or lighting devices
• CPC Class Codes: Y02T 50/40 Weight reduction

Abstract

An emergency lighting arrangement preferably includes plural emergency light units connected to an on-board power supply network of an aircraft, and plural emergency current sources that each include at least one capacitor. Each emergency light unit includes an emergency light emitting element and a control unit that automatically connects the capacitor of the emergency current source to the emergency light emitting element upon the failure of the on-board power supply network. Preferably, the emergency current source including the capacitor is integrated into the emergency light unit. The emergency light unit may further include normal operation light emitting elements selectively connected by the control unit to the on-board power supply network. The control unit switches between normal operation of the normal light emitting elements and charging of the capacitor, and emergency operation in which the capacitor discharges through the emergency light emitting element.

Claims

1. In an aircraft having an on-board power supply network and a plurality of emergency light units arranged distributed in said aircraft,

an improvement wherein:

each one of said emergency light units respectively comprises, incorporated therein as a unit, at least one normal operation light emitting element, at least one emergency light emitting element, at least one capacitor, and a controller that is connected to said power supply network, said at least one capacitor, and said at least one emergency light emitting element;

said controller is adapted to selectively switch between a normal mode when operating power is available from said power supply network and an emergency mode when said operating power is not available from said power supply network;

said normal operation light emitting element is connected directly or through said controller to said power supply network so as to be powered from said power supply network when said operating power is available;

said controller includes a charging circuit adapted to charge said at least one capacitor using said operating power in said normal mode; and

said controller further includes a switching circuit adapted to disconnect said at least one emergency light emitting element from said at least one capacitor in said normal mode, and to connect said at least one emergency light emitting element to said at least one capacitor in said emergency mode so as to illuminate said at least one emergency light emitting element using power supplied from said at least one capacitor in said emergency mode.

2. An emergency lighting arrangement in an aircraft that includes an on board power supply network, said emergency lighting arrangement comprising:

a plurality of emergency light units arranged in a cabin of said aircraft, wherein each one of said emergency light units respectively includes, incorporated therein, at least one emergency light emitting element and at least one normal operation light emitting element; and

a plurality of emergency current sources arranged in said cabin, wherein each one of said emergency current sources respectively includes at least one capacitor and a controller connected thereto;

wherein each one of said emergency current sources is respectively allocated and connected to said at least one emergency light emitting element of at most two of said emergency light units;

wherein, respectively with respect to each said emergency current source, said controller of said emergency current source is connected to said power supply network to detect whether operating power is available from said power supply network, and said controller of said emergency current source is arranged and adapted to automatically connect said at least one capacitor of said emergency current source to said at least one emergency light emitting element to which said emergency current source is allocated, so as to power said at least one emergency light emitting element with electrical energy stored in said at least one capacitor when. said operating. power is not available from said power supply network; and

wherein said at least one normal operation light emitting element of each one of said emergency light units is connected to said power supply network and powered from said power supply network when said operating power is available.

3. The emergency lighting arrangement according to claim 2, wherein each respective one of said emergency current sources is respectively individually allocated to each one of said emergency light units.

4. The emergency lighting arrangement according to claim 3, wherein each one of said emergency light units respectively includes, incorporated therein, said respective one of said emergency current sources.

5. The emergency lighting arrangement according to claim 3, wherein each respective one of said emergency current sources is respectively externally connected to a respective individual one of said emergency light units.

6. The emergency lighting arrangement according to claim 2, wherein each respective one of said emergency current sources is respectively allocated to, and externally connected to, two of said emergency light units.

7. The emergency lighting arrangement according to claim 2, wherein each one of said emergency current sources respectively comprises a plurality of said capacitors connected in series with one another.

8. The emergency lighting arrangement according to claim 2, wherein said at least one capacitor in each one of said emergency current sources has a sufficient energy storage capacity to power said at least one emergency light emitting element connected thereto via said controller for at least 300 seconds.

9. The emergency lighting arrangement according to claim 2, wherein said at least one capacitor in each one of said emergency current sources has a sufficient energy storage capacity to power said at least one emergency light emitting element connected thereto via said controller for at least 600 seconds.

10. The emergency lighting arrangement according to claim 2, wherein each said at least one emergency light emitting element has an operating voltage less than an on-board supply voltage of said operating power of said power supply network.

11. The emergency lighting arrangement according to claim 2, wherein each said at least one emergency light emitting element respectively comprises a light emitting diode (LED).

12. The emergency lighting arrangement according to claim 2, wherein each respective one of said emergency current sources further includes a charging device connected to said at least one capacitor of said respective emergency current source and adapted to be connected to said power supply network, wherein said charging device is adapted to charge said at least one capacitor from said operating power of said power supply network.

13. The emergency lighting arrangement according to claim 12, wherein said charging device is incorporated in said controller of said respective emergency current source.

14. The emergency lighting arrangement according to claim 2, further comprising two power connection lines that connect each said controller to said power supply network.

15. The emergency lighting arrangement according to claim 14, further comprising a manually operable on-off switch interposed in a first one of said power connection lines.

16. The emergency lighting arrangement according to claim 15, wherein said first power connection line is adapted to carry a DC operating voltage of said operating power from said power supply network to said controller and a second one of said power connection lines is adapted to carry a zero volt reference potential, and further comprising a power fault signaling line that connects said controller to said operating voltage of said operating power.

17. The emergency lighting arrangement according to claim 15, wherein said first power connection line is adapted to carry a zero volt reference potential, and wherein said controller is adapted to detect the availability of said operating power directly via a second one of said power connection lines which is adapted to carry a DC operating voltage of said operating power.

18. The emergency lighting arrangement according to claim 2, wherein a respective one of said emergency current sources is allocated to and externally connected to only a neighboring pair of said emergency light units.

19. The emergency lighting arrangement according to claim 2, completely omitting and excluding any and all rechargeable batteries connected to said at least one emergency light emitting element for powering said at least one emergency light emitting element.

20. An emergency lighting arrangement in an aircraft that includes an on-board power supply network, said emergency lighting arrangement comprising:

a signal line adapted to provide a signal indicating a failure of said on-board power supply network;

an emergency power source comprising at least one power storage capacitor, which is connected at least indirectly to said on-board power supply network to be charged by power from said on-board power supply network in a normal operating mode when power is available from said on-board power supply network;

normal operation light emitting elements, which are connected at least indirectly to said on-board power supply network to be powered by power from said on-board power supply network in said normal operating mode; and

at least one emergency light unit that comprises emergency light emitting elements, and a controller that is connected to said on-board power supply network, said signal line, said emergency light emitting elements, and said normal operation light emitting elements;

wherein said controller is adapted to detect said failure of said on-board power supply network and in response thereto to automatically connect said emergency light emitting elements with said power storage capacitor so as to power said emergency light emitting elements.