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Direct jet aircraft stove burner

A burner and aircraft technology, which is applied in the field of household gas stoves, can solve the problems of weak flames in the structure of aircraft burners

Pending Publication Date: 2019-11-08
杭正荣
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The current structure of the aircraft furnace head is weak

Method used

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  • Direct jet aircraft stove burner
  • Direct jet aircraft stove burner

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Experimental program
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Effect test

Embodiment Construction

[0012] Center fire nozzle 2 is contained on the plane nozzle hole on the center fire gas inlet 6 on the burner head 1, corresponds to the lower opening of center fire guideway 4. The outer ring fire nozzle 3 is contained on the upper left plane nozzle hole of the outer ring fire gas inlet 7, corresponding to the lower opening of the outer ring fire guideway 5. The air inlet 10 is the space between the lower opening of the center fire injection channel 4 and the outer ring fire injection channel 5 and the center fire nozzle 2 and the outer ring fire nozzle 3 .

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Abstract

The invention discloses a direct jet aircraft burner, and belongs to the technical field of household gas stoves. The direct jet aircraft burner is composed of a furnace burner nozzle component. The furnace burner is provided with two ejecting channels for central fire and outer ring fire, a fuel gas inlet and an air inlet. The direct jet aircraft burner has the remarkable effects of changing thestructure of a traditional aircraft furnace burner, the fuel gas jetting is strong, and the flame temperature is high.

Description

[0001] Technical field [0002] The innovation belongs to the technical field of household gas stoves Background technique [0003] The current structure of the aircraft furnace head is weak Contents of the invention [0004] A direct-injection aircraft burner is provided now, and the technical solution for solving its technical problems is composed of a burner and a nozzle component. On the burner, there are a center fire injection channel, an outer ring fire injection channel, a gas inlet, an air inlet and a mating surface with the burner of a general-purpose aircraft. [0005] The two nozzles are installed on the two nozzle holes on the upper plane of the two gas inlets, corresponding to the lower openings of the two ejector channels, and the space between the two nozzles and the lower ports of the two ejector channels is the air inlet. [0006] The remarkable effect of this innovation is due to the change of the structure of the traditional aircraft burner, so that the...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F23D14/04
CPCF23D14/04
Inventor 杭正荣
Owner 杭正荣
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