This invention generally relates to a venting system, and more specifically to a protective venting system for self-contained marine and aviation lighting equipment.
Self-contained marine and aviation lighting equipments relates to those lighting equipments that can operate autonomously with minimum human intervention for a long period of time, e.g. several months or even years. These lighting equipments are generally powered by solar panel charged rechargeable batteries. The capability to maintain their performance during a predetermined lifespan is a top priority for this kind of lighting equipments. However, changing environment conditions, such as temperature, dust, salt, and moisture may considerably impact the performance of these lighting equipments. For example, rain or splashing sea water can cool down the enclosure of the lighting equipment dramatically, causing a vacuum of 150 mbar or more inside the enclosure. To equalize the pressure, air and moisture are drawn through the seal into the enclosure where the moisture condenses on the cooler inner walls. This can considerably impair the performance of the electronic system of the lighting equipment. In another aspect, the rechargeable battery may release battery gases such as hydrogen and oxygen in the event that the battery is abused or over-charged. Buildup of these battery gases in the enclosure of the lighting equipments may pose an explosion hazard.
There thus exists a need of a protective venting system for self-contained marine and aviation lighting equipments. The venting system should be capable of preventing battery gas buildup in the enclosure of the lighting equipment as well as maintaining its pressure equilibrium with the outside environment. In addition, the venting system should be water and dust proof to prevent debris or ice buildup.
The accompanying figures, where like reference numerals refer to identical or functionally similar elements throughout the separate views and which together with the detailed description below are incorporated in and form part of the specification, serve to further illustrate various embodiments and to explain various principles and advantages all in accordance with the present invention.
a illustrates an exemplary marine lighting equipment with the disclosed protective venting system;
b illustrates the structure of the protective venting system;
c is a vertical cross-section view of the protective venting system.
Skilled artisans will appreciate that elements in the figures are illustrated for simplicity and clarity and have not necessarily been drawn to scale. For example, the dimensions of some of the elements in the figures may be exaggerated relative to other elements to help to improve understanding of embodiments of the present invention.
Before describing in detail embodiments that are in accordance with the present invention, it should be observed that the embodiments reside primarily in combinations of method steps and apparatus components related to a protective venting system for self-contained marine and aviation lighting equipment. Accordingly, the apparatus components and method steps have been represented where appropriate by conventional symbols in the drawings, showing only those specific details that are pertinent to understanding the embodiments of the present invention so as not to obscure the disclosure with details that will be readily apparent to those of ordinary skill in the art having the benefit of the description herein.
In this document, relational terms such as first and second, top and bottom, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. The terms “comprises,” “comprising,” or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. An element proceeded by “comprises . . . a” does not, without more constraints, preclude the existence of additional identical elements in the process, method, article, or apparatus that comprises the element.
Referring to
The structure of the protective venting system 108 is further illustrated in
In the foregoing specification, specific embodiments of the present invention have been described. However, one of ordinary skill in the art appreciates that various modifications and changes can be made without departing from the scope of the present invention as set forth in the claims below. Accordingly, the specification and figures are to be regarded in an illustrative rather than a restrictive sense, and all such modifications are intended to be included within the scope of present invention. The benefits, advantages, solutions to problems, and any element(s) that may cause any benefit, advantage, or solution to occur or become more pronounced are not to be construed as a critical, required, or essential features or elements of any or all the claims. The invention is defined solely by the appended claims including any amendments made during the pendency of this application and all equivalents of those claims as issued.
This application claims an invention which was disclosed in Provisional Patent Application No. 60/869,180, filed Dec. 8, 2006, entitled “Protective Venting System for Self-Contained Marine and Aviation Lighting Equipment.” The benefit under 35 USC § 119(e) of the above mentioned U.S. Provisional Applications is hereby claimed, and the aforementioned applications are hereby incorporated herein by reference.
Number | Date | Country | |
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60869180 | Dec 2006 | US |