The present invention relates generally to lighting systems, in particular to obstruction lighting systems utilizing light emitting diodes.
The Federal Aviation Administration (FAA) requires that obstructions to aircraft navigation, such as towers, cables and tall buildings be fitted with visibly perceivable elements to render these structures highly visible to approaching aircraft. FAA Advisory Circular 150/5345-43 forms a specification of technical requirements for these lights in the United States. Within Advisory Circular 150/5345-43 there exists a requirement for a medium-intensity flashing red obstruction light system, designated the “L-864” and a medium-intensity flashing white obstruction light, designated the “L-865.” These obstruction lights are to be placed in accordance with a set plan at levels on all obstructions that are potential hazards to air navigation.
For the L-864 obstruction light, at all radials throughout a 360 degree azimuth, there must be a peak effective intensity of 2,000±25 percent candela. There must also be a minimum effective intensity of 750 candela throughout a minimum vertical beam spread of 3 degrees. For the L-865 obstruction light, at all radials throughout a 360 degree azimuth, there must be a peak effective intensity of 20,000±25 percent candela during operation at day and twilight conditions, and 2,000±25 percent candela during night conditions. The L-865 obstruction light also includes a minimum vertical beam spread of 3 degrees.
A drawback of these obstruction lights is that they typically utilize incandescent lamps, which have a relatively limited service life. Consequently, the incandescent lamps require frequent replacement. Since the obstruction lights are mounted atop tall structures, replacing these lamps can be inconvenient, time-consuming, expensive and even dangerous. Utilizing light emitting diodes (LEDs) as a light source in obstruction lights overcomes many of these drawbacks. However, LEDs present new design challenges.
Another drawback of conventional obstruction lights is light pollution. Light pollution as it relates to obstruction lighting may be generally defined as the emission of light outside the band specified by Advisory Circular 150/5345-43. Light pollution can be an annoyance, particularly when the obstruction light is proximate to residential areas. In some cases light pollution can cause problems such as sleep deprivation or the blocking of an evening view.
In an optical system for an obstruction light, one approach for arranging LED light sources is to orient them vertically, aimed outwardly from the light assembly. However, shaping multiple light sources into a tight continuous horizontal beam requires a lens, which is less efficient than a reflector. Additionally, the LED junctions thusly configured are more vulnerable to damage due to lightning effects.
Another approach is to mount the LEDs so they are oriented horizontally and aimed upwardly, using a reflector to shape and redirect the light outwardly. In this configuration the reflector is very efficient and also acts as a lightning mediator. Another advantage of this arrangement is that it minimizes direct-light emissions from the LEDs shining downwardly from the obstruction light, which may be considered a neighborhood annoyance.
Orienting LEDs so that they are aimed downwardly is also desirable since it offers more efficient cooling of the LEDs and makes servicing of the LEDs more convenient. However, this arrangement is problematic because it inherently directs some of the LED light toward the neighborhood below the obstruction light.
Moreover, horizontally orienting LEDs and aiming them toward a reflector is undesirable, as this directs the brightest part of the LED beam toward the flatter area of the reflector, thereby reducing beam focus.
An obstruction light utilizing LEDs as a light source is disclosed according to an embodiment of the present invention. The LEDs are oriented and aimed toward a reflector so as to minimize downwardly-directed light while also enhancing the characteristics of the desired light output from the reflector.
One object of the present invention is a lighting system comprising a reflector having a plurality of reflecting surfaces. The plurality of reflecting surfaces have at least one optical axis, and the reflecting surfaces further include a linearly projected cross-section along a respective linear axis. In one embodiment, the linearly projected cross-section of the reflecting surfaces comprise a substantially conic shape. A plurality of light emitting diodes (LEDs) are positioned in a line generally parallel to the linearly projected cross-section of the plurality of reflecting surfaces. The LEDs are oriented relative to an associated reflecting surface such that a central light-emitting axis of the plurality of LEDs is angled relative to the at least one optical axis of the associated reflecting surface at about 45°. The reflecting surfaces redirect and collimate a light output of the plurality of LEDs at an angle of about 45° with respect to the central light emitting axis of the plurality of LEDs.
