Integral oil tank heat exchanger
US-2017096938-A1 · Apr 6, 2017 · US
US10976214B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10976214-B2 |
| Application number | US-201816190569-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 14, 2018 |
| Priority date | Feb 21, 2018 |
| Publication date | Apr 13, 2021 |
| Grant date | Apr 13, 2021 |
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A tank that may be used in combination with an actuating means such as a pneumatic door actuator includes a first, inner, enclosure positioned and enclosed within a second, outer, enclosure, to provide an enclosed chamber between the inner enclosure and outer enclosure. The pressure in the chamber may be measured with a gauge that does not extend into the inner enclosure. The measured pressure may then be monitored and compared in order to detect a change in pressure and thereby also detect a leak through a wall from the inner enclosure. The tank may also be used to inflate and/or deploy an emergency evacuation slide in an aircraft.
Opening claim text (preview).
The invention claimed is: 1. A tank comprising: a first, inner enclosure provided inside a second, outer enclosure to form an enclosed chamber between the outer surface of the wall of the first enclosure and the inner surface of the wall of the second enclosure, and wherein a first pressurized gas is provided within said first, inner enclosure; and wherein a pressure measuring sensor is positioned relative to said chamber so as to allow the measurement of a pressure within said chamber; wherein a wall of said first, inner enclosure comprises a section that is configured to perforate upon application of an impact force to said section; and wherein the inner enclosure is permanently sealed with said section. 2. A tank comprising: a first, inner enclosure provided inside a second, outer enclosure to form an enclosed chamber between the outer surface of the wall of the first enclosure and the inner surface of the wall of the second enclosure; wherein a first pressurized gas is provided within said first, inner enclosure; and wherein a pressure measuring sensor is positioned relative to said chamber so as to allow the measurement of a pressure within said chamber; and further comprising: a pressure regulator that is integrally formed with said tank. 3. The tank of claim 2 , wherein said pressure regulator includes a first end positioned internally to said inner enclosure and an opposite, second end positioned at an exit of said inner enclosure, and wherein said second end comprises a section that is configured to perforate upon application of said impact force to thereby open said exit. 4. The tank of claim 3 , wherein said section that is configured to perforate comprises a membrane. 5. The tank of claim 1 wherein said tank is connectable to an actuating system to allow said first pressurized gas to flow from an exit of said first enclosure of said tank to said actuating system. 6. The tank of claim 1 , wherein said first enclosure and/or said second enclosure are made by an additive manufacturing method. 7. The tank of claim 1 , wherein said pressure sensor comprises a membrane and a strain gauge and wherein said membrane is made by an additive manufacturing method. 8. The tank of claim 7 , wherein said tank is a pneumatic tank connectable to a pneumatic door actuating mechanism. 9. The tank of claim 7 , wherein said tank is a pneumatic tank connectable to an aircraft inflatable evacuation slide. 10. A method of detecting a leak through a wall of the inner enclosure or outer enclosure of a tank as recited in claim 1 , said method comprising one of: using said pressure measuring sensor to measure the pressure in said chamber and detecting a change in said pressure over time, said change in pressure over time indicating said leak; comparing the pressure within said chamber to a pressure outside of said chamber; and comparing the pressure within said chamber to a threshold or thresholds to detect an increase or decrease in said pressure within said chamber, said increase or decrease indicating said leak. 11. A method for manufacturing a pneumatic tank comprising: forming a first, inner enclosure within a second, outer enclosure, to provide an enclosed chamber between the first enclosure and the second enclosure, and providing a pressure measuring sensor positioned relative to said chamber so as to allow for the measurement of a pressure within said chamber. 12. The method of claim 11 , further comprising: forming said first and second enclosures and a membrane of said pressure measuring sensor by an additive manufacturing method.
Closures, e.g. cap, breakable member ({for autoclaves B01J3/03}; closures for {large} containers in general B65D {B65D90/54}; {for pressure vessels in general F16J13/00}) · CPC title
Pressure difference · CPC title
pierceable · CPC title
Air · CPC title
Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge (pressurised apparatus for purposes other than storage, see the relevant subclasses such as A62C, B05B; associated with vehicles, see the appropriate subclass of classes B60 - B64; pressure vessels in general F16J12/00 {; autoclaves B01J3/04; tank vehicles B60P3/22; railway tank wagons for carrying fluent materials B61D5/00; accumulators for supplying fluid under pressure F15B1/04; liquefied gas stoves F24C3/00}) · CPC title
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