The invention relates to a dual-redundancy valve device applied to a
stratosphere aerostat. The dual-redundancy valve device is composed of an inner set of subsystem and an outer set of subsystem, namely, a main subsystem and an auxiliary subsystem, wherein the inner set of subsystem and the outer set of subsystem are symmetrical about a valve
machine base. An inner valve cover corresponds to the main subsystem, and an outer valve cover corresponds to the auxiliary subsystem. The main structure of the dual-redundancy valve device comprises a dual-redundancy valve cover, transmission mechanisms and the valve
machine base, and each valve cover corresponds to one set of transmission mechanism. Each transmission mechanism comprises a prime motor, a
turbine, a worm and other main structures. All devices are installed on the valve
machine base used for supporting all components and transmitting a load to a bag body. A feedback
signal of a micro-switch can be used for feeding an in-place state of a valve back, and provide an outage basis. The opened angle of each valve cover is measured through rotation, and the measurement of the switching value is achieved. A pressure measuring air
nozzle is used for measuring
differential pressure of the bag body, and provides a basis for controlling. A hollow boss is arranged on the inner valve cover and can be
cut down by a
cutting device when failure happens, and reliability of the
system is improved.