Further features of the inventive embodiments will become apparent to those skilled in the art to which the embodiments relate from reading the specification and claims with reference to the accompanying drawings, in which:
The general arrangement of a lighting system 10 usable as an obstruction light, among other purposes, is shown in
With continued reference to
In some embodiments of the present invention reflecting surface 24 is neither concave or convex along linear axis 28. In other embodiments reflecting surface 24 may be concave along linear axis 28. In still other embodiments reflecting surface 24 may be convex along linear axis 28.
Each reflecting surface 24 has an associated optical axis 34. In one embodiment, each reflecting surface 24 reflects a beam of light having an angular distribution that is horizontally symmetric to the associated optical axis 34, i.e., symmetric about the associated optical axis in directions along linear axis 28.
Reflector 22 may be made from any suitable material including, without limitation, metal or a reflective material. Non-limiting examples of materials for reflector 22 include highly-polished metal, a coated (i.e., “metalized”) metal or non-metal substrate, and a reflective film applied to a metal or non-metal substrate.
For each reflecting surface 24, optic 12 comprises at least one associated LED 32. LED 32 typically emits light in a hemisphere centered and concentrated about central light-emitting axis 30. LED 32 is positioned relative to the associated reflecting surface 24 such that central light-emitting axis 30 of the LED is angled at a predetermined angle θ2 relative to the optical axis 34 associated with the reflecting surface 24. In a preferred embodiment, θ2 has a value of about 45°. In some embodiments of the present invention, the about 45° value has a tolerance of ±15°, i.e., from 30° to 60°.
With reference now to
As shown in
Referring again to
Although
In some embodiments of the present invention the plurality of reflecting surfaces 24 of reflector 22 may be connected together. Accordingly, reflecting surfaces 24 may be made as separate pieces and joined together. Alternatively, reflecting surfaces 24 may be formed as a unitary piece.
A view in section of lighting system 10 is shown in
LEDs 32 may be any type of light emitting diode suitable for use with lighting system 10. As a non-limiting example, LEDs 32 may be arranged in a linear or non-linear array (
By positioning LEDs 32 in the manner shown in
In some embodiments of the present invention LEDs 32 are mounted on detachable, insulated metal substrates 44 to form light source assemblies that easily plug into mating connectors situated in lighting system 10. Such non-leaded assemblies reduce the labor associated with replacing the LEDs and eliminate service problems associated with wire-lead breakage.
For example, substrates 44 may include a connector portion 46A that is configured to electrically and mechanically couple to a mating connector 46B mounted to heat sink 40. Connectors 46A, 46B are preferably selectably detachable. Thus, in the event that one or more substrates 44 are replaced, heat sink 40 may be detached from lighting system 10 by removing a fastener 48 from a threaded receptacle in housing 16 to expose substrates 44. The select substrates 44 are detached from their respective mating connectors 46B and replaced. Once the select substrate(s) 44 are replaced, heat sink 40 is placed onto lighting system 10 and fastener 48 is re-installed, securing the heat sink to the lighting system.
In some embodiments of the present invention lighting system 10 includes at least one auxiliary lighting assembly having one or more auxiliary LEDs 50, preferably configured to emit light upwardly from lighting system 10. In some embodiments auxiliary LED 50 may differ from LEDs 32. For example, auxiliary LED 50 may be configured to emit infrared light to alert flight crews operating with night vision imaging systems (NVIS).
With reference to
A driver 56 of control system 52 controls the operation of LEDs 32, 50, controlling the voltage and/or current supplied to the LEDs, and detecting and compensating for faults within the LEDs. Driver 56 may also control the flash rate of LEDs 32, 50 in accordance with control signals provided by controller 54. Furthermore, when LEDs 32, 50 are to be turned off driver 56 may remove power supplied to the LED in accordance with control signals provided by controller 54.
