Fuel manifold for a gas turbine engine

Patent metadata

Field	Value
Publication number	US-10132244-B2
Application number	US-201414911357-A
Country	US
Kind code	B2
Filing date	Aug 29, 2014
Priority date	Aug 30, 2013
Publication date	Nov 20, 2018
Grant date	Nov 20, 2018

Abstract

A fuel supply manifold for a gas turbine engine includes a first manifold segment includes a first multiple of double-barrel fittings in communication with a primary fuel circuit and a secondary fuel circuit. A second manifold segment includes a second multiple of double-barrel fittings in communication with the primary fuel circuit and the secondary fuel circuit. The first manifold segment is connected to the second manifold segment.

First claim

What is claimed is:

1. An assembly for a gas turbine engine, comprising:
a first manifold segment including a first multiple of double-barrel fittings which at least partially defines a primary fuel circuit and a secondary fuel circuit;
a second manifold segment attachable to the first manifold segment, the second manifold segment including a second multiple of double-barrel fittings that at least partially define the primary fuel circuit and the secondary fuel circuit;
a first pigtail;
a second pigtail;
a third pigtail;
a fourth pigtail;
a first fuel injector that includes a first primary fuel injector port and a first secondary fuel injector port; and
a second fuel injector that includes a second primary fuel injector port and a second secondary fuel injector port,
wherein a double-barrel fitting of the first multiple of double-barrel fittings includes a first primary pigtail port in communication with the primary feel circuit and a first secondary pigtail port in communication with the secondary fuel circuit,
wherein a double-barrel fitting of the second multiple of double barrel fittings includes a second primary pigtail port in communication with the primary fuel circuit and a second secondary pigtail port in communication with the secondary fuel circuit,
wherein the first pigtail is received by the first primary fuel injector port and the first primary pigtail port,
wherein the second pigtail is received by the first secondary fuel injector port and the first secondary pigtail port,
wherein the third pigtail is received by the second primary fuel injector port and the second primary pigtail port, and
wherein the fourth pigtail is received by the second secondary fuel injector port and the second secondary pigtail port.

2. The assembly as recited in claim 1 , wherein the first manifold segment defines an arc of 180 degrees, and wherein the second manifold segment defines an arc of 180 degrees.

3. The assembly as recited in claim 1 , wherein the primary fuel circuit is at least partially defined by a multiple of first straight tubes and the secondary fuel circuit is at least partially defined by a multiple of second straight tubes, wherein the multiple of first straight tubes are brazed between each two of the first multiple of double-barrel fittings, and wherein the multiple of second straight tubes are brazed between each two of the second multiple of double-barrel fittings.

4. The assembly as recited in claim 1 , wherein the first manifold segment includes a fuel manifold feed subassembly in communication with the primary fuel circuit and the secondary fuel circuit.

5. The assembly as recited in claim 4 , wherein the fuel manifold feed subassembly is located at bottom dead center of the gas turbine engine.

6. The assembly as recited in claim 1 , wherein each of the first and second multiple of double-barrel fittings further comprises:
a first primary fuel circuit port of the primary fuel circuit that defines a first primary axis; and
a second primary fuel circuit port of the primary fuel circuit in communication with the first primary fuel circuit port, wherein the second primary fuel circuit port defines a second primary axis that defines an angle with respect to the first primary axis.

7. The assembly as recited in claim 6 , wherein the angle is one hundred sixty (160) degrees.

8. The assembly as recited in claim 1 ,
wherein the first pigtail includes a first B-nut that is screwed into the first primary fuel injector port and a second B-nut that is screwed into the first primary pigtail port,
wherein the second pigtail includes a third B-nut that is screwed into the first secondary fuel injector port and a fourth B-nut that is screwed into the first secondary pigtail port,
wherein the third pigtail includes a fifth B-nut that is screwed into the second primary fuel injector port and a sixth B-nut that is screwed into the second primary pigtail port, and
wherein the fourth pigtail includes a seventh B-nut that is screwed into the second secondary fuel injector port and an eighth B-nut that is screwed into the second secondary pigtail port.

9. An assembly for a gas turbine engine, comprising:
a first manifold segment including a primary fuel circuit and a secondary fuel circuit each at least partially formed of a first multiple of straight tubes;
a second manifold segment including a primary fuel circuit and a secondary fuel circuit each at least partially formed of a second multiple of straight tubes, wherein the first manifold segment is attachable to the second manifold segment,
a first pigtail;
a second pigtail;
a third pigtail;
a fourth pigtail;
a first fuel injector that includes a first primary fuel injector port and a first secondary fuel injector port; and
a second fuel injector that includes a second primary fuel injector port and a second secondary fuel injector port,
wherein the first manifold segment includes a first multiple of double-barrel fittings that interconnect the first multiple of straight tubes,
wherein the second manifold segment includes a second multiple of double-barrel fittings that interconnect the second multiple of straight tubes,
wherein a double-barrel fitting of the first multiple of double-barrel fittings includes a first primary pigtail port in communication with the primary fuel circuit and a first secondary pigtail port in communication with the secondary fuel circuit,
wherein a double-barrel fitting of the second multiple of double barrel fittings includes a second primary pigtail port in communication with the primary fuel circuit and a second secondary pigtail port in communication with the secondary fuel circuit,
wherein the first pigtail is received by the first primary fuel injector port and the first primary pigtail port,
wherein the second pigtail is received by the first secondary fuel injector port and the first secondary pigtail port,
wherein the third pigtail is received by the second primary fuel injector port and the second primary pigtail port, and
wherein the fourth pigtail is received by the second secondary fuel injector port and the second secondary pigtail port.

10. The assembly as recited in claim 9 , wherein each of the first multiple of double-barrel fittings further comprise:
a first primary fuel circuit port of the primary fuel circuit of the first manifold segment that defines a first primary axis; and
a second primary fuel circuit port of the primary fuel circuit of the first manifold segment in communication with the first primary fuel circuit port, wherein the second primary fuel circuit port defines a second primary axis that defines a first angle with respect to the first primary axis.

11. The assembly as recited in claim 10 , wherein each of the second multiple of double-barrel fittings further comprise:
a first primary fuel circuit port of the primary fuel circuit of the second manifold segment that defines a third primary axis; and
a second primary fuel circuit port of the primary fuel circuit of the second manifold segment in communication with the first primary fuel circuit port of the primary fuel circuit of the second manifold segment, wherein the second primary fuel circuit port of the primary fuel circuit of the second manifold segment defines a fourth primary axis that defines a second angle with respect to the third primary axis.

12. The assembly as recited in claim 10 , wherein the first angle is one hundred sixty (160) degrees.

13. The assembly as recited in claim 9 , wherein the first manifold segment includes a fuel manifold feed subassembly in communication with the primary fuel circuit and the secondary fuel cir

Assignees

• United Technologies Corp

Inventors

• Chasse Jr James P
• Tu Peter
• Sheil Robert F

Classifications

• F23R3/28

  characterised by the fuel supply (burners F23D) · CPC title

• F23K5/06

  from a central source to a plurality of burners · CPC title

• F05D2240/40

  Use of a multiplicity of similar components · CPC title

• F02C7/228

  Dividing fuel between various burners · CPC title

• F02C7/22 Primary

  Fuel supply systems · CPC title