Igbt temperature dampening systems and methods
US-2024397678-A1 · Nov 28, 2024 · US
US9326367B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9326367-B2 |
| Application number | US-201314090577-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 26, 2013 |
| Priority date | Jul 25, 2013 |
| Publication date | Apr 26, 2016 |
| Grant date | Apr 26, 2016 |
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In some aspects, nozzles for gas-cooled plasma torches can include a body having a first end and a second end that define a longitudinal axis; a plenum region substantially formed within the body that extends from the first end and is configured to receive a plasma gas flow; an exit orifice located at the second end oriented substantially coaxially with the longitudinal axis, the exit orifice fluidly connected to the plenum region; and a feature on an outer surface of the body to increase cooling by receiving a high velocity cooling gas flow flowing in a direction along a length of the body, an impingement surface of the feature to receive the cooling gas flow at a substantially perpendicular direction relative to the impingement surface and to redirect the cooling gas flow to promote cooling and uniform shield flow.
Opening claim text (preview).
What is claimed: 1. A nozzle cooling system for a plasma arc torch comprising: a nozzle having a body with a first end and a second end that define a longitudinal axis, a plenum region substantially formed within the body, the plenum region extending from the first end of the body and configured to receive a plasma gas flow, an exit orifice located at the second end of the body and oriented substantially coaxially with the longitudinal axis, the exit orifice fluidly connected to t…
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