Control system 52 may utilize a local or remote global positioning satellite (GPS) receiver 58, a clock 60, and so on to determine sundown and sunup to automatically turn lighting system 10 on and off accordingly and/or control the brightness of the output light via driver 56. In one embodiment of the present invention an ambient light sensor 62 may be utilized for this purpose, providing to controller 54 an electrical signal corresponding to the level of ambient light proximate lighting system 10. Ambient light sensor 62 may likewise be used as a control signal for control system 52 to dim the light output from LEDs 32 during periods of low-light, such as during inclement or overcast weather.
Control system 52 may also include a one-way or two-way communication link 64 to facilitate remote control and monitoring of the status and operation of lighting system 10. Communication link 64 may include one or more of a radio frequency or light-based communication link.
In some embodiments of the present invention lighting system 10 may include an Automatic Dependent Surveillance-Broadcast (ADS-B) surveillance system 66 to detect aircraft equipped with ADS-B capability. ADS-B is an anti-collision technology being adopted by aircraft operators to provide airborne collision avoidance capability. ADS-B is the linchpin technology of the Federal Aviation Administration's (FAA's) current “NextGen air traffic management system.” ADS-B is intended to enable the FAA to safely increase the density of air traffic while simultaneously reducing aircraft fuel consumption, allowing more dynamic and direct routing, improving anti-collision capability in aircraft, and enabling information exchange with airborne aircraft. At the core of the ADS-B system is a “heartbeat” that is transmitted by outfitted aircraft providing the aircraft's identification, location, velocity, and other relevant state data. Ground-based and airborne ADS-B transceivers can receive this heartbeat and accurately determine an aircraft's position, direction, and velocity in a timely manner.
ADS-B system 66 may include sensing apparatus within or proximate to lighting system 10 to detect “targets,” i.e., vehicles in the vicinity of a predetermined area, or an object or structure and then generate data relating to the targets. Alternatively, ADS-B system 66 may receive target data from sources remote from lighting system 10, either directly or via communication link 64. In various embodiments of the present invention ADS-B system 66 may utilize, without limitation, radar, sonar and proximity sensors to generate target data. ADS-B system 66 may also utilize information obtained on the Internet to generate target data. In fact, ADS-B system 66 may include or utilize any type of system, device or apparatus now known or later invented having a target detection capability. It is intended that ADS-B system 66 be configured with the ability to detect a target vehicle.
With reference to
A method of using optic 12 or lighting system 10 includes arranging a plurality of reflecting surfaces 24 relative to each other, the reflecting surfaces having a linearly-projected cross-section 28. The method also includes the step of positioning at least one LED 32 relative to at least one of the reflecting surfaces 24, the positioning step angling the central light-emitting axis 30 of the LED relative to the optical axis 34 associated with the reflecting surface 24 at about 45°. The method also comprises transmitting light from LED 32 to the reflecting surface 24. In one embodiment of the method, the about 45° has a tolerance of ±15°.
In one embodiment of the method, the at least one LED 32 comprises a plurality of LEDs, the at least one optical axis 34 comprises a plurality of optical axes, and the positioning step comprises positioning each of the plurality of LEDs relative to a respective one of the plurality of optical axes 34 at about 45°. In one embodiment of the method, each reflecting surface 24 comprises a cross-section projected along a linear axis 28, and the arranging step comprises arranging the plurality of reflecting surfaces 24 relative to each other so that a plurality of the linear axes are angled relative to each other.
While this invention has been shown and described with respect to a detailed embodiment thereof, it will be understood by those skilled in the art that changes in form and detail thereof may be made without departing from the scope of the claims of the invention. For example, although the disclosed invention is described in terms of use as an obstruction light for the purpose of illustration, one skilled in the art will appreciate that the disclosed invention may be utilized to advantage in any suitable type of lighting.
This application claims priority to U.S. provisional application 61/453,944, filed Mar. 17, 2011, U.S. provisional application 61/454,237, filed Mar. 18, 2011, and U.S. provisional application 61/511,872, filed Jul. 26, 2011, the contents of each being incorporated herein by reference.
