IP Library Granted Patent US 11,566,565
Granted Patent B2
US 11,566,565 · App. 17/133,303 · Granted Jan 31, 2023

Access hatch for internally mounted torch ignitor

Inventors: Jason Ryon (Carlisle, IA); Lev A. Prociw (Johnston, IA); Brandon Phillip Williams (Johnston, IA)
Assignee: Collins Engine Nozzles, Inc.
F02C7/264F05D2220/32F05D2230/72F05D2230/80F05D2240/35F05D2260/99
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 11,566,565
App. No.
17/133,303
Granted
Jan 31, 2023
Kind
B2
Abstract

An embodiment of an ignition system for a gas turbine engine includes a high pressure engine case, a torch ignitor disposed at least partially within the high pressure engine case, the torch ignitor having a combustion chamber oriented about a torch axis, the combustion chamber having axially upstream and downstream ends defining a flow direction through the combustion chamber, along the axis. The ignition system also includes an access hatch configured to allow access through a high pressure engine case to the cap and to seal against the high pressure engine case when not accessing the cap. An embodiment of a method includes removing a hatch from a high pressure engine case to open a hatch opening, performing maintenance on a torch ignitor that is inside the high pressure engine case by accessing the torch ignitor through the hatch opening, replacing the hatch to close the hatch opening after completion of maintenance on the torch ignitor.

Claims (28)

1. An ignition system for a gas turbine engine, the ignition system comprising:

a high pressure engine case defining an engine axis;

a torch ignitor disposed at least partially within the high pressure engine case, having a torch-ignitor combustion chamber oriented about a torch axis that is oriented circumferentially with respect to the engine axis, the torch-ignitor combustion chamber having axially upstream and downstream ends defining a flow direction through the combustion chamber, along the axis;

a cap defining the axially upstream end of the torch-ignitor combustion chamber and oriented about the axis, wherein a fuel injector and at least one glow plug are seated in the cap; and

a tip at a downstream end of the torch-ignitor combustion chamber for issuing flame; and

an access hatch configured to allow access through the high pressure engine case to the cap and to seal against the high pressure engine case when not accessing the cap, wherein the access hatch and the combustion chamber of the torch ignitor are forward relative to a combustor dome wall of a main combustor in a direction along the engine axis, and wherein the access hatch is radially outboard of the cap, fuel injector, and glow plug relative to the engine axis.

2. The ignition system as recited in claim 1 , wherein the cap is mounted inside the high pressure engine case and the tip is mounted to the main combustor within the high pressure engine case for fluid communication of combustion products from the torch-ignitor combustion chamber into the main combustor.

3. The ignition system as recited in claim 2 , wherein the access hatch is mounted to an outside surface of the high pressure engine case proximate the cap.

4. The ignition system as recited in claim 2 , wherein the access hatch is mounted to an inside surface of the high pressure engine case proximate the cap.

5. The ignition system as recited in claim 2 , further comprising an elbow connected to the downstream end of the torch-ignitor combustion chamber for issuing combustion products along an ignition jet flame axis that is off of the torch axis for injection of combustion products into the main combustor.

6. The ignition system as recited in claim 2 , further comprising a plurality of main fuel injectors mounted to the main combustor, wherein the torch-ignitor combustion chamber is outside of the main combustor, and wherein none of the plurality of main fuel injectors includes a torch-ignitor combustion chamber outside of the main combustor.

7. The ignition system as recited in claim 6 , wherein the main combustor is annular and includes an inner wall and an outer wall spaced radially apart from one another, and wherein a combustor dome wall joins the inner and outer walls, wherein the plurality of main fuel injectors are mounted to the combustor dome wall.

8. The ignition system as recited in claim 7 , wherein the tip is mounted to the combustor dome wall.

9. The ignition system as recited in claim 4 , wherein the access hatch is sealed using a c-seal.

10. The ignition system as recited in claim 4 , wherein the access hatch is attached to the high pressure engine case with at least one of bolts, studs, nuts, threads, and/or clamping.

11. A method comprising:

removing the access hatch as recited in claim 1 from the high pressure engine case to open a hatch opening;

and performing maintenance on the torch ignitor that is inside the high pressure engine case by accessing the torch ignitor through the hatch opening.

12. The method as recited in claim 11 , further comprising replacing the access hatch to close the hatch opening after completion of maintenance on the torch ignitor.

13. The method as recited in claim 11 , wherein performing maintenance on the torch ignitor includes:

removing a used glow plug from the torch ignitor through the hatch opening;

inserting a replacement glow plug through the hatch opening; and

installing the replacement glow plug into the torch ignitor.

14. The method as recited in claim 11 , wherein performing maintenance on the torch ignitor includes:

removing a used fuel injector from the torch ignitor through the hatch opening;

inserting a replacement fuel injector through the hatch opening; and

installing the replacement fuel injector into the torch ignitor.

15. The ignition system as recited in claim 8 , wherein the tip is aligned to issue a flame from the torch ignitor from the combustor dome wall in parallel with the plurality of main fuel injectors of the main combustor.

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 Mar 18, 2021
From: RYON, JASON; PROCIW, LEV A.; WILLIAMS, BRANDON PHILLIP
To: DELAVAN INC
Reel/Frame 055635/0367 →
Continuity (1)
Related Publication 20220195940A1 · Jun 23, 2022
Cited By (1)
US 12,228,086