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Automatic instant lighting system for liquid fuel burner

  • US 5,417,565 A
  • Filed: 10/17/1994
  • Issued: 05/23/1995
  • Est. Priority Date: 10/17/1994
  • Status: Expired due to Fees
First Claim
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1. A fuel control mechanism for a liquid fuel burner comprising:

  • a burner,a fuel tank for storing liquid fuel,a feed tube assembly mounted in the fuel tank and having upper and lower ends, the lower end adapted to be immersed in liquid fuel and having fuel inlet means for allowing liquid fuel to flow from the fuel tank into the feed tube assembly, the feed tube assembly having a fuel passage extending from adjacent the lower end of the feed tube assembly to the upper end of the feed tube assembly and an air passage extending from adjacent the upper end of the feed tube assembly to the lower end of the fuel passage,a conduit for conducting fuel from the upper end of the fuel tube assembly to the burner, the conduit including a generator tube positioned adjacent the burner whereby when the generator tube is heated by the burner, fuel within the generator tube is vaporized,a control valve operably connected to the conduit for opening and closing the conduit,regulating means movably mounted in the lower end of the fuel feed tube assembly for movement between a starting position in which the regulating means restricts flow of liquid fuel through the fuel inlet means and a running position in which the regulating means allows unrestricted flow of liquid fuel through the fuel inlet means, the regulating means being responsive to flow of liquid fuel through the fuel inlet means when the control valve is opened for moving to the starting position for restricting the flow of liquid fuel through the fuel inlet means whereby air flows from the upper portion of the fuel tank through the air passage and into the fuel passage and is entrained with liquid fuel which flows through the fuel inlet means into the fuel passage, the regulating means falling to the running position when fuel in the generator tube is vaporized whereby flow of liquid fuel through the inlet means is unrestricted and flow of air through the air passage is discontinued.

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