GB2409023A - Wireless light system with master controller - Google Patents

Wireless light system with master controller Download PDF

Info

Publication number
GB2409023A
GB2409023A GB0328696A GB0328696A GB2409023A GB 2409023 A GB2409023 A GB 2409023A GB 0328696 A GB0328696 A GB 0328696A GB 0328696 A GB0328696 A GB 0328696A GB 2409023 A GB2409023 A GB 2409023A
Authority
GB
United Kingdom
Prior art keywords
led
light source
master controller
pulsed
power consumption
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.)
Granted
Application number
GB0328696A
Other versions
GB0328696D0 (en
GB2409023B (en
Inventor
Peter David Stokes
Dan Leach
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.)
Saf T Glo Ltd
Original Assignee
Saf T Glo Ltd
STG Aerospace Ltd
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 Saf T Glo Ltd, STG Aerospace Ltd filed Critical Saf T Glo Ltd
Priority to GB0328696A priority Critical patent/GB2409023B/en
Publication of GB0328696D0 publication Critical patent/GB0328696D0/en
Priority to US10/945,360 priority patent/US7265684B2/en
Publication of GB2409023A publication Critical patent/GB2409023A/en
Application granted granted Critical
Publication of GB2409023B publication Critical patent/GB2409023B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05BELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B45/00Circuit arrangements for operating light-emitting diodes [LED]
    • 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
    • B64D25/00Emergency apparatus or devices, not otherwise provided for
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F21LIGHTING
    • F21VFUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
    • F21V33/00Structural combinations of lighting devices with other articles, not otherwise provided for
    • H05B37/0272
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05BELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B47/00Circuit arrangements for operating light sources in general, i.e. where the type of light source is not relevant
    • H05B47/10Controlling the light source
    • H05B47/175Controlling the light source by remote control
    • H05B47/19Controlling the light source by remote control via wireless transmission
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60QARRANGEMENT OF SIGNALLING OR LIGHTING DEVICES, THE MOUNTING OR SUPPORTING THEREOF OR CIRCUITS THEREFOR, FOR VEHICLES IN GENERAL
    • B60Q2900/00Features of lamps not covered by other groups in B60Q
    • B60Q2900/30Lamps commanded by wireless transmissions
    • 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
    • B64D2011/0038Illumination systems for cabins as a whole
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F21LIGHTING
    • F21YINDEXING SCHEME ASSOCIATED WITH SUBCLASSES F21K, F21L, F21S and F21V, RELATING TO THE FORM OR THE KIND OF THE LIGHT SOURCES OR OF THE COLOUR OF THE LIGHT EMITTED
    • F21Y2101/00Point-like light sources
    • F21Y2101/02

Landscapes

  • Engineering & Computer Science (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • General Engineering & Computer Science (AREA)
  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Circuit Arrangement For Electric Light Sources In General (AREA)

Abstract

A lighting system comprises a network of devices arranged to communicate wirelessly with a master controller. One or more of the devices is provided with an LED light source. The LED is pulsed in order to reduce power consumption. Preferably, the LED is pulsed at a frequency invisible to the human eye. This frequency may be 100Hz. A variable load factor, which is proportional to the average illumination level, may be applied to the LED. The system may also be operable with a decreasing brightness reduce power consumption. The system may be used in a vehicle, such as an aircraft, as an emergency lighting system.

