Combustor
US-2024191874-A1 · Jun 13, 2024 · US
US10288292B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10288292-B2 |
| Application number | US-201614996510-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 15, 2016 |
| Priority date | Jan 15, 2016 |
| Publication date | May 14, 2019 |
| Grant date | May 14, 2019 |
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Official abstract text for this publication.
A swirler includes a swirler body defining a longitudinal axis. A stack of swirler plates is assembled to the swirler body stacked in a direction along the longitudinal axis. Each of the swirl plates defines a vane portion. The swirler plates are mounted rotated circumferentially about the longitudinal axis relative to neighboring ones of the swirler plates so the vane portions form a swirler vane.
Opening claim text (preview).
What is claimed is: 1. A swirler comprising: a swirler body defining a longitudinal axis; and a stack of swirler plates assembled to the swirler body stacked in a direction along the longitudinal axis, wherein each of the swirl plates defines a vane portion, and wherein the swirler plates are mounted stationary with respect to the swirler body, and wherein each of the swirler plates is angled circumferentially about the longitudinal axis relative to neighboring ones of the swirler plates so the vane portion forms a swirler vane, wherein the swirler plates are identical to one another and further comprising an end swirler plate at one end of the stack of swirler plates, wherein the end swirler plate includes a swirl vane portion positioned to form part of the swirler vane, wherein the end swirler plate differs from the swirler plates of the stack of swirler plates in at least one of material or axial thickness. 2. The swirler as recited in claim 1 , wherein each of the swirler plates includes a plurality of vane portions, and wherein the respective vane portions of the swirler plates form a plurality of respective swirler vanes. 3. The swirler as recited in claim 1 , wherein each of the swirler plates includes a peripheral ring, wherein the vane portion of the swirler plates extends radially inward from the respective peripheral ring. 4. The swirler as recited in claim 1 , wherein each of the swirler plates includes at least one alignment tongue engaged with an alignment grove defined in the swirler body for registration of the swirler plates to form the swirler vane. 5. The swirler as recited in claim 4 , wherein the alignment tongue of each of the swirler plates is positioned circumferentially relative to the respective vane portion in a circumferential location common to all of the swirler plates, and wherein the alignment grove of the swirler body is profiled to define the swirler vane by registration of the at least one alignment tongue with the alignment groove. 6. The swirler as recited in claim 1 , wherein the swirler body defines an annular flow passage therethrough, wherein the stack of swirler plates is mounted within the annular flow passage to impart swirl on fluids flowing through the annular flow passage.
Fuel flow conduits, e.g. manifolds · CPC title
producing a swirling discharge · CPC title
in gas turbines · CPC title
having fuel-air premixing devices (F23R3/30 takes precedence) · CPC title
by using swirl vanes · CPC title
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