Inline pilot with flame detection device and method thereof

1. An inline pilot assembly comprising:

a fuel orifice;

a fuel mixer;

a base hub;

a spacer tube;

a nozzle assembly having a diffuser and a burner nozzle for maintaining combustion, wherein the diffuser has a central opening and is configured for receiving a flame rod through the central opening in the diffuser; and

a flame rod;

wherein the fuel orifice is fluidly connected the fuel mixer at an upstream end of the fuel mixer, the fuel mixer is fluidly connected to the base hub at an upstream end of the base hub, the base hub is fluidly connected to the spacer tube at an upstream end of the spacer tube, and the spacer tube is fluidly connected to the upstream end of the nozzle assembly;

wherein the flame rod is disposed internally within the spacer tube and extends coaxially within at least a portion of a length of the spacer tube and also extends coaxially through the central opening in the diffuser and into the nozzle assembly; and

wherein the diffuser is configured for directing fuel into the burner nozzle adjacent to the flame rod.

2. The inline pilot assembly of claim 1 , wherein the burner nozzle has a ground connection.

3. The inline pilot assembly of claim 1 , further comprising a set screw connected to the diffuser and disposed on the diffuser internally to the burner nozzle.

4. The inline pilot assembly of claim 3 , wherein the set screw is configured to permit formation of a spark between the set screw and a conductive region of the flame rod.

5. The inline pilot assembly of claim 1 , wherein the diffuser has a plurality of radial holes disposed in a radial wall of the diffuser.

6. The inline pilot assembly of claim 5 , wherein the diffuser has a plurality of axial holes disposed in a downstream end of the diffuser adjacent a perimeter of the downstream end of the diffuser.

7. The inline pilot assembly of claim 6 , wherein one or more of plurality of axial holes in the diffuser is larger than one or more of the plurality of radial holes in the diffuser.

8. The inline pilot assembly of claim 7 , wherein each of the plurality of the axial holes in the diffuser is disposed equidistance from each of the adjacent axial holes in the diffuser.

9. The inline pilot assembly of claim 7 , wherein each of the plurality of radial holes in the diffuser is disposed equidistance from each of the adjacent radial holes in the diffuser.

10. The inline pilot assembly of claim 7 , wherein

the burner nozzle includes a plurality of a longitudinal series of holes disposed radially in the burner nozzle, wherein a first hole of each longitudinal series of holes is disposed near a base end of the burner nozzle and is larger than downstream holes in the same longitudinal series of holes;

wherein a radial channel is formed between the outer radial wall of the diffuser and an inner radial surface of the burner nozzle;

wherein one or more of the plurality of radial holes in the diffuser is disposed in the diffuser at a position that is not in line with one of the plurality of axial holes in the diffuser; and

wherein the first hole of each of the plurality of longitudinal series of holes, said first hole being disposed near a base end of the burner nozzle, faces an area of the radial wall of the diffuser between two of the radial holes in the pilot diffuser.

11. A pilot nozzle assembly for use with a coaxially configured inline pilot comprising:

a pilot nozzle, wherein the pilot nozzle includes a plurality of a longitudinal series of holes disposed radially in the pilot nozzle, wherein a first hole of each longitudinal series of holes is disposed near a base end of the pilot nozzle and is larger than downstream holes in the same longitudinal series of holes;

a pilot diffuser disposed in the base end of the pilot nozzle, wherein the pilot diffuser has a central opening for receiving a flame rod;

wherein a radial channel is formed between an outer radial wall of the pilot diffuser and an inner radial surface of the pilot nozzle;

a plurality of radial holes disposed in the radial wall of the pilot diffuser adjacent to the radial channel;

a plurality of axial holes disposed in a downstream end of the pilot diffuser adjacent a perimeter of the downstream end of the pilot diffuser;

wherein the axial holes in the pilot diffuser are larger than the radial holes in the pilot diffuser and the radial holes in the pilot diffuser are not in line with the axial holes in the pilot diffuser; and

wherein each first hole of each longitudinal series of holes in the pilot nozzle face an area of the radial wall of the pilot diffuser between two of the radial holes in the pilot diffuser.

12. The pilot nozzle assembly of claim 11 , wherein a top edge of the downstream end of the pilot diffuser extends into the pilot nozzle to a distance fixed between a first upstream side an opening forming the first hole of the longitudinal series of holes disposed near the base end of the pilot nozzle and a second downstream side of the opening forming the first hole of the longitudinal series of holes disposed near the base end of the pilot nozzle.

13. The pilot nozzle assembly of claim 12 , wherein the top edge of the downstream end of the pilot diffuser extends into the pilot nozzle to a distance that is about ¾ of the distance to the second downstream side of the opening forming the first hole of the longitudinal series of holes disposed near the base end of the pilot nozzle.

14. A pilot nozzle assembly of claim 12 , wherein one or more of the plurality of radial holes in the pilot diffuser are disposed within the radial channel between two of the first holes of the plurality of longitudinal series of holes that are disposed in the inner radial surface of the pilot nozzle adjacent to said one or more of the plurality of radial holes.