Rotary hearth furnace
US-10294535-B2 · May 21, 2019 · US
US10066873B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10066873-B2 |
| Application number | US-57932704-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 16, 2004 |
| Priority date | Nov 18, 2003 |
| Publication date | Sep 4, 2018 |
| Grant date | Sep 4, 2018 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
[Problems] A combustion gas extraction probe that is capable of preventing burnout of a head metal portion of a probe, capable of rapidly cooling a high-temperature gas in a uniform manner in a probe, and whose outer diameter can be kept small. [Means for Solving Problems] A combustion gas extraction probe ( 4 ) having a hollow-cylindrical inner tube ( 4 a ) in which a high-temperature combustion gas flows, a hollow-cylindrical outer tube ( 4 b ) surrounding the inner tube ( 4 a ), a low-temperature gas discharge hole ( 4 c ) provided in the inner tube ( 4 a ), and a low-temperature gas supply means ( 9 ) for supplying a low-temperature gas between the inner tube ( 4 a ) and the outer tube ( 4 b ) and discharging the low-temperature gas from the discharge hole ( 4 c ) into the direction that is substantially perpendicular to the sucking direction of the high-temperature combustion gas and is toward the center of the flow of said high-temperature combustion gas. Alternatively, plural discharge holes ( 4 c ) may be provided, where the individual discharge holes ( 4 c ) are arranged at substantially the same positions from the head of the probe in the high-temperature combustion gas sucking direction, or alternatively, the discharge holes ( 4 c ) may be arranged in stages in the high-temperature combustion gas sucking direction. The flow speeds of the low-temperature gas and the high-temperature combustion gas are preferably not less than 40 m/s and not more than 100 m/s.
Opening claim text (preview).
The invention claimed is: 1. A combustion gas extraction probe for extracting a high-temperature combustion gas while cooling said high-temperature combustion gas with a low-temperature gas characterized by: an outer tube; and a metal inner tube positioned within the outer tube to define a cooling fluid passage therebetween, the metal inner tube being of unitary construction and having an inner diameter defining a flow path area substantially along the entire tube and through which extracted high-temperature combustion gas flows, the metal inner tube configured to emit low-temperature gas into the flow path area only in a single transverse plane generally perpendicular to a sucking direction of the high-temperature combustion gas, the inner tube having a plurality of low-temperature discharge holes in direct fluid communication with the cooling fluid passage and the flow path area and spaced from a sucking end of the inner tube and disposed about respective axes aligned within a single plane for emitting said low-temperature gas so as to flow in a direction that is substantially perpendicular to the sucking direction of the high-temperature combustion gas and is toward a center of a flow of said high-temperature combustion gas such that said low-temperature gas reaches the centermost portion of said high-temperature combustion gas to create a single transverse sheet of low-temperature gas for mixed cooling and that all vector components of said low-temperature gas emitted into the high-temperature gas and parallel to the flow direction of said high-temperature gas are in a downstream direction of the high-temperature combustion gas; and a plurality of collars coupled to the inner tube and disposed about respective ones of the plurality of low-temperature discharge holes, each collar being disposed about a respective axis which is perpendicular to the sucking direction of the high-temperature combustion gas; the inner tube being independent of a discharge hole disposed about an axis spaced from the single plane and arranged perpendicular to the inner tube. 2. The combustion gas extraction probe as claimed in claim 1 comprising: a low-temperature gas supply means for supplying the low-temperature gas between the inner tube and the outer tube, and discharging the low-temperature gas from the discharge hole into the inner tube; the inner tube being connected to the outer tube such that all of the low-temperature gas flowing in the inner tube passes through the plurality of low-temperature gas discharge holes. 3. The combustion gas extraction probe as claimed in claim 2 , wherein individual discharge holes are rotationally symmetrically arranged at substantially the same positions from a head of the probe in the high-temperature combustion gas sucking direction. 4. The combustion gas extraction probe as claimed in claim 2 , wherein the outer tube defines a closed end. 5. The combustion gas extraction probe as claimed in claim 4 , wherein the inner tube defines an open end through which the high-temperature combustion gas enters the inner tube. 6. The combustion gas extraction probe as claimed in claim 5 , wherein the closed end of the outer tube circumnavigates the open end of the inner tube. 7. The combustion gas extraction probe as claimed in claim 2 , wherein: the inner tube terminates to define an inner entrance end through which the high-temperature gas enters the inner tube, the inner entrance end defining an inner entrance plane; and the inner and outer tubes are configured such that the low-temperature gas does not traverse the inner entrance plane. 8. The combustion gas extraction probe as claimed in one of claims 1 - 2 and 3 , wherein flow speeds of the low-temperature gas and the high-temperature combustion gas are not less than 40 m/s and not more than 100 m/s. 9. The combustion gas extraction probe as claimed in one of claims 1 and 3 , characterized by having a blaster injecting compressed air in an opposite direction to the sucking direction of the high-temperature combustion gas at a head of the probe. 10. The combustion gas extraction probe as claimed in claim 1 , wherein the low-temperature gas is emitted along at least two intersecting axes. 11. The combustion gas extraction probe as claimed in claim 10 , wherein the low-temperature gas is emitted along at least two perpendicular axes. 12. The combustion gas extraction probe as claimed in claim 1 , wherein the low-temperature gas is emitted into the high-temperature combustion gas to cool a peripheral portion of the high-temperature combustion gas as well as a central portion of the high-temperature combustion gas.
Processes · CPC title
of jets leaving an orifice · CPC title
Mechanical Engineering · mapped topic
Arrangements of cooling devices · CPC title
With selectively operated flow control means · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.