Helicopter temperature regulation and oil tank explosion-proof system

Abstract

The invention discloses a helicopter temperature regulation and oil tank explosion-proof system which comprises a first-stage compressor, a condenser, a second-stage compressor, a first-stage evaporation refrigeration cycle system, a second-stage evaporation refrigeration cycle system, a cooling inerting module, a cabin pressurization system and a main controller. The first-stage evaporation refrigeration cycle system is connected with the cabin pressurization system, and a generated cooling capacity is used for reducing the temperature of a passenger cabin and a cabin; the second-stage evaporation refrigeration cycle system is connected with the cooling inerting module; the cooling inerting module is used for inerting liquid fuel oil in an onboard oil tank; and high-temperature and high-pressure refrigerant steam output by a first-stage compressor is condensed through a condenser and then subjected to pressure reduction treatment, one part of the steam is output to a first-stage evaporation cold circulation system, and the other part of the steam is output to a second-stage evaporation cold circulation system. The system solves the problem of insufficient air entraining pressure of the helicopter, reduces the total weight of an environment control system and an inerting system, and has the advantages of simple structure, reliable performance, safety, environmental protection and convenience in installation and maintenance.

Description

technical field [0001] The invention relates to a temperature regulation and explosion-proof system, in particular to a helicopter temperature regulation and fuel tank explosion-proof system. Background technique [0002] With the opening of low-altitude airspace in our country, the future development potential of civil helicopters is huge. In recent years, helicopters have been widely used in law enforcement, ambulance, agriculture, military, transport patrol, tourism and so on. A helicopter is an aircraft that is powered by a turbine engine in the form of a rotating output shaft and directly drives the rotor through a mechanical transmission system to generate lift and propulsion. It is a flight action that cannot be accomplished by conventional fixed-wing aircraft. As a special-purpose aircraft, the improvement and perfection of helicopter equipment has always been the key development goal of various countries. Installing the environmental control system on the helicop...

AI Technical Summary

Problems solved by technology

However, there are still some problems with this technology, such as the need to bleed a large amount of air from the engine, resulting in a large compensatory load; the inertness of the hollow airborne fiber membrane cannot be used, and the total mass of the system is too large

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