This invention relates generally to approach lighting systems, and more particularly, to preventing damage to approach lighting systems due to electrical surges.
Airports employ many complex lighting systems that help pilots identify runways and land aircraft. For example, many airports have runway lighting systems (e.g., Runway End Identifier Lists (REIL), Runway Visual Range (RVR), etc.) and approach lighting systems (e.g., High Intensity Approach Lighting Systems with Sequence Flashing Lights (ALSF-2), Medium Intensity Approach Lighting Systems with Runway Alignment Indicator Lights (MALSR), etc. The runway lighting systems generally mark and identify runways. The approach lighting systems generally aid pilots in judging distances and positioning aircraft with respect to the runway. Approach lighting systems generally comprise light bars and/or strobe lights positioned atop of towers or posts that extend away from the runway toward the approach path of aircraft. These lights are generally referred to as “flashers.” An Individual Control Cabinet (an “ICC box”) controls the lights associated with the approach lighting system. For example, the ICC box provides power and control signals to the lights associated with the approach lighting system.
As with all electronics, the ICC box, lights, and wiring associated with an approach lighting system can be damaged by electrical surges. Specific to approach lighting systems, lightning strikes at the towers or posts can cause “upstream” electrical surges. These electrical surges can damage and/or destroy the ICC box, lights, and wiring associated with the approach lighting system. These problems have led to dissatisfaction with current systems.
Embodiments of the inventive subject matter are illustrated in the figures of the accompanying drawings in which:
Introduction
The disclosure provided by this application describes methods, systems, and apparatuses for protecting airport lighting systems from damage due to electrical surges. This disclosure includes three primary zones of protection: a first zone of protection 102, a second zone of protection 104, and a third zone of protection 106.
While
Advanced Transient Protection System
At block 902, box dimensions are determined. Any suitable box dimensions can be used. For example, the box dimensions can the same or different than those depicted in
At block 904, a board is cut for the inner enclosure panel. The board can be any suitable material, such as a plastic or metal board. The board can have any suitable dimensions. For example, the board can be 49.5 cm×53.34 cm×2.54 cm. The flow continues at block 906.
At block 906, the inductor(s) is placed. Any suitable number of inductors can be used. In one example, the inductors are placed using a superior plate and an inferior plate. The superior and inferior plates can take any suitable form and comprise any suitable material. For example, the superior plates can be 10.1 cm×10.1 cm×0.2 cm and be formed from acrylic and metal, and the inferior plates can be 10.1 cm×10.1 cm×0.2 cm and be formed from rubber and metal. The inductors can be placed between the four plates two-by-two and affixed using fasteners (e.g., screws, rivets, bolts, etc.). As one example, the fasteners can be positioned at the corners. The flow continues at block 908.
At block 908, the terminal(s) is placed. Any suitable number and type of terminals can be used. In one example, the terminal(s) is a strip terminal and attached to the inner enclosure panel using fasteners. The flow continues at block 910.
At block 910, the metal-oxide varistor(s) is placed. Any suitable number and type of metal-oxide varistors can be used. In one example, the metal-oxide varistor(s) is attached to the inner enclosure panel using fasteners. The flow continues at block 912.
At block 912, the interlock(s) is placed. Any suitable number and type of interlocks can be used. In one example, the interlock(s) is attached to the inner enclosure plate using fasteners. The flow continues at block 914.
At block 914, the transient voltage suppressor diode(s) is placed. Any suitable number and type of transient voltage suppressor diodes can be used. In one example, the transient voltage suppressor diode(s) is attached to the inner enclosure plate using fasteners. The flow continues at block 916.
At block 916, the ground is placed. The ground can be electrically coupled to some or all of the components of the ATPS in series or in parallel. The flow continues at block 918.
At block 918, the strap is placed. The flow continues at block 920.
At block 920, the input and output holes are placed. Any suitable number of input and output holes can be used. Additionally, the input and output holes can be placed in any suitable location.
