Injection system for a turbine engine combustion chamber configured for direct injection of two coaxial fuel flows
US-2015377489-A1 · Dec 31, 2015 · US
US10823397B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10823397-B2 |
| Application number | US-201414907796-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 3, 2014 |
| Priority date | Aug 1, 2013 |
| Publication date | Nov 3, 2020 |
| Grant date | Nov 3, 2020 |
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A burner arrangement (1), for a mobile heater operated with liquid fuel, is provided; having a combustion chamber (2) for converting fuel with combustion air in a flaming combustion, which combustion chamber (2) extends along a longitudinal axis (Z) in a main flow direction (H); a pre-mixing chamber (3), which is arranged fluidicly upstream of the combustion chamber (2), for generating a fuel-combustion air-mixture, which pre-mixing chamber (3) comprises a side wall (4); a fuel evaporation surface (O) arranged in the pre-mixing chamber; a fuel supply (10) for supplying liquid fuel; and a first combustion air supply (6) having a swirl body (7) for supplying a combustion air flow into the pre-mixing chamber (3) with a swirl such that the combustion air is guided along the fuel evaporation surface (O) with a tangential flow component. A neck portion (5) is formed at a transition from the pre-mixing chamber (3) to the combustion chamber (2) at which the flow cross-section abruptly widens in the main flow direction (H).
Opening claim text (preview).
The invention claimed is: 1. A burner arrangement for a mobile heater operated with liquid fuel, said arrangement comprising: a combustion chamber converting fuel with combustion air in a flaming combustion, said combustion chamber extending along a longitudinal axis in a main flow direction; a pre-mixing chamber in which a flame does not form during regular heating operation, arranged upstream of the combustion chamber, formed separate from the combustion chamber and generating a fuel-combustion air-mixture, said pre-mixing chamber including a side wall tapering in the main flow direction; a fuel evaporation surface arranged in the pre-mixing chamber and provided by an absorbent material evaporator body being arranged in the pre-mixing chamber; a fuel supply supplying liquid fuel to said pre-mixing chamber; and a first combustion air supply having a swirl body and supplying a combustion air flow into the pre-mixing chamber with a swirl such that the combustion air is guided along the fuel evaporation surface with a tangential flow component, wherein a neck portion is formed at a transition from the pre-mixing chamber to the combustion chamber at which a flow cross-section abruptly widens in the main flow direction. 2. The burner arrangement according to claim 1 , wherein the fuel evaporation surface extends over at least a portion of the side wall and the fuel supply includes a fuel outlet opening out at the side wall. 3. The burner arrangement according to claim 1 , wherein the first combustion air supply is formed such that the combustion air flow is supplied substantially parallel to the main flow direction with a tangential flow component. 4. The burner arrangement according to claim 1 , wherein the first combustion air supply opens out into the pre-mixing chamber at a face side of the pre-mixing chamber which faces away from the combustion chamber. 5. The burner arrangement according to claim 4 , wherein the first combustion air supply opens out into the pre-mixing chamber at the face side in a radially outer region of the face side. 6. The burner arrangement according to claim 1 , wherein the fuel outlet opens out in a region in which the evaporator body is arranged. 7. The burner arrangement according to claim 1 , wherein the first combustion air supply and the transition from the pre-mixing chamber to the combustion chamber are formed such that the fuel-combustion air-mixture is introduced into the combustion chamber with a tangential flow component such that a recirculation region in which gases flow opposite to the main flow direction forms in the combustion chamber behind the transition in a radially inner region at a longitudinal axis. 8. The burner arrangement according to claim 1 , wherein the first combustion air supply and the pre-mixing chamber are formed such that the fuel-combustion air-mixture enters into the combustion chamber with a swirl factor of at least 0.6. 9. The burner arrangement according to claim 1 , wherein a second combustion air supply supplying combustion air into the combustion chamber is formed downstream of the pre-mixing chamber. 10. A mobile heater operated with liquid fuel having a burner arrangement according to claim 1 .
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