Description

IMPROVEMENTS IN OR RELATING TO ONBOARD EQUIPMENT
FOR AIRCRAFT AND THE LIKE
This invention concerns improvements in or relating to onboard equipment for aircraft and the like. The invention has particular, but not exclusive application to powered units employed for a variety of purposes, especially battery powered units such as may be used for lighting.
In our co-pending International patent application No. PCT/GB2003/003006 we describe a wireless communication system employing spread spectrum communication for controlling operation of networked communication devices such as battery powered light units for an emergency lighting system to assist evacuation of the aircraft in an emergency.
In our aforesaid application, the devices communicate wirelessly with a master controller and are arranged to cycle between an operable (awake) condition in which they can respond directly or indirectly to a signal transmitted by the master controller and an inoperable (sleep) condition in which they cannot respond to such a signal.
By arranging the devices to re-transmit any broadcast signal, not all the devices have to be within range of the master controller and synchronization of the wake/sleep cycle of the devices is not required. As a result, battery power is conserved and the effective life of the battery can be usefully extended without significantly affecting the overall response of the system to a signal transmitted by the master controller.
In the application to networked devices for emergency lighting, each light unit preferably employs light emitting diodes (LEDs). Typically an array of LEDs is employed requiring a low power consumption whereby the level and duration of light output can be achieved to comply with regulatory requirements using a small battery.
In our co-pending UK patent application No.0321959.9 we describe various improvements in and relating to onboard equipment employed in aircraft and the like especially wireless communication devices of the type described in our aforesaid International patent application.
In particular, we describe ways in which the battery life can be increased.
For example we describe a system for a vehicle such as an aircraft comprising a plurality of networked communication devices arranged to communicate wirelessly with a master controller wherein each device is arranged to cycle between an operable (awake) condition and an inoperable (sleep) condition in which the wake-up time is approximately 1 millisecond or less, preferably 0.5 millisecond or less and/or in which a multi-code generator is employed providing multiple switched outputs and spacing the switched outputs in the code space such that a search time for each device to detect a broadcast signal is reduced.
The present invention seeks to provide improvements to such systems whereby battery life may be further increased.
Thus according to one aspect of the present invention, we provide a system for a vehicle such as an aircraft comprising a plurality of networked communication devices arranged to communicate wirelessly with a master controller wherein one or more devices is provided with a light source comprising at least one LED wherein, in use, power consumption is reduced by pulsing said at least one LED.
Preferably, said at least one LED is pulsed at a frequency so that no pulsing is visible to the human eye. For example, we may employ a pulsing frequency of 100Hz.
Where the light source is employed as part of an emergency lighting system to indicate an escape route to the exit(s) of an aircraft, the current regulations require the system provide illumination for a minimum period of l 0 minutes in an emergency. However, many aircraft operators specify a longer minimum period, typically 20 minutes, so as to provide a safety margin to ensure the system will meet the minimum requirements at the time of use. In some cases, even longer periods of illumination in an emergency such as in the ETOPS [extended twin engined operations] scenario may be desirable.
Each device employs a battery to power the light source which requires the battery to have a minimum residual battery life sufficient to provide the necessary power for this period of illumination. Accordingly, extending the battery life by reducing power consumption through pulsing an LED light source may contribute to a reduction in system costs without compromising safety. In addition, the system may be capable of more than one "switch-on" without replacing the batteries such that the operational capability of the system is not compromised after an inadvertent " switchon " . According to a preferred feature of the invention we may employ pulsing of the light source with a variable load factor. The measured average illumination level is proportional to the load factor of the pulse and varying the load factor enables the light source to be effectively dimmed to produce a saving in power consumption and further extend battery life.
Thus, we may employ a variety of load factors between 10 and 100% of ON time according to the requirements of the system. The resulting
J
savings in battery life are also proportional and an ON time operation for minutes at a pulsed load of 1 No is approximately equivalent to a standard ON time operation for 5 minutes full load.
The ability to dim the illumination has particular benefits when the system is employed to provide emergency lighting. Thus, we may operate the light source at full brightness for an initial period after switching on and then gradually reduce the brightness to a pre-determined minimum. In this way, the operation of the system can be matched to meet the ability of the human eye to dark adapt over time to a reduction in the level of illumination. As a result, power consumption is reduced at the time of use allowing the period of illumination to be increased providing additional safety margins, especially in the ETOPS scenario, while still meeting current rules and regulations.
Thus, according to another aspect of the present invention, we provide a system for a vehicle such as an aircraft comprising a plurality of networked communication devices arranged to communicate wirelessly with a master controller wherein one or more devices is provided with a light source comprising at least one LED wherein, in use, said at least one LED is capable of providing a variable illumination level.
Preferably, the level of illumination is controlled by pulsing the at least one LED with a variable load factor. For example, we may vary the load factor from 10 to looted ON time while pulsing the LED at a frequency that is not visible to the human eye, for example 100Hz, by means of an appropriate logic signal in the control system. In this way, the level of illumination can be varied according to requirements and power consumption can be reduced to provide extended illumination. Thus, when providing emergency lighting, we may gradually reduce the illumination level to match the dark adaptation of the human eye to lower illumination levels without compromising safety.
In the above-described aspects of the invention, each device may have a light source comprising one or more LEDs which may be white LEDs and/or coloured LEDs. A plurality of LEDs may be arranged in an array or take the form of flat panel diffuser as described in our aforementioned UK patent application.
Other features of the construction and operation of the networked communication devices and the systems employing such devices are not described further herein and the reader is directed to our co-pending UK patent application which should be read in conjunction with this application for such details.

