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Instantaneous energy efficiency optimization method for comprehensive integrated heat/energy system of airplane

An energy management system and aircraft technology, applied in the direction of control/regulation system, general control system, instrument, etc., can solve the problems of lack of research on comprehensive integrated heat/energy optimization control methods, solve the problem of power source distribution, and ensure accurate Search, the effect of improving fuel economy

Active Publication Date: 2021-11-19
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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Problems solved by technology

[0003] Judging from the research status at home and abroad, the research on the energy distribution management of the integrated heat / energy system is still limited to the introduction of key technologies, and the research on the optimal control method of the integrated heat / energy is relatively lacking.

Method used

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  • Instantaneous energy efficiency optimization method for comprehensive integrated heat/energy system of airplane
  • Instantaneous energy efficiency optimization method for comprehensive integrated heat/energy system of airplane
  • Instantaneous energy efficiency optimization method for comprehensive integrated heat/energy system of airplane

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Embodiment Construction

[0078] The technical solution of the invention will be described in detail below in conjunction with the accompanying drawings.

[0079] In this embodiment, the instantaneous energy efficiency optimization method based on multiple evaluation objectives is applied to the integrated thermal / energy system of the aircraft, such as figure 1 As shown, the comprehensive integrated heat / energy system is divided into two units, namely a semi-closed air refrigeration cycle unit and a combined power unit. In the figure, ISG is the integrated starter / generator, C is the compressor, CT is the cooling turbine, and PT is the power turbine. The combined power unit includes a compressor, an integrated starter / generator, a cooling turbine, a power turbine, and a dual-mode combustor, which provide power for the entire system and are the core components of the aircraft's integrated thermal / energy system. The semi-closed air cooling cycle unit draws air from the main engine or the outside atmosph...

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Abstract

The invention discloses an instantaneous energy efficiency optimization method for a comprehensive integrated heat / energy system of an airplane, relates to a comprehensive integrated heat / energy management technology of the airplane, and belongs to the technical field of calculation, reckoning or counting. According to the method, in a high dynamic environment, multiple evaluation targets such as system fuel consumption rate, engine stability margin and the like are considered for an aircraft comprehensive integrated heat / energy system, optimization constraint conditions are determined, system power source distribution is optimized by adopting a dynamic particle swarm optimization algorithm based on double-population coevolution combinatorial variation, power source modes such as bleed air extraction, shaft work extraction and fuel oil combustion are comprehensively regulated, controlled and distributed, a power source distribution scheme with the optimal energy efficiency is obtained, and the system meets the requirement for multiple evaluation targets. According to the method, the fuel economy of the comprehensive integrated heat / energy system of the aircraft can be improved on the basis of ensuring the stability margin of the engine.

Description

technical field [0001] The invention discloses an instantaneous energy efficiency optimization method for an aircraft integrated heat / energy system, relates to an aircraft integrated heat / energy technology, and belongs to the technical field of calculation, calculation or counting. Background technique [0002] In order to meet the development needs of energy-optimized aircraft, the multi-electric and integrated technology of airborne systems has become the focus of current research. The new integrated thermal / energy system is regarded as an important development direction of integrated thermal / energy management technology for airborne systems. It integrates the functions of the emergency power system, auxiliary power system and environmental control system in the traditional airborne The integrated combined power unit realizes the cross-linking and optimal management of multiple energy forms in the system, and uses multiple heat sink forms such as fuel oil and fan ducted ai...

Claims

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Application Information

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IPC IPC(8): G05B13/04
CPCG05B13/042
Inventor 张镜洋傅杰城郑峰婴陈宇昂金行健何中泽施良宇骆必泰
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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