Electromagnetic control type fuel injecting nozzle

A fuel nozzle and control technology, which is applied in the field of aviation engine fuel injection devices, can solve the problems of inability to accurately control the fuel supply, the inability to adjust the fuel supply, and the adjustment of engine power, etc., to improve fuel economy and simple structure , Sealing and reliable effect

Inactive Publication Date: 2008-12-31
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
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AI Technical Summary

Problems solved by technology

The disadvantage of this is that it is impossible to precisely control the fuel supply to adjust the engine power. At the same time, due to the adjustment characteristics of the qualitative variables of the carburetor, it is impossible to adjust the fuel supply in real time according to the actual working conditions of the engine.
[0003] In addition, the naturally aspirated fuel supply system injects the oil-air mixture into the cylinder. During the exhaust stroke, a part of the oil-air mixture will be directly discharged out of the cylinder with the exhaust gas, causing pollution and waste, because during the scavenging process of the two-stroke engine For a period of time, the intake port is open while the exhaust port is open, so that a part of the mixed gas newly entering the cylinder is directly discharged out of the cylinder body

Method used

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  • Electromagnetic control type fuel injecting nozzle
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  • Electromagnetic control type fuel injecting nozzle

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Embodiment Construction

[0013] The present invention will be further described below in conjunction with the accompanying drawings.

[0014] The present invention provides an electromagnetically controlled fuel nozzle. The nozzle structure includes an upper casing 1, a lower casing 2, a coil frame 3 and a magnetic yoke 4, such as figure 1 As shown, the upper shell 1 and the lower shell 2 are welded. The bobbin 3 is welded outside the upper casing 1 and the lower casing 2, and the electromagnetic coil is wound on the bobbin 3; the yoke 4 is divided into two parts, which are symmetrically welded on the surfaces of the upper casing 1 and the lower casing 2 , the electromagnetic coil is enclosed between the inside of the yoke 4 and the coil frame 3 . Such as figure 2 Shown is the axial sectional view of the electronically controlled fuel nozzle of the present invention, as can be seen from the figure, an oil inlet 101 is arranged at the upper end of the upper housing 1, and an injection hole 5 is arra...

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Abstract

The invention discloses an electromagnetic control fuel-oil nozzle; the nozzle comprises an upper shell body, a lower shell body, a coil reel and a magnet yoke; the upper shell body is welded with the lower shell body; the coil reel is welded out of the upper shell body and the lower shell body; an electromagnetic coil is winded on the coil reel; the magnet yoke is divided into two parts which are symmetrically welded on the surfaces of the upper shell body and the lower shell body; the electromagnetic coil is wrapped between the interior of the magnet yoke and the coil reel. A valve core body is composed of a valve core head, a valve core rod and a steel ball which are welded together from top to the bottom; a spring is arranged between the valve core and the upper shell body. The electromagnetic control fuel-oil nozzle has the advantages of simple structure, reliable sealing, high response frequency, low manufacturing cost, improving the duration performance of the airplane while improving the fuel oil economy and reducing the exhaust of the engine.

Description

technical field [0001] The invention relates to an electromagnetically controlled fuel nozzle, in particular to an electromagnetic fuel nozzle used in an electronically controlled fuel injection system of an aviation two-stroke gasoline engine, and belongs to the technical field of aviation engine fuel injection devices. Background technique [0002] The fuel supply devices of micro gasoline engines used in the domestic aviation field all use carburetors to mix fuel and air into the cylinders, and control the amount of mixed gas supplied by adjusting the opening of the throttle valve, thereby controlling the power of the engine . The disadvantage of this is that it is impossible to accurately control the fuel supply to adjust the engine power. At the same time, due to the adjustment characteristics of the qualitative variables of the carburetor, it is impossible to adjust the fuel supply in real time according to the actual working conditions of the engine. [0003] In addi...

Claims

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Application Information

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IPC IPC(8): F02M51/06F02M61/20
Inventor 杜发荣陈巍韩树军张奇丁水汀徐国强
Owner BEIHANG UNIV
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