This invention relates to the field of gas (e.g., oxygen) flow tubes, and in particular to a gas/oxygen flow tube and a gas/oxygen flow gauge that is illuminated to allow the flow tube or gauge to be viewed in low light conditions to confirm flow.
Supplemental oxygen systems for aviation use are known. Supplemental oxygen systems can be permanently installed in an aircraft or may be portable in order to be moved from aircraft to aircraft as needed. Similarly, oxygen systems are widely used in medical applications and emergency situations, such as for example by firefighters. In each of these circumstances the user of the oxygen system or person responsible for the system may need to verify that the system is indeed providing oxygen, and in particular providing a desired amount of oxygen, even in low light conditions (e.g., while flying at night).
Therefore, there is a need for an illuminated gas (e.g., oxygen) flow tube, and a need for an illuminated gas (e.g., oxygen) flow gauge.
Briefly, according to an aspect of the present invention, a gas (e.g., oxygen) flow tube includes a tube that is at least partially transparent and illuminated, in order to allow visual verification in low light conditions of gas/oxygen flow through the tube.
In one embodiment, the transparent flow tube may include phosphorescent or photoluminescent material at least partially lengthwise surrounding the exterior of the flow tube to illuminate the interior of the tube. The material may include for example PERMALIGHT® photoluminescent material from American Permalight, Inc.
It is contemplated that the flow tube may be illuminated by other passive illuminating materials, or even possibly by active illuminating materials such as by an LED. The LED of course requires a power source, such as a small battery.
These and other objects, features and advantages of the present invention will become more apparent in light of the following detailed description of preferred embodiments thereof, as illustrated in the accompanying drawings.
Significantly, a length of photoluminescent material 28 at least partially lengthwise surrounds the exterior of the flow tube. Advantageously, the material 28 illuminates the interior flow chamber 22 of the tube during low light conditions allowing for the visual verification of gas flow through the tube based upon the location of the specific gravity ball 24. For example, while flying a user must periodically verify that she/he is receiving a sufficient volume of oxygen at altitude (to ensure hypoxia is not an issue) by simply looking at the illuminated flow tube to verify the location of the specific gravity ball 24 within the interior flow chamber 22.
Another advantage of the flow tube illustrated in
Although the present invention has been illustrated and described with respect to several preferred embodiments thereof, various changes, omissions and additions to the form and detail thereof, may be made therein, without departing from the spirit and scope of the invention.
This application claims priority under 35 U.S.C. §119(e) from U.S. provisional application Ser. No. 60/911,395 filed Apr. 12, 2007, which is hereby incorporated by reference.
Number | Date | Country | |
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60911395 | Apr 2007 | US |