Number | Name | Date | Kind |
---|---|---|---|
4498004 | Adolfsson et al. | Feb 1985 | A |
4609306 | Loire | Sep 1986 | A |
5155666 | Radford et al. | Oct 1992 | A |
5608290 | Hutchisson et al. | Mar 1997 | A |
5642933 | Hitora | Jul 1997 | A |
5838247 | Bladowski | Nov 1998 | A |
5929788 | Vukosic | Jul 1999 | A |
6022124 | Bourn et al. | Feb 2000 | A |
6070994 | Sebek et al. | Jun 2000 | A |
6183100 | Suckow | Feb 2001 | B1 |
6364506 | Gallo | Apr 2002 | B1 |
6379026 | Petrick | Apr 2002 | B1 |
6464373 | Petrick | Oct 2002 | B1 |
6525668 | Petrick | Feb 2003 | B1 |
6561689 | Kidd et al. | May 2003 | B1 |
6601970 | Ueda et al. | Aug 2003 | B2 |
6637921 | Coushaine | Oct 2003 | B2 |
6679618 | Suckow et al. | Jan 2004 | B1 |
6705745 | Pederson | Mar 2004 | B1 |
6793372 | Wehner et al. | Sep 2004 | B2 |
6932496 | Rizkin et al. | Aug 2005 | B2 |
6948830 | Petrick | Sep 2005 | B1 |
6991351 | Petrick | Jan 2006 | B1 |
7040782 | Mayer | May 2006 | B2 |
7079041 | Fredericks et al. | Jul 2006 | B2 |
7160004 | Peck | Jan 2007 | B2 |
7163322 | Tatewaki et al. | Jan 2007 | B2 |
7236105 | Brenner et al. | Jun 2007 | B2 |
7237929 | Stahl | Jul 2007 | B2 |
7497593 | Wang | Mar 2009 | B2 |
7568821 | Peck et al. | Aug 2009 | B2 |
7578600 | Czajkowski | Aug 2009 | B2 |
7604384 | Peck | Oct 2009 | B2 |
7658513 | Peck | Feb 2010 | B2 |
RE41153 | Mork et al. | Mar 2010 | E |
7758210 | Peck | Jul 2010 | B2 |
7783427 | Woodell et al. | Aug 2010 | B1 |
7791497 | Clerk | Sep 2010 | B2 |
7832908 | Peck et al. | Nov 2010 | B2 |
7908079 | Dabney et al. | Mar 2011 | B1 |
RE42708 | Mark et al. | Sep 2011 | E |
8033683 | Fields | Oct 2011 | B2 |
8096677 | Fields et al. | Jan 2012 | B2 |
8591073 | Peck et al. | Nov 2013 | B2 |
20010015899 | Kondo et al. | Aug 2001 | A1 |
20040004836 | Dubuc | Jan 2004 | A1 |
20040057234 | Mohacsi | Mar 2004 | A1 |
20040057244 | Amano | Mar 2004 | A1 |
20040145910 | Lisowski | Jul 2004 | A1 |
20040196646 | Machi et al. | Oct 2004 | A1 |
20050015202 | Poe et al. | Jan 2005 | A1 |
20050094393 | Czajkowski | May 2005 | A1 |
20050157490 | Klose | Jul 2005 | A1 |
20060007012 | Machi et al. | Jan 2006 | A1 |
20060012990 | Walser et al. | Jan 2006 | A1 |
20060198141 | Peck et al. | Sep 2006 | A1 |
20060291209 | Booth et al. | Dec 2006 | A1 |
20080192480 | Rizkin et al. | Aug 2008 | A1 |
20090115637 | Naimer et al. | May 2009 | A1 |
20090201190 | Huthoefer et al. | Aug 2009 | A1 |
20090219715 | Peck et al. | Sep 2009 | A1 |
20100027281 | Waters et al. | Feb 2010 | A1 |
20100084979 | Burton et al. | Apr 2010 | A1 |
20100194603 | Wobben | Aug 2010 | A1 |
20100244748 | Haab et al. | Sep 2010 | A1 |
20100253546 | Ibrahim et al. | Oct 2010 | A1 |
20100259929 | Henri et al. | Oct 2010 | A1 |
20110018439 | Fabbri et al. | Jan 2011 | A1 |
20110051421 | Chew | Mar 2011 | A1 |
