Fuel injection system
A fuel injection system is described, and which has an upstream portion and a downstream portion. The upstream portion includes a source of fuel, the fuel inlet of a fuel injection servo or flow regulator, and a first fuel flow line connected in fuel flowing relation relative to the source of fuel and to the fuel inlet of the fuel injection servo. The downstream portion includes a flow divider, at least one fuel outlet of the fuel injection servo, and a second fuel flow line connected in fuel flowing relation relative to the flow divider and the fuel outlet of the fuel injection servo. A fuel accumulator pressure damper is mounted in fuel flowing relation relative to the downstream portion of the fuel injection system so as to substantially reduce standing waves in the fuel injection system.
1. A fuel injection system, comprising:
a fuel injection servo with a fuel inlet and at least one fuel outlet;
an upstream portion of the fuel injection system, comprising a source of fuel; the fuel inlet of the fuel injection servo; and a first fuel flow line connected in fuel flowing relation relative to the source of fuel and to the fuel inlet of the fuel injection servo;
a downstream portion of the fuel injection system, comprising a flow divider;
at least one fuel outlet of the fuel injection servo; and a second fuel flow line connected in fuel flowing relation relative to the flow divider and the at least one fuel outlet of the fuel injection servo; and
a fuel accumulator mounted in fuel flowing relation relative to the downstream portion of the fuel injection system; wherein the fuel accumulator comprises a vessel fabricated from a pressure compliant material received within containment housing.
2. A fuel injection system as claimed in claim 1 , and wherein the fuel accumulator vessel is a tube.
3. A fuel injection system as claimed in claim 1 , and wherein the fuel accumulator is mounted in serial fuel flowing relation relative to the second fuel flow line.
4. A fuel injection system as claimed in claim 1 , and wherein the second fuel flow line further comprises a T-fitting with a first end connected in fuel flowing relation relative to the first fuel outlet of the fuel injection servo, and a second end connected in fuel flowing relation relative to the flow divider, and a third end connected in fuel flowing relation relative to the fuel accumulator.
5. A fuel injection system as claimed in claim 1 , and wherein the fuel injection servo has a second fuel line, and wherein the fuel accumulator is connected in fuel flowing relation relative to the second fuel line of the fuel injection servo.
6. A fuel injection system as claimed in claim 1 , and wherein the flow divider comprises an auxiliary fuel port, and wherein the fuel accumulator is connected in fuel flowing relation relative to the auxiliary fuel port of the flow divider.
7. A fuel injection system as claimed in claim 1 , and wherein the fuel accumulator substantially reduces standing waves in the downstream portion of the fuel injection system.
8. A fuel injection system for an aircraft engine, comprising:
a source of fuel;
a fuel injection servo with a fuel inlet, and wherein the source of fuel is connected in fuel supplying relation relative to the fuel inlet of the fuel injection servo; and
a fuel accumulator mounted downstream of the fuel inlet of the fuel injection servo, and wherein the fuel accumulator comprises a vessel fabricated from a pressure compliant material which substantially reduces standing waves in the fuel injection system.
9. A fuel injection system as claimed in claim 8 , and wherein the fuel injection servo has a fuel outlet, and wherein a fuel flow line connects the fuel outlet of the fuel injection servo in fuel supplying relation relative to a flow divider.
10. A fuel injection system as claimed in claim 9 , and wherein the fuel accumulator is mounted in serial fuel flowing relation relative to the fuel flow line.
11. A fuel injection system as claimed in claim 9 , and wherein the fuel flow line further comprises a T-fitting with a first end connected in fuel receiving relation relative to the fuel outlet of the fuel injection servo, and a second end connected in fuel supplying relation relative to the flow divider, and a third end connected in fuel flowing relation relative to the fuel accumulator.
12. A fuel injection system as claimed in claim 9 , and wherein the flow divider comprises an auxiliary fuel port, and wherein the fuel accumulator is connected in fuel flowing relation relative to the auxiliary fuel port of the flow divider.
13. A fuel injection system as claimed in claim 9 , and wherein the fuel injection servo has a first and a second fuel outlet, and wherein the fuel accumulator is connected in fuel flowing relation relative to the second fuel outlet of the fuel injection servo.
14. A fuel injection system as claimed in claim 9 , and wherein the fuel accumulator is mounted to the second fuel outlet of the fuel injection servo with a single threaded fitting.