Portable gas-fired forced-draft heater

• US 4,762,488 A
• Filed: 02/02/1987
• Issued: 08/09/1988
• Est. Priority Date: 05/20/1985
• Status: Expired due to Fees

• Current Assignee: City of Lander, Leader (Crowley Holdings Preferred LLC), Lander Valley Ventures
• Original Assignee: Thaddeus A. Schilling
• Inventors: Schilling, Thaddeus A.
• Primary Examiner(s): Scott, Samuel
• Assistant Examiner(s): KAMEN, NOAH P
• Application Number:
  US07/010,009
• Time in Patent Office: 554 Days
• Field of Search: 431/8, 431/116, 431/170, 431/171, 431/172, 431/187, 431/344, 431/347, 431/348, 431/350, 431/353, 431/354, 431/355, 431/203, 432/222, 432/223, 110/260
• US Class Current: 431/350
• CPC Class Codes: F23D 14/64 with injectors
• CPC Class Codes: F23D 14/70 Baffles or like flow-disturbing devices
• CPC Class Codes: F23D 14/76 Protecting flame and burner parts
• CPC Class Codes: F24C 3/062 stoves
• CPC Class Codes: F24C 3/14 with special adaptation for travelling, e.g. collapsible
• CPC Class Codes: F24H 3/0488 using fluid fuel
• CPC Class Codes: Y02B 30/00 Energy efficient heating, ventilation or air conditioning [HVAC]

Abstract

A portable gas-fired forced-draft heater has a burner assembly mounted in a tube coupled to the intake port of a motor-driven blower. The burner operates in a stream of high velocity air which flows past the burner to the blower. The burner includes shrouds which cooperate with a fuel and air mixing nozzle to enable fuel to be burned efficiently and reliably over a wide range of fuel flow rates to the burner. A flame stabilization surface is spaced appropriately from the nozzle to enable reliable ignition of the fuel-air mixture. A controlled portion of the warm gases passing through the blower is routed to a receptacle for a fuel container to maintain pressure in the container as the preferably liquified gas fuel is consumed during operation of the heater.

Claims

1. Combustion apparatus for burning a gaseous fuel-air mixture and adapted for use within a surrounding high velocity air stream, the apparatus comprising:

(a) a fuel and air mixing nozzle assembly for mixing fuel supplied to the assembly with air, for creating an essentially entirely gaseous mixture of fuel and air, and for discharging that mixture along a discharge axis of the assembly to a combustion zone downstream of the nozzle assembly and surrounded by the air stream, the assembly being adapted for connection to a source of fuel for supply of fuel from the source under pressure to the assembly, the assembly having a discharge end on said axis through which the mixture is discharged to the combustion zone, and

(b) spaced upstream and downstream combustion zone shroud means for creating in the combustion zone, during the existence of said air stream therepast, a region of relatively nonturbulent gas having a pressure higher than the pressure in said air stream and in which combustion of the fuel air mixture can occur, the shroud means being disposed along said axis respectively (1) upstream of and adjacent the nozzle assembly discharge end and (2) substantially at a downstream end of the combustion zone and including plate means disposed substantially normal to the axis upstream and downstream of the discharge end of the nozzle assembly,

(c) the apparatus being characterized by the absence, between the upstream and downstream shroud means, of physical structure between the high velocity air stream and the combustion zone and the region of relatively nonturbulent gas therein.

2. Apparatus according to claim 1 wherein the downstream shroud means defines openings therethrough for controlled passage of gas therethrough from said relatively nonturbulent higher pressure region.

3. Apparatus according to claim 2 wherein the upstream shroud means defines openings therethrough for controlled passage of air therethrough.

4. Apparatus according to claim 3 wherein the aggregate area of the openings in the downstream shroud means is greater than that of the openings in the upstream shroud means.

5. Apparatus according to claim 3 wherein the upstream shroud means comprises a substantially circular plate disposed substantially normal to said axis upstream of the discharge end of the nozzle assembly and a wall member secured to the rim of the plate about the periphery of the plate and extending a selected distance in a downstream direction from the plate substantially parallel to the axis, and the openings in the upstream shroud means are defined in the plate proximate the periphery thereof.

6. Apparatus according to claim 5 wherein said selected distance is at least about substantially one-half the diameter of the plate.

7. Combustion apparatus for burning a gaseous fuel-air mixture and adapted for use within a surrounding high velocity air stream, the apparatus comprising:

(a) a fuel and air mixing nozzle assembly for mixing air with a fluid fuel supplied to the assembly at a rate within a substantial range of fuel flow rates, for creating an essentially entirely gaseous mixture of fuel and air having substantially a selected ratio of fuel to air, and for discharging that mixture along a discharge axis of the assembly to a combustion zone downstream of the nozzle assembly and surrounded by the air stream, the assembly being adapted for connection to a source of fluid fuel for supply of fuel from the source to the assembly at a fuel flow rate within the substantial range of fuel flow rates, the assembly having a discharge end of said axis through which the mixture is discharged to the combustion zone, and

(b) spaced upstream and downstream combustion zone shroud means for creating in the combustion zone over said range of fuel flow rates, during the existence of said air stream therepast, a region of relatively nonturbulent gas having a pressure higher than the pressure in said air stream and in which combustion of the fuel-air mixutre can occur, the shroud means being disposed along said axis respectively (1) upstream of and adjacent the nozzle assembly discharge end and (2) substantially at a downstream end of the combustion zone and disposed substantially normal to the axis upstream and downstream of the discharge end of the nozzle assembly and defining openings for controlled flow of air into the region and for controlled flow of gas from the region,

(c) the apparatus being characterized by the absence, between the upstream and downstream shroud means, of physical structure between the high velocity air stream and the region of relatively nonturbulent gas.