Design method for supercharging system of aviation piston two-stroke engine

A supercharging system and design method technology, which is applied in the direction of combustion engines, machines/engines, mechanical equipment, etc., can solve the problem of difficult to realize the power and economy of aviation piston two-stroke engines, long design period of supercharging system, and test volume Major problems, to achieve the effect of reducing the amount and cost of testing, shortening the research and development cycle, and strong versatility

Pending Publication Date: 2022-06-21
AEROSPACE TIMES FEIHONG TECH CO LTD
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Problems solved by technology

The supercharging system designed by this method has long design period, high trial production cost, and large amount of testing, and it is difficult to realize the optimal design of multi-objective parameters for power and economy of the aviation piston two-stroke engine under full operating conditions.

Method used

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  • Design method for supercharging system of aviation piston two-stroke engine
  • Design method for supercharging system of aviation piston two-stroke engine
  • Design method for supercharging system of aviation piston two-stroke engine

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Embodiment Construction

[0038] The technical solutions of the present invention will be further described below with reference to the accompanying drawings and specific embodiments.

[0039] The present invention provides a method for designing a supercharging system of an aviation piston two-stroke engine. Through the invention, the design process of the supercharging system can shorten the research and development period, reduce the trial production cost and reduce the Test the amount of experiments to improve design efficiency.

[0040] like figure 1 As shown, according to the design process of the aviation piston two-stroke engine supercharging system design method of the present invention, the design process specifically includes the following steps:

[0041] Determine the basic parameters and performance enhancement target parameters of the aviation piston two-stroke engine;

[0042] According to the basic parameters and performance optimization target parameters of the aviation piston two-st...

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Abstract

The invention discloses an aviation piston two-stroke engine supercharging system design method, and belongs to the technical field of aviation piston two-stroke engine supercharging system design. The method comprises the steps that basic parameters and performance strengthening target parameters of the aviation piston two-stroke engine are determined; selecting and matching a supercharger and preliminarily designing structural parameters of a resonant tube; determining common working condition parameters of the aviation piston two-stroke engine and a use weighted value of each working condition; optimizing structure parameters of the resonant tube through a genetic algorithm, and determining control target parameters; and according to a supercharger and the optimized resonance tube, a supercharging system is machined and assembled for the aviation piston two-stroke engine, and test verification is carried out. The design method of the aviation piston two-stroke engine supercharging system is suitable for an aircraft with high lift limit, high maximum level flight speed and long endurance, high comprehensive performance under all working conditions is considered, the design period is short, and the trial-manufacturing cost is low.

Description

technical field [0001] The invention belongs to the technical field of design of an aviation piston two-stroke engine supercharging system, and relates to a design method of an aviation piston two-stroke engine supercharging system. Background technique [0002] In the face of multi-scenario and multi-functional application requirements, the requirements of UAVs for high ceiling, high maximum level flight speed, and long endurance are increasing day by day. With the increase of the altitude and flight height of the take-off site, and affected by the decrease of environmental pressure, the naturally aspirated engine has problems such as reduced intake pressure, significant power attenuation, and poor high-altitude power, which seriously affects the ceiling and maximum level flight speed of the UAV. and flight time performance. The application of the supercharging system can effectively increase the intake pressure of the aviation piston two-stroke engine, restore its high-al...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F30/17G06F30/27G06N3/12F02B37/00G06F111/06
CPCG06F30/17G06F30/27G06N3/126F02B37/00G06F2111/06
Inventor 董雪飞陈建国王振宇从骁宇袁帅
Owner AEROSPACE TIMES FEIHONG TECH CO LTD
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