This invention discloses a pre-
combustion chamber auxiliary stabilization
system based on a sealed microcavity
flare and its operation method. The pre-
combustion chamber auxiliary stabilization
system includes a
flare stabilization microcavity, an
oxygen-enriched pre-
combustion chamber, a fuel-enriched pre-
combustion chamber, an oxidizer
storage tank, and a
liquid ammonia storage tank. The
flare stabilization microcavity, the
oxygen-enriched pre-
combustion chamber, and the fuel-enriched pre-
combustion chamber are each connected to the oxidizer
storage tank via an oxidizer supply channel
assembly. The flare stabilization microcavity, the
oxygen-enriched pre-combustion chamber, and the fuel-enriched pre-combustion chamber are each connected to the
liquid ammonia storage tank via a
fuel supply channel
assembly. The flare stabilization microcavity is connected to the oxygen-enriched pre-combustion chamber and the fuel-enriched pre-combustion chamber via a flare stabilization channel. The oxygen-enriched pre-combustion chamber and the fuel-enriched pre-combustion chamber are each connected to the
thrust chamber. This invention is applied to the field of propulsion systems, enabling propulsion systems to possess excellent combustion stability margins throughout the entire process from
cold start to rated operating conditions and across a wide operating range.