산업용,공학용,교육용 소프트웨어 선두주자 김화기술, maple, tecplot, dymola

IOSO 소개

IOSO NM

IOSO 기술세미나

IOSO 자료실

제조사홈페이지

IOSO 응용범례

항공우주 (PDF 4.7MB)

자동차 (PDF 300KB)

재료소재 (PDF 200KB)

전자냉각 (PDF 2MB)

광학시스템 (PDF 150KB)

교량디자인 (PDF 300KB)

건설 건축 (PDF 200KB)

Increasing of effectiveness of complicated technical system
by application of IOSO Technology

Object	Problem	The achieved result
Gas-turbine engine	The improving of engines fan effectiveness		The increasing in the fan efficiency up to 3% was achieved by optimal profiling of its blades vanes and passage, which allowed to have the optimal distribution of compression work between the stages and by the radius. Dimensionality - up to 63.
	The improving of engines fuel economy at throttled operating modes		The optimal control laws of engines passage controllable elements were obtained, which allowed to decrease the specific fuel consumption at throttled operating modes up to 8% due to optimal coordination of engines functional elements work. Dimensionality - up to 14.
	The decreasing of engines acceleration time		The optimal time control laws of passage controllable elements were achieved, which allowed to decrease the acceleration time 1.5 times as less due to optimal coordination of all control efforts during transitional process. Dimensionality - 20.
Multistage axial flow compressor for engine with high bypass ratio	The improving of the high pressure compressor effectiveness		The high pressure compressor efficiency was increased by 1.5% due to its optimal profiling. The rise of effectiveness was reached due to optimal coordination of gas-dynamic parameters of work of elementary vanes in a system of the compressor. Dimensionality - up to 96.
	The improving of middle pressure compressor effectiveness		The middle pressure compressor efficiency was increased by 1.7% due to optimal control laws of its stator blades. The optimal structure of compressors stator blades control was determined. The rise in effectiveness was provided by optimal distribution of compression work between compressors stages. Dimensionality - 5.
Heat machine	Remaking of aircraft engine without operational resource in heat machine with minimal modifications		The fuel economy of heat machine was improved by more then 10%. Optimal coordination of components of engines without operational resource was carried out for their operation in a complex of heat machine.
The technological process	Improving of metal structures welding technologies		Just in industrial process due to optimal coordination of 13 technological parameters the improving of strength indicators of metal structures welded joint by 14% was achieved.
Gas-turbine engine with high bypass ratio	The increasing of engines fan effectiveness at engines take-off and cruising operating modes simultaneously		The means was proposed to increase fans rotor efficiency by 2.5% for engines take-off operating mode and by 2% for its cruising operating mode by means of optimal profiling of fans rotor blades. The advantage in effectiveness was reached due to optimal distribution of rotor blades work by the radius. Dimensionality-19.
Military aircraft	Improving of aircraft maneuverability		Optimal control laws of power plant controllable elements and of the aircraft were determined, which allowed to reduce the time of aerobatics maneuvers making by 5-10%. The dimensionality of optimization problems - up to 70 variables.
automobile engine	Insurance of best fuel economy under securing of required level of exhaust toxicity (NOx, COetc.).		Engines fuel economy was improved by up to 6%. Optimal calibration of electronic fuel supply and ignition control system was carried out. Dimensionality - up to 6.
Multilayer optical coverings	Insurance of minimal values of reflection (adsorption) ratios of the surface in given range of wave lengths.		Optimal values of surface multilayer optical covering layer thickness were determined, which assured the considerable reducing of reflection ratio on given range of wave length. The dimensionality of optimization problems - up to 96 variables.
STOVL aircraft power plant	Improving of aircraft take-off performance for its short take-off		There were determined optimal time control laws of 7 controllable elements of power plant passage, of angles of nozzles setting and aircraft pitch, which allowed to reduce the length of take-off run by 2.5 times comparing with ordinary power plant control. Dimensionality - 49 variables.
All-wheels driven car transmission	Increasing of wear-resistance and durability of automobile transmission parts.		Optimal values of car transmis- sion 38 structure-arrangement parameters were determined, insuring improving of 5 effecti- veness indicators by 6 to 85%.
Multistage axial flow compressor	The increasing of the compressor efficiency for the design-point operating mode.		The solution was obtained, which improved the compressor efficiency up to 4% for the design-point operating mode. The optimal profiling of the compressor blade rows was performed, which allowed to redistribute optimally the work of stages. Dimensionality - 140.
	The search of a compromise between the compressor efficiency and stall margin.		4 non-improvable (Pareto- optimal) solutions were found, ensuring the compromise between the compressor efficiency and stall margin for the design-point operating mode. Dimensionality - 140.
	The increasing of the compressor efficiency for the off-design operating modes.		The optimal control laws of the compressor stator blades were found, which allowed to improve the compressor efficiency up to 2.4% for the off-design operating modes.
	The increasing of the probability of the compressor design parameters practical implementation.		The optimal profiling of the compressor blade rows was performed taking into account their manufacturing accuracy. For the first time the multicriteria stochastic optimization problem has been solved with the dimensionality of 140 variables and 3 criteria. There was obtained the set of Pareto- optimal solutions by the criteria: the efficiency, the probability of constraints keeping, the effectiveness parameters spread.