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Afterburner adopting planar fan nozzles for oil supply

An afterburner and fan-shaped nozzle technology, applied in the field of aero-engines, can solve the problems of small nozzle diameter, small fuel spray expansion angle, poor nozzle atomization effect, etc., to improve combustion characteristics, reduce the number of nozzles, and achieve radial distribution. uniform effect

Active Publication Date: 2018-11-20
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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Problems solved by technology

[0003] At present, the fuel injection rod in the afterburner chamber of the common turbofan engine usually adopts a direct injection fuel nozzle, the fuel spray has a small expansion angle, the atomization effect is poor, and the equivalent diameter of the nozzle is small, which can easily lead to nozzle blockage, which is serious Affect the stability and reliability of the engine combustion chamber
With the rapid development of aviation technology, modern advanced fighters have higher and higher requirements on the performance of aero-engines. The direct nozzles on the fuel injection rods in the traditional afterburner have poor atomization effect, which can easily lead to clogging and coking when heated. , The problem of uneven radial and circumferential concentration distribution of fuel is becoming more and more prominent, which is not conducive to the reliable and stable combustion of the afterburner, and seriously affects the overall performance of the aero-engine

Method used

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  • Afterburner adopting planar fan nozzles for oil supply
  • Afterburner adopting planar fan nozzles for oil supply
  • Afterburner adopting planar fan nozzles for oil supply

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Embodiment Construction

[0024] In order to make the object, technical solution and effect of the present invention clearer and clearer, the present invention will be further described in detail below with reference to the accompanying drawings and examples. It should be pointed out that the specific implementations described here are only used to explain the present invention, not to limit the present invention.

[0025] Such as figure 1 As shown, in the afterburner of the present invention, which adopts a flat fan-shaped nozzle to supply oil, a low-pressure compressor 1 and a high-pressure compressor 2 are arranged in sequence along the outlet of the air inflow direction 100 (the direction indicated by the arrow in the figure). The main combustion chamber 3 connected to the high-pressure compressor 2; the main combustion chamber 3 is connected to the turbine 4, and a blender 5 is arranged between the turbine 4 and the side wall of the afterburner 8; after the blender 5, a diffuser section 6 is forme...

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Abstract

The invention discloses an afterburner adopting planar fan nozzles for oil supply, and belongs to the field of aero-engines. The afterburner adopting the planar fan nozzles for oil supply is characterized in that supporting plates are arranged on an oil supply device in the afterburner, and are uniformly arranged along the circumference of the afterburner in the perpendicular direction; and oil spraying rods are arranged on the inner sides of the supporting plates in the radial direction, the planar fan nozzles are arranged on the side walls of the oil spraying rods in the radial direction, and the opening cross section of each planar fan fuel nozzle is V-shaped. According to the design of the afterburner adopting the planar fan nozzles for oil supply, the fuel spray extending angle is enlarged, the number of the nozzles is reduced, the diameter of each nozzle is increased, and meanwhile, the fuel radial and circumferential concentration distribution is more uniform, so that reliable and stable combustion of the afterburner is facilitated, and the problems in the prior art are solved.

Description

technical field [0001] The invention belongs to the field of aero-engines, and specifically refers to an afterburner which adopts a flat fan-shaped nozzle for oil supply. Background technique [0002] Since the last century, the afterburner has been more and more widely used in aero-engines. In order to improve the combat performance and flight envelope of military fighter jets, it is necessary to increase the fuel atomization effect in the afterburner chamber so that the fuel and air are completely mixed and the fuel is evenly distributed in space. The quality of the fuel atomization effect determines the quality of the combustion chamber's working characteristics. Therefore, fuel atomization research is a very important part of aero-engine research. [0003] At present, the fuel injection rod in the afterburner chamber of the common turbofan engine usually adopts a direct injection fuel nozzle, the fuel spray has a small expansion angle, the atomization effect is poor, a...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F23R3/28
CPCF23R3/28
Inventor 韩宗英颜应文刘云鹏李井华刘勇
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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