Safety device for aircraft
US-10293195-B2 · May 21, 2019 · US
US11300053B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11300053-B2 |
| Application number | US-201916591128-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 2, 2019 |
| Priority date | Oct 2, 2019 |
| Publication date | Apr 12, 2022 |
| Grant date | Apr 12, 2022 |
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A flame arrestor system includes a heat exchanger through which a cooling gas flow stream is directed. A zone adjacent the heat exchanger is susceptible to possible flame and through which the cooling gas flow stream is directed. A flame arrestor containing a passage-structure matrix is disposed between the zone and the heat exchanger to quench flame from entering the heat exchanger.
Opening claim text (preview).
What is claimed is: 1. A flame arrestor system comprising: an auxiliary power unit including a gas turbine engine; a duct channeling a cooling gas flow stream into the auxiliary power unit; a heat exchanger through which the cooling gas flow stream is directed; a zone adjacent the heat exchanger in which flame is possible and through which the cooling gas flow stream is directed; and a flame arrestor containing a passage-structure matrix and disposed between the zone and the heat exchanger, wherein the flame arrestor is passive with no moving parts, wherein the flame arrestor includes a structure and passages combination, the passages defined by walls of the structure extending along the gas flow stream and the structure, wherein the walls are configured to quench flame while the passages allow free flow of the cooling gas flow stream through the duct, including in a presence of flame and while the auxiliary power unit remains in operation. 2. The flame arrestor system of claim 1 , wherein the cooling gas flow stream is directed through the flame arrestor. 3. The flame arrestor system of claim 1 , wherein the walls of the structure comprise elongated tube-like structures. 4. The flame arrestor system of claim 1 , wherein the zone comprises an auxiliary power unit compartment. 5. The flame arrestor system of claim 1 , wherein the zone comprises an exhaust duct. 6. The flame arrestor system of claim 1 , wherein the flame arrestor has a first flow area and the heat exchanger has a second flow area smaller than the first flow area, and comprising a header adapting the flame arrestor to the heat exchanger, diverging laterally out from the duct, expanding from the second flow area to the first flow area, and through which the cooling gas flow stream is directed. 7. The flame arrestor of claim 1 , wherein the heat exchanger comprises an oil cooler. 8. The flame arrestor system of claim 1 , wherein the flame arrestor is disposed in the cooling gas flow stream upstream from the heat exchanger and comprising a second flame arrestor disposed in the cooling gas flow stream downstream from the heat exchanger. 9. The flame arrestor system of claim 1 , wherein the zone comprises an eductor plenum. 10. The flame arrestor system of claim 9 , wherein the eductor plenum is configured to educt the cooling gas flow stream through the heat exchanger. 11. The flame arrestor system of claim 1 , wherein the passage-structure matrix comprises at least one of a micro-truss foam material and/or a honeycomb material. 12. A flame arrestor system comprising: an auxiliary power unit including a gas turbine engine; a duct channeling a cooling gas flow stream into the auxiliary power unit; a heat exchanger vulnerable to elevated temperature and through which the cooling gas flow stream is directed; a zone in which flame is possible and through which the cooling gas flow stream is directed; and a flame arrestor containing a passage-structure matrix configured to quench flame, the flame arrestor disposed between the zone and the heat exchanger, wherein the cooling gas flow stream is directed through the flame arrestor, wherein the flame arrestor is passive with no moving parts, wherein the flame arrestor includes a structure and passages combination, the passages defined by walls of the structure extending along the gas flow stream and the structure, wherein the walls are configured to quench flame while the passages allow free flow of the cooling gas flow stream through the duct, including in a presence of flame and while the auxiliary power unit remains in operation. 13. The flame arrestor system of claim 12 , wherein the walls of the structure comprise uniform elongated channel-like structures. 14. The flame arrestor system of claim 12 , wherein the zone comprises an enclosed auxiliary power unit compartment. 15. The flame arrestor system of claim 12 , wherein the zone comprises an exhaust duct. 16. The flame arrestor system of claim 12 , wherein the flame arrestor has a first flow area and the heat exchanger has a second flow area smaller than the first flow area, and comprising a header adapting the flame arrestor to the heat exchanger, diverging laterally out from the duct, expanding from the second flow area to the first flow area, and through which the cooling gas flow stream is directed. 17. The flame arrestor of claim 12 , wherein the heat exchanger comprises an oil cooler. 18. The flame arrestor system of claim 12 , wherein the flame arrestor is disposed in the cooling gas flow stream upstream from the heat exchanger and comprising a second flame arrestor disposed in the cooling gas flow stream downstream from the heat exchanger. 19. The flame arrestor system of claim 12 , wherein the zone comprises an eductor plenum configured to educt the cooling gas flow stream through the heat exchanger. 20. A flame arrestor system for an auxiliary power unit comprising: a duct channeling a cooling gas flow stream into the auxiliary power unit; an oil cooler comprising an aluminum material and through which a cooling air flow stream is directed; an eductor, configured to educt the cooling air flow stream through the oil cooler and to convey combustion gases to an exhaust duct, wherein the eductor comprises a possible flame zone; and a flame arrestor containing a passage-structure matrix configured to quench flame, the flame arrestor disposed between the eductor and the oil cooler, wherein the cooling gas flow stream is directed through the flame arrestor, wherein the flame arrestor is passive with no moving parts, wherein the flame arrestor includes a structure and passages combination, the passages defined by walls of the structure extending along the gas flow stream and the structure, wherein the walls are configured to quench flame while the passages allow free flow of the cooling gas flow stream through the duct, including in a presence of flame and while the auxiliary power unit remains in operation.
Flame traps allowing passage of gas but not of flame or explosion wave · CPC title
for auxiliary power units (APU's) · CPC title
Fire detection or protection; Erosion protection, e.g. from airborne particles · CPC title
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