Method of machining a gas turbine engine component
US-2016083852-A1 · Mar 24, 2016 · US
US10890116B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10890116-B2 |
| Application number | US-201916287223-A |
| Country | US |
| Kind code | B2 |
| Filing date | Feb 27, 2019 |
| Priority date | Mar 26, 2018 |
| Publication date | Jan 12, 2021 |
| Grant date | Jan 12, 2021 |
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A fuel injector comprises a fuel feed arm and a fuel injector head and the fuel injector head has a fuel passage. The fuel feed arm has a fuel supply passage in fluid communication with the fuel passage in the fuel injector head. A first light guide extends through the fuel feed arm and has a distal end arranged to direct light into the fuel passage in the fuel injector head. A light source is arranged to supply light into a proximal end of the first light guide. A second light guide extends through the fuel feed arm and has a distal end arranged to receive transmitted light in the fuel passage in the fuel injector head and a light receiver is arranged to collect light at a proximal end of the second light guide.
Opening claim text (preview).
The invention claimed is: 1. A fuel injector comprising a fuel feed arm and a fuel injector head, the fuel injector head having a fuel passage, the fuel feed arm having a fuel supply passage in fluid communication with the fuel passage in the fuel injector head, a first light guide extending through the fuel feed arm and having a distal end arranged to direct light into the fuel passage in the fuel injector head, a second light guide extending through the fuel feed arm and having a distal end arranged to receive light in the fuel passage in the fuel injector head, in operation a proximal end of the first light guide being connectable to a light source arranged to supply light and a proximal end of the second light guide being connectable to a light receiver. 2. A combustion chamber comprising a fuel injector, the fuel injector comprising a fuel feed arm and a fuel injector head, the fuel injector head having a fuel passage, the fuel feed arm having a fuel supply passage in fluid communication with the fuel passage in the fuel injector head, a first light guide extending through the fuel feed arm and having a distal end arranged to direct light into the fuel passage in the fuel injector head, a second light guide extending through the fuel feed arm and having a distal end arranged to receive light transmitted through the fuel passage in the fuel injector head from the distal end of the first light guide, a light source arranged to supply light to a proximal end of the first light guide and a light receiver arranged to collect light at a proximal end of the second light guide. 3. A combustion chamber as claimed in claim 2 , wherein the light receiver is a photo-electric device arranged to convert the received light into an electrical signal. 4. A combustion chamber as claimed in claim 3 , wherein a recorder is arranged to record the electrical signal. 5. A combustion chamber as claimed in claim 3 , wherein a processor is arranged to measure the amplitude of the electrical signal corresponding to the light received by the second light guide. 6. A combustion chamber as claimed in claim 5 , wherein the processor is arranged to compare the amplitude of the electrical signal corresponding to the light received by the second light guide with a datum amplitude. 7. A combustion chamber as claimed in claim 3 , wherein the processor is arranged to monitor the amplitude of the electrical signal corresponding to the light received by the second light guide, the processor is arranged to detect a reduction in the amplitude of the electrical signal corresponding to the light received by the second light guide due to coking in the fuel injector. 8. A combustion chamber as claimed in claim 2 , wherein the fuel injector is a gas turbine fuel injector. 9. A combustion chamber as claimed in claim 2 , wherein the fuel injector is an air blast fuel injector. 10. A combustion chamber as claimed in claim 2 , wherein the fuel injector is a rich burn fuel injector, the rich burn fuel injector comprises: a fuel feed arm having a fuel supply passage extending there-through, a fuel injector head having an air-blast fuel injector, the air-blast fuel injector comprising, in order radially outwardly, a coaxial arrangement of an inner air swirler passage and an outer air swirler passage, an annular fuel passage being arranged to supply fuel into the inner air swirler passage and/or into the outer air swirler passage. 11. A combustion chamber as claimed in claim 2 , wherein the fuel injector is a lean burn fuel injector, the lean burn fuel injector comprises: a fuel feed arm having a pilot fuel supply passage extending there-through and a main fuel supply passage extending there-through, a fuel injector head having a coaxial arrangement of an inner pilot air-blast fuel injector and an outer main air-blast fuel injector, the outer main air-blast fuel injector being arranged coaxially radially outwardly of the inner pilot air-blast fuel injector, the inner pilot air-blast fuel injector comprising, in order radially outwardly, a coaxial arrangement of a pilot inner air swirler passage and a pilot outer air swirler passage, an annular pilot fuel passage being arranged to supply pilot fuel into the pilot inner air swirler passage and/or into the pilot outer air swirler passage, the outer main air-blast fuel injector comprising, in order radially outwardly, a coaxial arrangement of a main inner air swirler passage and a main outer air swirler passage, an annular main fuel passage being arranged to supply main fuel to the main inner air swirler passage and/or the main outer air swirler passage. 12. A combustion chamber as claimed in claim 11 , wherein the first light guide having a distal end arranged to direct light into the annular main fuel passage in the fuel injector head and the second light guide having a distal end arranged to receive light in the annular main fuel passage. 13. A combustion chamber as claimed in claim 11 , wherein the first light guide having a distal end arranged to direct light into the annular pilot fuel passage in the fuel injector head and the second light guide having a distal end arranged to receive light in the annular pilot fuel passage. 14. A combustion chamber as claimed in claim 11 , wherein the lean burn fuel injector having a first light guide extending through the fuel feed arm and having a distal end arranged to direct light into the annular main fuel passage in the fuel injector head, a first light source arranged to supply light into a proximal end of the first light guide, a second light guide extending through the fuel feed arm and having a distal end arranged to receive light in the annular main fuel passage and a first light receiver arranged to collect light at a proximal end of the second light guide, a third light guide extending through the fuel feed arm and having a distal end arranged to direct light into the annular pilot fuel passage in the fuel injector head, a second light source arranged to supply light into a proximal end of the third light guide, a fourth light guide extending through the fuel feed arm and having a distal end arranged to receive light in the annular pilot fuel passage and a second light receiver arranged to collect light at a proximal end of the fourth light guide. 15. A method of detecting coking in a fuel injector, wherein the fuel injector being arranged in a combustion chamber, the fuel injector comprising a fuel feed arm and a fuel injector head, the fuel injector head having a fuel passage, the fuel feed arm having a fuel supply passage in fluid communication with the fuel passage in the fuel injector head, the method comprising directing light into the fuel passage in the fuel injector head, detecting light transmitted through the fuel passage in the fuel injector head and monitoring the light transmitted through the fuel passage in the fuel injector head to detect coking in the fuel injector. 16. A method as claimed in claim 15 , comprising converting the light that has been detected to an electrical signal. 17. A method as claimed in claim 16 , comprising recording the electrical signal. 18. A method as claimed in claim 16 , comprising measuring the amplitude of the electrical signal corresponding to the light that has been detected. 19. A method as claimed in claim 18 , comprising comparing the amplitude of the electrical signal corresponding to the light that has been detected with a datum amplitude. 20. A method as claimed in claim 16 , comprising monitoring the amplitude of the electri
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Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed (F02C9/30 - F02C9/38, F02C9/44 take precedence) · CPC title
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characterised by the fuel supply (burners F23D) · CPC title
Combustors or associated equipment · CPC title
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