US2023103813A1PendingUtilityA1

Ornamental-flame burner

Assignee: WARMING TRENDS LLCPriority: Mar 10, 2020Filed: Mar 9, 2021Published: Apr 6, 2023
Est. expiryMar 10, 2040(~13.6 yrs left)· nominal 20-yr term from priority
F23D 14/58F24C 3/08F23D 23/00F24C 3/006F23D 14/045F23D 14/085F23D 2900/14641F23D 14/64F23D 2203/007F23C 5/02F23D 2900/21004F23D 2900/14003
53
PatentIndex Score
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Claims

Abstract

A burner includes a plurality of end nipples and at least one jet supported by and protruding outwardly from each end nipple. The end nipples and the jets are brass. Each end nipple includes a first end that is threaded and a second end that is closed. Each end nipple includes a wall extending from the first end to the second end and including a bore extending through the first end to the second end. Each end nipple includes a threaded hole extending through the wall to the bore. The first end of the end nipple, the second end of the end nipple, and the wall of the end nipple are unitary. Each jet includes a threaded portion threadedly engaged with the threaded hole and a fuel combustion outlet spaced from the threaded portion. Each jet includes a barrel extending from the fuel combustion outlet toward the threaded portion. The barrel has a larger outer diameter than the threaded portion.

Claims

exact text as granted — not AI-modified
1 . A burner comprising:
 a plurality of end nipples;   at least one jet supported by and protruding outwardly from each end nipple, the end nipples and the jets are brass;   each end nipple including a first end that is threaded and a second end that is closed;   each end nipple including a wall extending from the first end to the second end and including a bore extending through the first end to the second end, each end nipple including a threaded hole extending through the wall to the bore;   the first end of the end nipple, the second end of the end nipple, and the wall of the end nipple being unitary;   each jet including a threaded portion threadedly engaged with the threaded hole and a fuel combustion outlet spaced from the threaded portion;   each jet including a barrel extending from the fuel combustion outlet toward the threaded portion, the barrel having a larger outer diameter than the threaded portion;   each jet including a tapering portion extending from the threaded portion to the barrel, an outer diameter of the tapering portion tapering from the barrel to the threaded portion; and   a wall thickness of the tapering portion increasing from the barrel to the threaded portion.   
     
     
         2 . (canceled) 
     
     
         3 . (canceled) 
     
     
         4 . The burner of  claim 1 , wherein the tapering portion has a full taper angle, the full taper angle is 60 degrees. 
     
     
         5 . The burner of  claim 1 , wherein the threaded portion and the barrel each have a length along a longitudinal axis of the jet, the length of the threaded portion is between 0.2-0.3 inches and the length of the barrel is between 0.6-0.7 inches. 
     
     
         6 . The burner of  claim 1 , wherein each jet includes a length along a longitudinal axis of the jet, the length is between 0.9-1.1 inches. 
     
     
         7 . The burner of  claim 6 , wherein the outer diameter of the barrel is between 0.3-0.5 inches. 
     
     
         8 . The burner of  claim 6 , wherein the threaded portion has 1/16-27 National Pipe Thread Taper (NPT) threads. 
     
     
         9 . The burner of  claim 1 , wherein each jet defines a bore, the size of the diameter of the bore being between 75%-85% the size of the outer diameter of the threaded portion. 
     
     
         10 . The burner of  claim 1 , wherein each jet defines a bore extending through the fuel combustion outlet and an inlet bore extending through the threaded portion, a diameter of the bore is larger than a diameter of the inlet bore. 
     
     
         11 . The burner of  claim 10 , wherein an end of the bore of the jet is aligned along a longitudinal axis of the jet between the tapering portion and the fuel combustion outlet. 
     
     
         12 . The burner of  claim 11 , wherein each jet includes a countersink extending from the bore of the jet to the inlet bore, the countersink terminating at the inlet bore at an end of the countersink aligned with the tapering portion along the longitudinal axis of the jet. 
     
     
         13 . (canceled) 
     
     
         14 . (canceled) 
     
     
         15 . (canceled) 
     
     
         16 . (canceled) 
     
     
         17 . The burner of  claim 10 , wherein the diameter of the bore is constant from the fuel combustion outlet to the tapering portion and the diameter of the inlet bore is constant from the tapering portion through the threaded portion. 
     
     
         18 . (canceled) 
     
     
         19 . The burner of  claim 1 , wherein the barrel includes a wall extending from the fuel combustion outlet towards the threaded portion and an oxygen hole extending through the wall to the bore, the oxygen hole being between the threaded portion and the fuel combustion opening. 
     
     
         20 . (canceled) 
     
     
         21 . (canceled) 
     
     
         22 . (canceled) 
     
     
         23 . (canceled) 
     
     
         24 . (canceled) 
     
     
         25 . The burner of  claim 1 , wherein each end nipple has flats at the second end of the end nipple, the flats being arranged circumferentially about the second end of the end nipple. 
     
     
         26 . The burner of  claim 1 , wherein the first end of each end nipple has ¼-18 National Pipe Thread Taper (NPT) threads. 
     
     
         27 . The burner of  claim 1 , wherein each end nipple has an outer diameter, the outer diameter of the end nipple is between 0.5-0.6 inches. 
     
     
         28 . The burner of  claim 27 , wherein the bore of each end nipple has a diameter, the diameter of the bore is between 0.3-0.4 inches. 
     
     
         29 . The burner of  claim 12 , wherein the countersink terminates at the bore at an end of the countersink aligned with the barrel along the longitudinal axis of the jet. 
     
     
         30 . A burner comprising:
 a plurality of end nipples;   at least one jet supported by and protruding outwardly from each end nipple, the end nipples and the jets are brass;   each end nipple including a first end that is threaded and a second end that is closed;   each end nipple including a wall extending from the first end to the second end and including a bore extending through the first end to the second end, each end nipple including a threaded hole extending through the wall to the bore;   each jet including a threaded portion threadedly engaged with the threaded hole and a fuel combustion outlet spaced from the threaded portion;   each jet including a barrel extending from the fuel combustion outlet toward the threaded portion, the barrel having a larger outer diameter than the threaded portion;   each jet including a tapering portion extending from the threaded portion to the barrel, an outer diameter of the tapering portion tapering from the barrel to the threaded portion; and   a wall thickness of the tapering portion increasing from the barrel to the threaded portion.   
     
     
         31 . The burner of  claim 30 , wherein each jet defines a bore extending through the fuel combustion outlet and an inlet bore extending through the threaded portion, a diameter of the bore is larger than a diameter of the inlet bore. 
     
     
         32 . The burner of  claim 31 , wherein an end of the bore of the jet is aligned along a longitudinal axis of the jet between the tapering portion and the fuel combustion outlet. 
     
     
         33 . The burner of  claim 32 , wherein each jet includes a countersink extending from the bore of the jet to the inlet bore, the countersink terminating at an end aligned with the tapering portion along longitudinal axis of the jet.

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