专利摘要:
A gas turbulator (21) is used in burners (20) of different kinds to obtain better combustion. The turbulator is placed in a chamber or passageway (10) for hot combustion gases. The turbulator fills the passageway forcing the gases to pass a double-walled unit comprising a first membrane wall (22) with radial slits (24) and another membrane wall (23) with a central exhaust opening (26). An expansion nozzle (27) is connected to this opening (26). The slits (24) have oblique wings (25) at least along one edge, which causes the gases to mix intensively within the space between the membrane walls (22, 23). These are during burning maintained at a high temperature, which garanties an efficient final combustion.
公开号:SU1753959A3
申请号:SU853990054
申请日:1985-12-13
公开日:1992-08-07
发明作者:Эстбо Нильс
申请人:Нильс Эстбо (SE);
IPC主号:
专利说明:

The invention relates to energy and can be used in combustion chambers for various purposes.
The purpose of the invention is to increase the thermal efficiency.
FIG. 1 shows a hot water boiler with a turbulator; in fig. 2 is a section A-A in FIG. one; in fig. 3 - part of the exhaust manifold of an internal combustion engine with turbulizers; in fig. 4 - exhaust manifold with one turbulator; in fig. 5 is a section BB in FIG. four.
The boiler contains a vertical combustion chamber 1 and an afterburning chamber 2, as well as smoke tubes 3 connected to the upper manifold 4 connected to the exhaust pipe 5. The smoke tubes 3 pass through the water collector 6 connected to the water jacket 7. The boiler is equipped pipelines 8, 9 supply and return of water. A burner 10 is installed in the upper part of the combustion chamber 1, and a turbulator 12 having an inlet section 13 and a diffusive outlet section 14 is installed in the channel 11 for the exit of combustion products. slots 16 and oblique bends 17. The visor 15 in the embodiment (FIG. 1) has a central control window 18. In the embodiment (FIG. 3), the turbulators 12 are installed in the exhaust pipes of the collecting manifold 20, and in the embodiment in FIG. 4 - in the common pipe 21 from the collector 22.
When the device, in which the turbulizer 12 is located, is operated, the latter heats up and contributes to the combustion of the gases passing through it, directing and turbulizing their flow. When the gases exit
vi ate
O5 O SL O
 WITH
through the turbulizer 12, due to its expanding form, the increase in speed is converted into pressure and the jet reaches the bottom of the afterburner chamber 2, where it is rapidly cooled, which reduces the content of nitrogen oxides in the exhaust gases.
权利要求:
Claims (3)
[1]
Claim 1. A turbulator installed in the channel for the exit of combustion products with its complete overlap and having an inlet section with a swirler and a diffuser outlet section11, characterized in that, in order to increase the thermal efficiency, the inlet section of the turbulizer is made
0
tapering, and the swirler is made in the form of a conical visor in contact with the inlet section only with its large base, and is provided with radial slots and inclined limb located at least on one side of each slot.
[2]
2, the turbulizer according to claim 1, in which the diffuser outlet section has a rounded end edge.
[3]
3.Turbulator on PP. 1 and 2, that is, with the fact that the swirler visor is made with a central control window.
L
 e flrA
fig 2
fig.Z
15
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同族专利:
公开号 | 公开日
NO156504B|1987-06-22|
ES8701357A1|1986-11-16|
AU4232285A|1985-11-15|
WO1985004947A1|1985-11-07|
FI854878A0|1985-12-10|
NO156504C|1987-09-30|
EP0176587A1|1986-04-09|
DK582985D0|1985-12-16|
JPS61501942A|1986-09-04|
AU577118B2|1988-09-15|
SE8402133D0|1984-04-17|
ES542111A0|1986-11-16|
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US4698016A|1987-10-06|
DK582985A|1985-12-16|
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EP0176587B1|1988-11-09|
SE8402133L|1985-10-18|
DE3566153D1|1988-12-15|
FI854878A|1985-12-10|
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HU197736B|1986-12-15|1989-05-29|Chinoin Gyogyszer Es Vegyeszet|Process for producing 5-hydroxy-pgf1 alpha-1,5-lakton derivatives|DE3608698C2|1986-01-18|1990-05-03|Deutsche Forschungsanstalt Fuer Luft- Und Raumfahrt Ev, 5300 Bonn, De|
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法律状态:
优先权:
申请号 | 申请日 | 专利标题
SE8402133A|SE442053B|1984-04-17|1984-04-17|turbulators|
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