20110058370 | Datz et al. | Mar 2011 | A1 |
20110121734 | Pape | May 2011 | A1 |
20110194283 | Roer | Aug 2011 | A1 |
20110235322 | Fields et al. | Sep 2011 | A1 |
20110241926 | Laufer | Oct 2011 | A1 |
20110305014 | Peck | Dec 2011 | A1 |
20120300449 | Fields | Nov 2012 | A1 |
20140036502 | Peck et al. | Feb 2014 | A1 |
Number | Date | Country |
---|---|---|
201636748 | Nov 2010 | CN |
1231109 | Aug 2002 | EP |
1698823 | Apr 2010 | EP |
2199206 | Jun 2010 | EP |
2001243821 | Sep 2001 | JP |
2009084049 | Jul 2009 | WO |
2009090185 | Jul 2009 | WO |
2009133326 | Nov 2009 | WO |
2012039776 | Mar 2012 | WO |
Entry |
---|
Avionics Today Article, NAV Canada Extends ADS-B Coverage, Mar. 30, 2012, www.aviationtoday.com/av/commercial/NAV-Canada-Extends-ADS-B-Coverage—76059.html#Umkns1M1nfs. |
European Search Report, Application EP12160211, mailed Aug. 7, 2013. |
Urgent Communications, View From the Top Blog, “A New Development in Tower-Aviation Safety”, pp. 1-3, Mar. 7, 2013, http://urgentcomm.com/blog/new-development-tower-aviation-safety. |
Federal Communications Commission, FCC 13-30 Report and Order, promoting aviation safety, Mar. 1, 2013. |
ADS-B Technologies, Product menu, “Mobile & Tactical ADS-B Systems”, Nov. 29, 2011, http://www.ads-b.com/LISTgallery3.htm. |
Patriot Technologies, LLC, Lori Huthoefer, Power Point Presentation, “The Runway Occupancy Warning System (ROWS)”, Jul. 18, 2011, www.patriot-technologies.com. |
Citation Excel, Informational Flyer, “Runway Status Lights”, Jun. 11, 2011, www.ce560xl.com/files/RWSL.pdf. |
Jeppesen, Jepp View 3.631, Informational Flyer, “Pilot Guide to Runway Status Lights (RWSL) Logan International Airport (BOS)”, Jun. 30, 2010. |
Roger-Wilco, Life Around Runways by Steve, “New Tools in the Arsenal to Prevent Runway Incursions—RWSL and Faros”, Mar. 16, 2010, www.roger-wilco.net. |
Lincoln Laboratory Journal, James R. Eggert, Bradley R. Howes, Maria Picardi Kuffner, Harald Wilhelmsen, and D. Jonathan Bernays, “Operational Evaluation of Runway Status Lights”, pp. 123-146, vol. 16, No. 1, 2006. |
NASA, J. Timmerman, Rockwell Collins, CR-2001-211242 Report, “Runway Incursion Prevention System ADS-B and DGPS Data Link Analysis Dallas—Ft. Worth International Airport”, Nov. 2001, Cedar Rapids, Iowa. |
Dialight Corp., Product datasheet for D164 Series LED Red Beacon, printed Jan. 21, 2011. |
Data Sheet, Orga Model AOL1000SA High Intensity Aeronautical Obstruction Light. |
Promotional Sheet, Excelitas Technologies “Lighting Solutions for Safety and Security”. 4 pages. |
European Search Report, Application EP12182139, mailed Dec. 12, 2013. |
Number | Date | Country | |
---|---|---|---|
20120236558 A1 | Sep 2012 | US |
Number | Date | Country | |
---|---|---|---|
61453944 | Mar 2011 | US | |
61454237 | Mar 2011 | US | |
61511872 | Jul 2011 | US |