IP Library Granted Patent US 11,454,395
Granted Patent B2
US 11,454,395 · App. 17/235,242 · Granted Sep 27, 2022

Thermal resistant air caps

Inventor: Steve J. Myers (Norwalk, IA)
Assignee: Collins Engine Nozzles, Inc.
F23R3/14F02C7/222F02C7/2365F23R3/283F23R3/286
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Quick Facts
Patent No.
US 11,454,395
App. No.
17/235,242
Granted
Sep 27, 2022
Kind
B2
Abstract

An air cap is configured to be affixed to a nozzle assembly as a downstream facing component of the nozzle assembly. The air cap includes a plurality of air wipe passages with outlets defined in a circumferential direction around a downstream facing surface of the air cap. A nozzle assembly can include an outer wall wherein the air cap is connected to the nozzle assembly outboard of the outer wall. An inner wall can be connected to the outer wall by a plurality of air swirl vanes. One or more fuel circuit components can be connected to the nozzle assembly inboard of the inner wall.

Claims (21)

1. An apparatus comprising:

an air cap affixed to a fuel nozzle assembly as a downstream facing component of the nozzle assembly, wherein the air cap includes a plurality of air wipe passages with outlets defined in a circumferential direction around a downstream facing surface of the air cap, wherein each air wipe passage extends from an interior surface of the air cap to the downstream facing surface of the air cap, winding in a helical direction about a spray axis of the air cap, wherein the air wipe passages are radially nested, helical passages.

2. An apparatus comprising:

an air cap affixed to a fuel nozzle assembly as a downstream facing component of the nozzle assembly, wherein the air cap includes a plurality of air wipe passages with outlets defined in a circumferential direction around a downstream facing surface of the air cap, wherein an annular passage is upstream of the air cap, wherein the air wipe passages are a plurality of radially nested, helical passages with inlets defined in an upstream facing surface of the air cap.

3. The apparatus as recited in claim 2 , wherein the downstream facing surface of the air cap includes a circumferentially extending series of steps, each step defining a circumferentially facing outlet face from which one or more of the outlets emerge.

4. The apparatus as recited in claim 2 , further comprising the fuel nozzle assembly including:

an outer wall wherein the air cap is connected to the fuel nozzle assembly outboard of the outer wall.

5. The apparatus as recited in claim 4 , wherein the fuel nozzle assembly further comprises:

an inner wall connected to the outer wall by a plurality of air swirl vanes, straight vanes, and/or standoffs.

6. The apparatus as recited in claim 5 , wherein the fuel nozzle assembly further comprises one or more fuel circuit components connected to the fuel nozzle assembly inboard of the inner wall.

7. The apparatus as recited in claim 6 , wherein a gas fuel circuit is defined inboard of the inner wall.

8. The apparatus as recited in claim 7 , wherein one or more liquid circuits are defined inboard of the gas fuel circuit.

9. The apparatus as recited in claim 6 , wherein the air cap, the inner wall, and the outer wall are a single integral component.

10. The apparatus as recited in claim 6 , wherein the air cap is a separate component from the outer wall, wherein the air cap is mounted to the outer wall.

11. The apparatus as recited in claim 6 , wherein an air wipe feed passage is defined between the outer wall and the air cap, wherein the plurality of air wipe passages is in fluid communication with the air wipe feed passage.

12. The apparatus as recited in claim 2 , wherein the air cap defines a central outlet orifice therethrough.

13. The apparatus as recited in claim 2 , wherein there is at least one radial cross-section of the air cap wherein the plurality of air wipe passages are layered at least two deep in an axial direction.

14. An apparatus comprising:

an air cap affixed to a nozzle assembly as a downstream facing component of the nozzle assembly, wherein the air cap includes a plurality of air wipe passages with outlets defined in a circumferential direction around a downstream facing surface of the air cap, further comprising a nozzle assembly including:

an outer wall wherein the air cap is connected to the nozzle assembly outboard of the outer wall, wherein the nozzle assembly further comprises:

an inner wall connected to the outer wall by a plurality of air swirl vanes, straight vanes, and/or standoffs, wherein the nozzle assembly further comprises one or more fuel circuit components connected to the nozzle assembly inboard of the inner wall, wherein an air wipe feed passage is defined between the outer wall and the air cap, wherein the air wipe feed passage is in fluid communication with the plurality of air wipe passages wherein the air wipe feed passage is connected to a gaseous fuel source to issue gaseous fuel through the plurality of air wipe passages.

Assignments (2)
CHANGE OF NAME Recorded May 23, 2022
From: DELAVAN INC
To: COLLINS ENGINE NOZZLES, INC.
Reel/Frame 060158/0900 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 28, 2021
From: MYERS, STEVE J.
To: DELAVAN INC
Reel/Frame 056067/0877 →
Continuity (2)
Provisional Application 63014935 · Apr 24, 2020
Related Publication 20210332980A1 · Oct 28, 2021