Advantageously, an airport lighting system includes one or more lighting elements, a transient protection apparatus, and one or more electrical control cabinets is provided by the approaches described herein. The transient protection apparatus is coupled to the one or more lighting elements. One or more electrical control cabinets are coupled to the transient protection apparatus. Each of the control cabinets produces one or more of control and power signals that are effective to operate the one or more lighting elements. The transient protection apparatus is configured to provide protection for one or more of the electrical control cabinets and the one or more lighting elements from electrical surges.
In aspects, the transient protection apparatus provides protection from electrical surges of up to 10000 volts and up to 10000 amperes. Other examples are possible. In some examples, the transient protection apparatus includes varistors, diodes, and inductors. In other examples, the one or more lighting elements comprise flashers.
In some examples, the transient protection apparatus includes a plurality of varistors arranged in parallel that provide an electrical path through which current flows during an electrical surge. In still other examples, a cable that is configured to ground the one or more lighting elements is provided. In aspects, at least one of a voltage feed line, a trigger line, a return line, a clock line, and a ground line pass through the transient protection apparatus.
In other examples, an airport lighting control system includes a transient protection apparatus and one or more electrical control cabinets. The transient protection apparatus is coupled to one or more lighting elements. The one or more electrical control cabinets are coupled to the transient protection apparatus. Each of the control cabinets produces one or more of control and power signals that are effective to operate the one or more lighting elements. The transient protection apparatus is configured to provide protection for one or more of the electrical control cabinets and the one or more lighting elements from electrical surges. The transient protection apparatus is located between the one or more lighting elements and the electrical control cabinets.
In yet other examples, a transient protection apparatus is coupled between one or more lighting elements and one or more electrical control cabinets. At the one or more electrical control cabinets, one or more of control signals and power signals are produced that are sent through the transient protection apparatus. The one or more of the control signals and power signals are effective to operate the one or more lighting elements. The transient protection apparatus is configured to provide protection for one or more of the electrical control cabinets and the one or more lighting elements from electrical surges.
Although the examples described herein relate to approach lighting systems, use of the ATPS is not so limited. For example, the ATPS described herein can be used with other aviation lighting systems, non-aviation lighting systems, and any system which may benefit from protection from electrical surges.
This application is a U.S. national phase application filed under 35 U.S.C. § 371 of International Application Number PCT/US16/65152, filed Dec. 6, 2016, designating the United States, which claim benefit of United States Provisional Application Number 62/264,083, filed Dec. 7, 2015.
This invention was made with government support under 12 G-005 awarded by the Federal Aviation Administration. The government has certain rights in the invention.
Filing Document | Filing Date | Country | Kind |
---|---|---|---|
PCT/US2016/065152 | 12/6/2016 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2017/100192 | 6/15/2017 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
3858088 | Scarpino | Dec 1974 | A |
4271446 | Comstock | Jun 1981 | A |
4584622 | Crosby | Apr 1986 | A |
4807083 | Austin | Feb 1989 | A |
5327316 | Yi | Jul 1994 | A |
5335160 | Savoca | Aug 1994 | A |
5485151 | Runyon | Jan 1996 | A |
5532897 | Carpenter, Jr. | Jul 1996 | A |
5926115 | Schleder et al. | Jul 1999 | A |
5969642 | Runyon et al. | Oct 1999 | A |
6122157 | Gerlach | Sep 2000 | A |
6304188 | Subak | Oct 2001 | B1 |
6477025 | Goldbach | Nov 2002 | B1 |
6870442 | Suzuki | Mar 2005 | B1 |
7106572 | Girard | Sep 2006 | B1 |
7852234 | Borenstein | Dec 2010 | B1 |
20080001782 | That | Jan 2008 | A1 |
20090073618 | Wang | Mar 2009 | A1 |
20100265625 | Montena | Oct 2010 | A1 |
20130250469 | English | Sep 2013 | A1 |
20170098934 | Laukkanen | Apr 2017 | A1 |
Entry |
---|
International Search Report and Written Opinion of PCT/US2016/065152, dated Feb. 24, 2017, p. 1-6. |
Number | Date | Country | |
---|---|---|---|
20180362186 A1 | Dec 2018 | US |
Number | Date | Country | |
---|---|---|---|
62264083 | Dec 2015 | US |