Claims (8)

1. A system for a vehicle such as an aircraft comprising a plurality of networked communication devices arranged to communicate wirelessly with a master controller wherein one or more devices is provided with a light source comprising at least one LED wherein, in use, power consumption is reduced by pulsing said at least one LED.
2. A system according to claim 1 wherein said at least one LED is pulsed at a frequency so that no pulsing is visible to the human eye.
3. A system according to claim 2 wherein said at least one LED is pulsed at a frequency of 100Hz.
4. A system according to any preceding claim wherein each device employs a battery to power the light source.
5. A system according to any preceding claim wherein the light source is pulsed with a variable load factor.
6. A system according to claim 5 wherein the load factor is variable between 10 and 100% of ON time
7. A system according to any preceding claim wherein the light source is operable at full brightness for an initial period after switching on and then gradually dimmed to reduce the brightness to a pre- determined minimum.
8. A system of networked communication devices substantially as hereinbefore described.
GB0328696A 2003-09-19 2003-12-11 Improvements in or relating to onboard equipment for aircraft and the like Expired - Fee Related GB2409023B (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB0328696A GB2409023B (en) 2003-12-11 2003-12-11 Improvements in or relating to onboard equipment for aircraft and the like
US10/945,360 US7265684B2 (en) 2003-09-19 2004-09-20 Onboard equipment for aircraft and the like

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0328696A GB2409023B (en) 2003-12-11 2003-12-11 Improvements in or relating to onboard equipment for aircraft and the like

Publications (3)

Publication Number Publication Date
GB0328696D0 GB0328696D0 (en) 2004-01-14
GB2409023A true GB2409023A (en) 2005-06-15
GB2409023B GB2409023B (en) 2007-06-06

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
GB0328696A Expired - Fee Related GB2409023B (en) 2003-09-19 2003-12-11 Improvements in or relating to onboard equipment for aircraft and the like

Country Status (1)

Country Link
GB (1) GB2409023B (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ITRM20080666A1 (en) * 2008-12-15 2010-06-16 Biofly Srl NETWORK OF RADIO-CONTROLLED LIGHT SIGNALING UNITS.
WO2011160903A1 (en) * 2010-06-21 2011-12-29 Siemens Ag Österreich Rail vehicle emergency lighting
RU2574311C2 (en) * 2010-06-21 2016-02-10 Сименс Аг Эстеррайх Emergency lighting for rail vehicle

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3787867A (en) * 1971-04-12 1974-01-22 Automatic Power Division Pennw Navigational aid system
US3894389A (en) * 1972-12-18 1975-07-15 Suwa Seikosha Kk Electronic watch
US5313188A (en) * 1989-10-11 1994-05-17 Bell Sports, Inc. Battery-powered flashing superluminescent light emitting diode safety warning light
US6174073B1 (en) * 1996-01-02 2001-01-16 Bernard Regan Radio frequency remote-controllable lighting system having plurality of lighting units
US20020163316A1 (en) * 1997-08-26 2002-11-07 Lys Ihor A. Methods and apparatus for sensor responsive illumination of liquids
US6703788B1 (en) * 2002-07-12 2004-03-09 John F. Miller Wireless lighting system

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3787867A (en) * 1971-04-12 1974-01-22 Automatic Power Division Pennw Navigational aid system
US3894389A (en) * 1972-12-18 1975-07-15 Suwa Seikosha Kk Electronic watch
US5313188A (en) * 1989-10-11 1994-05-17 Bell Sports, Inc. Battery-powered flashing superluminescent light emitting diode safety warning light
US6174073B1 (en) * 1996-01-02 2001-01-16 Bernard Regan Radio frequency remote-controllable lighting system having plurality of lighting units
US20020163316A1 (en) * 1997-08-26 2002-11-07 Lys Ihor A. Methods and apparatus for sensor responsive illumination of liquids
US6703788B1 (en) * 2002-07-12 2004-03-09 John F. Miller Wireless lighting system

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ITRM20080666A1 (en) * 2008-12-15 2010-06-16 Biofly Srl NETWORK OF RADIO-CONTROLLED LIGHT SIGNALING UNITS.
EP2199206A1 (en) * 2008-12-15 2010-06-23 Biofly S.r.l. Network of radio-controlled light-warning devices
WO2011160903A1 (en) * 2010-06-21 2011-12-29 Siemens Ag Österreich Rail vehicle emergency lighting
CN102947132A (en) * 2010-06-21 2013-02-27 奥地利西门子公司 Rail vehicle emergency lighting
CN102947132B (en) * 2010-06-21 2015-11-25 奥地利西门子公司 Guideway vehicle emergency lighting
RU2574311C2 (en) * 2010-06-21 2016-02-10 Сименс Аг Эстеррайх Emergency lighting for rail vehicle
US9446710B2 (en) 2010-06-21 2016-09-20 Siemens Ag Oesterreich Rail vehicle emergency lighting

Also Published As

Publication number Publication date
GB0328696D0 (en) 2004-01-14
GB2409023B (en) 2007-06-06

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Legal Events

Date Code Title Description
COOA Change in applicant's name or ownership of the application

Owner name: SAF-T-GLO LIMITED

Free format text: FORMER APPLICANT(S): STG AEROSPACE LIMITED

PCNP Patent ceased through non-payment of renewal fee

Effective date: 20181211