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Liquid hydrogen fuel carrying and heat exchanging system of hydrogen fuel high speed airplane

A liquid hydrogen, high-speed technology, applied in the field of aircraft, can solve the problems of aero-engines that do not have high power, pollution-free portable power supply, limited calorific value per unit mass, and increased take-off weight of aircraft, achieving significant economic and social benefits. Effects of eliminating air pollution and reducing take-off weight

Inactive Publication Date: 2006-06-14
SHANGHAI JIAO TONG UNIV
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Problems solved by technology

[0002] At present, aircraft engines are powered by conventional fuels, which are increasingly in short supply and cause air pollution
The calorific value per unit mass of conventional fuel is limited, and the carrying of fuel causes a substantial increase in the take-off weight of the aircraft. The "green variable aero-engine" with the patent number 97235783.1 in the existing technology proposes to provide power with an engine of a sustainable power generation device to reduce environmental pollution. pollution, but because there is currently no high-power, non-polluting portable power source to drive the aero-engine, the plan cannot be put into practice
The use of hydrogen fuel can not only avoid air pollution, but also alleviate the pressure of conventional energy shortages. However, liquid hydrogen has a low calorific value per unit volume, a large carrying volume, and low storage temperature, so it cannot be used directly. At present, there is no technology to overcome the above difficulties

Method used

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  • Liquid hydrogen fuel carrying and heat exchanging system of hydrogen fuel high speed airplane

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Embodiment Construction

[0008] The specific implementation of the present invention will be further described below in conjunction with the accompanying drawings.

[0009] Such as figure 1 As shown, the present invention mainly includes: main liquid hydrogen storage tank 1, wing liquid hydrogen storage tank group 2, fuselage liquid hydrogen storage tank group 3, stop valves 4, 5, 6, liquid hydrogen main pipe 7, first evaporator 8. Second evaporator 9, engine combustion chamber 10, hydraulic oil heat exchanger 11, lubricating oil heat exchanger 12, hydraulic system 13, fans 14, 15, lubrication system 16.

[0010] The main liquid hydrogen storage tank 1 is placed in the fuel tank of the aircraft, the wing liquid hydrogen storage tank group 2 and the fuselage liquid hydrogen storage tank group 3 are a group of boxes made according to the shape of the wing and the fuselage respectively, and are placed in Inside the wings and fuselage. The wing liquid hydrogen storage tank group 2 and the fuselage liqui...

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Abstract

A liquefied hydrogen fuel carrying and heat exchanging system for high-speed airplane using hydrogen as fuel is composed of master liquefied hydrogen tank, the liquefied hydrogen tanks hidden in wings, the liquefied hydrogen tanks hidden in main body, cut-off valves, liquefied trunk, two evaporators, combustion chamber of engine, hydraulic oil heat exchanger, lubricating oil heat exchanger, hydraulic system, fans and lubricating system. It features that the cold of liquefied hydrogen is transferred to hydraulic system and lubricating system.

Description

technical field [0001] The invention relates to a liquid hydrogen fuel carrying and heat exchange system, in particular to a liquid hydrogen fuel carrying and heat exchange system for a hydrogen-burning high-speed aircraft, and belongs to the technical field of aircraft. Background technique [0002] At present, aircraft engines are powered by conventional fuels, which are increasingly in short supply and cause air pollution. The calorific value per unit mass of conventional fuel is limited, and the carrying of fuel causes a substantial increase in the take-off weight of the aircraft. The "green variable aero-engine" with the patent number 97235783.1 in the existing technology proposes to provide power with an engine of a sustainable power generation device to reduce environmental pollution. pollution, but because there is no high-power, non-polluting portable power source to promote the aero-engine at present, the scheme cannot be put into practice. The use of hydrogen fue...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D37/30
CPCY02T90/40
Inventor 马捷戴斌
Owner SHANGHAI JIAO TONG UNIV
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