Ignition-quenching covers and methods for aerospace applications

{
  "publication_number": "US11571595B2",
  "country": "US",
  "kind": "B2",
  "title": "Ignition-quenching covers and methods for aerospace applications",
  "abstract": "Ignition-quenching covers are configured to quench an ignition event in a combustible environment triggered by an ignition source associated with an ignition-risk structure. Ignition-quenching covers comprise a porous body that includes two or more porous elements and are configured to cover the ignition-risk structure, wherein the ignition-risk structure is associated with a potential ignition source that may produce the ignition event in the combustible environment. The porous body defines passages sized to quench the ignition event. Methods comprise installing a porous ignition-quenching cover over an ignition-risk structure to prevent bulk combustion, e.g., of a fuel vapor in a fuel tank, due to an ignition event associated with the ignition-risk structure.",
  "claims": [
    "1. An ignition-quenching cover configured to quench an ignition event in jet fuel vapor triggered by an electrical arc, a hot particle ejection, or an electrostatic discharge associated with an electrically conductive fastener extending into an interior of a fuel tank, the ignition-quenching cover comprising: a porous body that includes two or more porous elements; wherein the porous body has a proximal cover side and a distal cover side opposite the proximal cover side, wherein the proximal cover side defines a recess that is sized and shaped to receive and engage the electrically conductive fastener extending into the interior of the fuel tank to cover the electrically conductive fastener extending into the interior of the fuel tank, and wherein the porous body defines passages sized to quench the ignition event.",
    "2. The ignition-quenching cover of claim 1, wherein a passage orientation of at least one of the two or more porous elements is different than a passage orientation of at least another of the two or more porous elements.",
    "3. The ignition-quenching cover of claim 1, wherein each porous element is independently selected from the group consisting of a reticulated lattice, a reticulated foam, and an open-cell foam.",
    "4. The ignition-quenching cover of claim 1, wherein the porous body has a mass density of at most 0.5 grams per cubic centimeter (g/cc).",
    "5. The ignition-quenching cover of claim 1, wherein the porous body has an average effective passage diameter that is less than a quenching distance of the jet fuel vapor.",
    "6. The ignition-quenching cover of claim 1, wherein the porous body is configured to prevent a hot particle of greater than a predetermined size from passing through the porous body along a straight line trajectory.",
    "7. The ignition-quenching cover of claim 1, wherein the ignition-quenching cover is configured to dissipate or impede a pressure wave associated with the ignition event.",
    "8. The ignition-quenching cover of claim 1, wherein the ignition-quenching cover is configured to permit a pressure wave associated with the ignition event to travel through the porous body.",
    "9. The ignition-quenching cover of claim 1, wherein the ignition-quenching cover is chemically nonreactive with the jet fuel vapor.",
    "10. The ignition-quenching cover of claim 1, wherein the porous body has a porosity of at least 50%.",
    "11. The ignition-quenching cover of claim 1, wherein the porous body has an average effective pore diameter that is at most 0.3 mm.",
    "12. The ignition-quenching cover of claim 1, wherein the porous body includes struts that define a reticulated lattice.",
    "13. The ignition-quenching cover of claim 12, wherein the struts have a diameter that is at most 75% of an average effective passage diameter of the passages of the porous body.",
    "14. The ignition-quenching cover of claim 12, wherein the struts are hollow and contain a haloalkane.",
    "15. The ignition-quenching cover of claim 1, wherein the porous body has a shape that is configured to avoid a corona discharge at an exterior surface of the ignition-quenching cover.",
    "16. The ignition-quenching cover of claim 1, wherein the recess is configured to thread onto, snap onto, and/or mechanically interlock with the electrically conductive fastener extending into the interior of the fuel tank.",
    "17. The ignition-quenching cover of claim 16, wherein the porous body comprises threads, snap-fit structure, and/or mechanical interlock structure that at least partially defines the recess.",
    "18. A method comprising: installing the ignition-quenching cover of claim 1 over the electrically conductive fastener extending into the interior of the fuel tank, wherein the installing the ignition-quenching cover includes at least partially enclosing the electrically conductive fastener within the recess of the ignition-quenching cover, wherein the fuel tank is a composite structure fuel tank.",
    "19. The method of claim 18, further comprising exposing the electrically conductive fastener and the ignition-quenching cover installed over the electrically conductive fastener to the jet fuel vapor.",
    "20. The method of claim 18, wherein the installing the ignition-quenching cover includes coupling the ignition-quenching cover to at least one of the electrically conductive fastener and the composite structure fuel tank.",
    "21. The method of claim 18, further comprising installing the electrically conductive fastener in a fuel volume of the composite structure fuel tank."
  ],
  "description_excerpt": "The present disclosure relates to systems, apparatuses, and methods for quenching ignition in aerospace applications, such as in connection with aircraft fuel tanks.\n\nIn many situations, devices must operate in potentially hazardous conditions, such as where a fuel mixture may be ignited by uncontrolled operating or environmental conditions. For example, vehicles, including aerospace vehicles, typically operate with a fuel that must be maintained in a safe condition during storage and use. The ignition hazard should be minimized even when the vehicle is subject to uncontrolled events such as an accident, electrical malfunction, a lightning strike, or static electrical discharge. Other applications requiring ignition hazard consideration include fuel transport, fuel storage, mining operations, chemical processing, metal fabrication, power plant construction and operation, and operations which involve combustible particulate such as sawdust, metal, flour, and grain.\n\nIn the aerospace industry, lightning strikes of aircraft are a concern because they could result in electrical arcs and/or heating sufficient to ignite vaporous fuel mixtures. Though lightning passes through aircraft virtually always without resulting harm, newer aircraft designs incorporating composite materials include less metal to shunt and/or dissipate the energy of a lightning strike.\n\nDesign of apparatuses exposed to ignition hazards typically involves reducing the likelihood of ignition, containing the ignition hazard, and/or withstanding the ignition hazard.",
  "cpc": [
    "A62C 3/07",
    "A62C 2/06",
    "A62C 3/06",
    "A62C 3/065",
    "A62C 3/08",
    "A62C 4/00",
    "B64D 37/32",
    "B64D 45/02",
    "F02D 41/22",
    "F02K 9/38",
    "F23Q 25/00",
    "F23Q 7/00",
    "F23Q 7/22",
    "F23Q 7/24",
    "H01T 13/04",
    "H01T 13/06",
    "Y02T 50/40"
  ],
  "ipc": [
    "A62C 2/06",
    "A62C 3/06",
    "A62C 3/07",
    "A62C 3/08",
    "A62C 4/00",
    "B64D 37/32"
  ],
  "assignees": [
    "Boeing Co"
  ],
  "inventors": [
    "Jason Scott Damazo",
    "Eddie Kwon",
    "Arthur C. Day",
    "John Rubrecht Lowell"
  ],
  "filing_date": "2019-11-14",
  "publication_date": "2023-02-07",
  "grant_date": "2023-02-07",
  "priority_date": "2015-07-21",
  "application_number": "US-201916684354-A",
  "family_id": "56360159",
  "cited_by_count": 3,
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