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Heavy-oil aero-engine and aircraft

A technology of aero-engine and heavy oil, applied in engine components, machines/engines, and bringing fuel into the engine through high-pressure gas. and other problems, to achieve the effect of smooth drainage, reducing the risk of knocking, and improving the impact effect.

Pending Publication Date: 2018-09-28
CHONGQING LONCIN ENGINE +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, due to the nature of the heavy oil itself, it cannot reach the atomization level of general oil products, and it cannot be mixed evenly with the combustion air. The original EFI ignition method cannot be used when ignition is started; even if the ignition method is used for operation , it will also cause a series of engine problems due to insufficient combustion, unable to achieve reliable atomization of heavy oil and unable to organize efficient combustion of mixed fuel, which makes the power, economy and emission of heavy oil used in engines unable to meet expectations effect, so that the application of heavy oil cannot be widely popularized

Method used

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  • Heavy-oil aero-engine and aircraft
  • Heavy-oil aero-engine and aircraft
  • Heavy-oil aero-engine and aircraft

Examples

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Embodiment Construction

[0022] As shown in the figure: the heavy oil aircraft engine of the present embodiment includes a cylinder block 5, a cylinder head 13 and a piston assembly. As shown in the figure, the piston of the piston assembly is located in the cylinder block 1, and the cylinder head 13 is provided with a The fuel injection assembly that is sprayed into the combustion chamber 11; the top surface of the piston is provided with an annular guide portion that is annularly sunken along the circumferential direction (concentric with the piston top surface), and the annular guide portion corresponds to the injection direction of the fuel injection assembly (referring to When the fuel assembly is injected, and the position of the piston makes the outer surface of the annular guide part correspond to the injection direction), the center of the annular guide part (generally also the center of the top surface of the piston) forms a guide protrusion 12, and the guide protrusion 12 is due to the The t...

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Abstract

The invention discloses a heavy-oil aero-engine and an aircraft. The heavy-oil aero-engine comprises a cylinder body, a cylinder head and a piston assembly, wherein a fuel injection assembly injectinga fuel into a combustion chamber is arranged on the cylinder head; and an annular guide part annularly sunken in the circumferential direction is arranged on the top surface of a piston, the outer side surface of the annular guide part corresponds to the injection direction of the fuel injection assembly, and a guide bulge is formed at the centre of the annular guide part. According to the heavy-oil aero-engine and the aircraft, the injected fuel is guided to an ignition area of a spark plug, the top surface of the piston is optimized, and then the combustion chamber is optimized, the compression ratio is changed, and the knock risk is lowered; and meanwhile, a tumbling effect is improved, adequate atomization mixing for heavy oil can be realized, uniform combustion mixed gas is formed after good mixing, and the fuel can further be organized for efficient combustion, so that the dynamic property, the economical efficiency and the emission performance of the heavy oil applied to an engine are ensured, and the energy conservation, the environment friendliness and the low cost of the heavy oil after being applied to the engine are realized.

Description

technical field [0001] The invention relates to an engine and its application, in particular to a heavy oil aeroengine and an aircraft. Background technique [0002] As the fuel for engines, heavy oil will become the power trend of small and medium-sized aircraft; however, heavy oil has high viscosity and poor low-temperature fluidity, which leads to poor atomization effect compared with ordinary light oil, which affects the combustion effect, and even causes difficulty in starting the engine and poor emission. Up to standard. [0003] In the prior art, in order to ensure good atomization and start-up of heavy fuel oil engines, there are fuel supply methods such as carburetor + auxiliary preheating technology, mechanical injection (fuel direct injection), electronically controlled fuel injection, etc. However, due to the nature of the heavy oil itself, it cannot reach the atomization level of general oil products, and it cannot be mixed evenly with the combustion air. The o...

Claims

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Application Information

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IPC IPC(8): F02F3/28F02M67/02F02F1/24
CPCF02F1/242F02F3/28F02M67/02
Inventor 翟明明石晓东唐程刘小林闪颂武罗晏林成
Owner CHONGQING LONCIN ENGINE
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