Combustor, jet engine, flying body, and operation method of jet engine
US-2017030297-A1 · Feb 2, 2017 · US
US10837369B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10837369-B2 |
| Application number | US-201715684546-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 23, 2017 |
| Priority date | Aug 23, 2017 |
| Publication date | Nov 17, 2020 |
| Grant date | Nov 17, 2020 |
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An igniter assembly for a gas turbine combustor includes a first electrode, a second electrode, and an insulator. The first electrode, the second electrode, and the insulator form a cavity, the second electrode forms an outlet passage extending from the cavity, a maximum cross-sectional area of the cavity is greater than a cross-sectional area of the outlet passage, and the cross-sectional area of the outlet passage is substantially constant along a longitudinal extent of the outlet passage. In addition, the first electrode and the second electrode are configured to ionize gas within the cavity in response to an electrical current applied to the first electrode or to the second electrode.
Opening claim text (preview).
The invention claimed is: 1. An igniter assembly for a gas turbine combustor, comprising: a first electrode, a second electrode, and an insulator, wherein the first electrode, the second electrode, and the insulator form a cavity, the second electrode forms an outlet passage extending from the cavity, a maximum cross-sectional area of the cavity is greater than a cross-sectional area of the outlet passage, a first longitudinal end of the outlet passage is positioned at an interface between the outlet passage and the cavity, a second longitudinal end of the outlet passage is positioned at a tip of the igniter assembly, the cavity includes a converging section extending to the interface with the outlet passage, and the cross-sectional area of the outlet passage is substantially constant along a longitudinal extent of the outlet passage between the first longitudinal end and the second longitudinal end; wherein the cavity includes a first portion forming the converging section, the first portion has a cross-sectional area that decreases between the maximum cross-sectional area of the cavity and the interface with the outlet passage, and the first portion is formed only by the second electrode; wherein the cavity includes a second portion having a substantially constant cross-sectional area substantially equal to the maximum cross-sectional area of the cavity, and the second portion is formed only by the insulator and the first electrode; and wherein the first electrode and the second electrode are configured to ionize gas within the cavity in response to an electrical current applied to the first electrode or to the second electrode. 2. The igniter assembly of claim 1 , wherein a longitudinal extent of the cavity is greater than the longitudinal extent of the outlet passage. 3. The igniter assembly of claim 2 , wherein the longitudinal extent of the cavity is about twice the longitudinal extent of the outlet passage. 4. The igniter assembly of claim 1 , wherein the first electrode comprises a center electrode, the second electrode comprises an outer shell electrode disposed circumferentially about the center electrode, and the insulator is disposed radially between the center electrode and the outer shell electrode. 5. The igniter assembly of claim 1 , wherein the maximum cross-sectional area of the cavity is more than two times greater than the cross-sectional area of the outlet passage. 6. The igniter assembly of claim 1 , wherein the outlet passage is the only fluid passage extending from the cavity. 7. An igniter assembly for a gas turbine combustor, comprising: a first electrode, a second electrode, and an insulator, wherein the first electrode, the second electrode, and the insulator form a cavity, the second electrode forms an outlet passage extending from the cavity to a tip of the igniter assembly, the outlet passage has a substantially constant cross-sectional area along a longitudinal extent of the outlet passage from the cavity to the tip of the igniter assembly, a maximum cross-sectional area of the cavity is greater than the substantially constant cross-sectional area of the outlet passage, the cavity includes a converging section having a cross-sectional area that decreases continuously from the maximum cross-sectional area of the cavity to the outlet passage, the converging section extends to an interface between the cavity and the outlet passage, the converging section is formed only by the second electrode, the cavity includes a substantially constant cross-sectional area section extending from the first electrode to the converging section, the substantially constant cross-sectional area section has a substantially constant cross-sectional area substantially equal to the maximum cross-sectional area of the cavity, and the substantially constant cross-sectional area section is formed only by the insulator and the first electrode; wherein the outlet passage is the only fluid passage extending from the cavity; and wherein the first electrode and the second electrode are configured to ionize gas within the cavity in response to an electrical current applied to the first electrode or to the second electrode. 8. The igniter assembly of claim 7 , wherein the first electrode comprises a center electrode, the second electrode comprises an outer shell electrode disposed circumferentially about the center electrode, and the insulator is disposed radially between the center electrode and the outer shell electrode. 9. The igniter assembly of claim 7 , wherein a longitudinal extent of the cavity is greater than a longitudinal extent of the outlet passage.
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