The application provides a multifunctional modular combination valve for a
space vehicle cold air pressurization
system, comprising a valve body and a subassembly installed on the valve body, wherein the subassembly comprises an electric explosion valve, a buffer valve, a pressure reducing valve, a
safety valve and a
pressure sensor; the valve body is a structure with multiple cavities inside; an air inlet interface and an air outlet interface are arranged side by side on one side of the valve body; the valve body is externally provided with mounting portions corresponding to the subassembly; and each subassembly is threadedly and sealingly connected to the valve body. The application has the advantages of compact structure, small size, simplified pressurization
system structure
layout, reduced space envelope size, improved
assembly process, improved
maintainability, satisfaction of the demand for
miniaturization, light weight and integration of a new generation of aircraft, reduction in the number of high-pressure pipelines and welds in the pressurization
system, reduction in the system weight, improvement in the sealing reliability and anti-mechanical environment performance.