The invention discloses a low opening and closing
pressure difference safety valve for ultrahigh-temperature large-flow
fuel oil steam media for
spaceflight, which comprises a shell, an inlet
pipe nozzle, an inlet locking nut, a large-flow valve core, a low-rigidity spring, a spring seat, a locking nut and an adjusting nut are arranged in the shell from front to back, and a flexible
graphite sealing ring is embedded at the
tail end of the inlet
pipe nozzle. The large-flow valve element slides in the shell in the axial direction, and the front end of the large-flow valve element is designed to be an arc-shaped
conical surface matched with an arc chamfer. The two ends of the spring abut against the spring seat and the
tail of the large-flow valve element respectively, a
safety valve exhaust hole is formed in the front end of the shell, and the
safety valve exhaust hole is communicated with an inlet of the inlet
pipe nozzle when the large-flow valve element is in a retreating state. The pressure relief function of a 380 DEG C ultra-high-temperature
fuel oil steam medium can be achieved, the ultralow opening and closing
pressure difference of 0.005 MPa under the dynamic and static environments is achieved, and the exhaust stability is guaranteed under the vibration and
impact environments.