Fuel system and method for supplying a combustion chamber in an aircraft turboshaft engine with fuel
US-2024318601-A1 · Sep 26, 2024 · US
US9851106B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9851106-B2 |
| Application number | US-201515125475-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 25, 2015 |
| Priority date | Apr 7, 2014 |
| Publication date | Dec 26, 2017 |
| Grant date | Dec 26, 2017 |
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A fuel injector for injecting fuel in a burner of a gas turbine where the fuel injector has a body with an inner hole and a valve element which is slideably arranged inside the inner hole. The body has a fuel inlet which is formed into the body for injecting fuel into the inner hole, wherein the fuel inlet is coupleable to a fuel supply line. The body further has a first outlet channel connected to the inner hole, wherein the first outlet channel is further coupleable to a burner. The valve element has a first passage which is formed such that in a first position of the valve element inside the inner hole, the first passage connects the fuel inlet with the first outlet channel and in a second position of the valve element inside the inner hole.
Opening claim text (preview).
The invention claimed is: 1. A fuel injector for injecting fuel in a burner of a gas turbine, the fuel injector comprising: a body comprising an inner hole, a valve element which is slideably arranged inside the inner hole, wherein the body comprises a fuel inlet which is formed into the body for injecting fuel into the inner hole, wherein the fuel inlet is coupleable to a fuel supply line, wherein the body comprises a first outlet channel connected to the inner hole, wherein the first outlet channel is further coupleable to the burner, wherein the valve element comprises a first passage which is formed such that in a first position of the valve element inside the inner hole, the first passage connects the fuel inlet with the first outlet channel, and in a second position of the valve element inside the inner hole, the valve element seals the fuel inlet from the first outlet channel, wherein the body comprises a second outlet channel connected to the inner hole, wherein the second outlet channel is further coupleable to the burner or a further burner, wherein the valve element is slideable inside the inner hole along a sliding direction, wherein the first outlet channel is spaced apart from the second outlet channel along the sliding direction, wherein the valve element comprises a second passage which is spaced apart from the first passage along the sliding direction, wherein the second passage is formed such that in the second position of the valve element inside the inner hole, the valve element seals the fuel inlet from the first outlet channel and from the second outlet channel, and in a third position of the valve element inside the inner hole the second passage connects the fuel inlet with the second outlet channel, wherein a fluid flow between the fuel inlet and the first outlet channel is prevented, and wherein the valve element comprises an inlet groove which is formed such that the fuel inlet is connected to the first passage and to the second passage. 2. The fuel injector according to claim 1 , wherein the second passage is formed such that in a fourth position of the valve element inside the inner hole, the second passage connects the fuel inlet with the first outlet channel and the second outlet channel. 3. The fuel injector according to claim 2 , wherein the valve element comprises a first outlet groove which is coupled to the first passage, wherein the first outlet groove comprises a length along the sliding direction which length is smaller than a distance between the first outlet channel and the second outlet channel along the sliding direction such that in the first position of the valve element the first outlet groove connects the first passage with the first outlet channel and the fuel inlet is sealed from the second outlet channel by the valve element. 4. The fuel injector according to claim 1 , wherein the valve element comprises a second outlet groove which is coupled to the second passage and which extends along the sliding direction, and wherein the second outlet groove comprises a length along the sliding direction which length is larger than a distance between the first outlet channel and the second outlet channel along the sliding direction such that in a fourth position of the valve element the second outlet groove connects the second passage with the first outlet channel and the second outlet channel. 5. The fuel injector according to claim 1 , further comprising a driving mechanism which is coupled to the valve element for driving the valve element within the inner hole. 6. The fuel injector according to claim 5 , wherein the driving mechanism comprises an actuator and a spindle element, wherein the spindle element is coupled to the body and to the valve element such that a pivoting of the spindle element generates a sliding motion of the valve element within the inner hole, wherein the actuator is coupled to the spindle element such that a torque is transferable to the spindle element by the actuator for pivoting the spindle element. 7. The gas turbine, comprising the burner, and the fuel injector according to claim 1 which is coupled to the burner for injecting fuel in the burner. 8. A method for operating a fuel injector for injecting fuel in a burner of a gas turbine, wherein the fuel injector comprises a body comprising an inner hole and a valve element which is slideably arranged inside the inner hole, wherein the body comprises a fuel inlet which is formed into the body for injecting fuel into the inner hole, wherein the fuel inlet is coupleable to a fuel supply line, wherein the body comprises a first outlet channel connected to the inner hole, wherein the first outlet channel is further coupleable to the burner, wherein the valve element comprises a first passage, the method comprising: sliding the valve element in a first position inside the inner hole such that the first passage connects the fuel inlet with the first outlet channel, and sliding the valve element in a second position of the valve element inside the inner hole such that the valve element seals the fuel inlet from the first outlet channel, wherein the body comprises a second outlet channel connected to the inner hole, wherein the second outlet channel is further coupleable to the burner or a further burner, wherein the valve element is slideable inside the inner hole along a sliding direction, wherein the first outlet channel is spaced apart from the second outlet channel along the sliding direction, wherein the valve element comprises a second passage which is spaced apart from the first passage along the sliding direction, wherein the second passage is formed such that in the second position of the valve element inside the inner hole, the valve element seals the fuel inlet from the first outlet channel and from the second outlet channel, and in a third position of the valve element inside the inner hole the second passage connects the fuel inlet with the second outlet channel, wherein a fluid flow between the fuel inlet and the first outlet channel is prevented, and wherein the valve element comprises an inlet groove which is formed such that the fuel inlet is connected to the first passage and to the second passage. 9. A fuel injector for injecting fuel in a burner of a gas turbine, the fuel injector comprising: a body comprising an inner hole, a valve element which is slideably arranged inside the inner hole, wherein the body comprises a fuel inlet which is formed into the body for injecting fuel into the inner hole, wherein the fuel inlet is coupleable to a fuel supply line, wherein the body comprises a first outlet channel connected to the inner hole, wherein the first outlet channel is further coupleable to the burner, wherein the valve element comprises a first passage which is formed such that in a first position of the valve element inside the inner hole, the first passage forms a fluid path that provides fluid communication between the fuel inlet and the first outlet channel, and in a second position of the valve element inside the inner hole, the valve element blocks the fluid communication between the fuel inlet and the first outlet channel, wherein the body comprises a second outlet channel connected to the inner hole, wherein the second outlet channel is further coupleable to the burner or a further burner, wherein the valve element is slideable inside the inner hole along a sliding direction, wherein the first outlet channel is spaced apart from the second outlet channel along the sliding direction, wherein the valve element comprises a second passage which is spaced apart from the first passage along the sliding d
Fuel valves {(control of fuel supply by means of fuel metering valves F02C9/263)}; Draining valves or systems (valves in general F16K) · CPC title
to control thermoacoustic behaviour in the combustion chambers · CPC title
Preventing, counteracting or reducing vibration or noise · CPC title
with flat slides · CPC title
characterised by the fuel supply (burners F23D) · CPC title
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