The invention discloses a large flow
liquid oxygen supercooling method based on a supersonic ejector. The large flow
liquid oxygen supercooling method comprises the steps that a
heat exchanger used inconventional saturated
liquid nitrogen supercooling liquid oxygen is used as a primary
heat exchanger, and the liquid
oxygen with a supercooling flow rate greater than 4500 L / min can be supercooled from 92K to 80K; a secondary
heat exchanger is arranged at the downstream position of the primary heat exchanger to supercool the liquid
oxygen which is supercooled to 80K and with the supercooling flow rate greater than 4500L / min to below 67K; the secondary heat exchanger is filled with
liquid nitrogen in a saturated state, the temperature of the
liquid nitrogen in the secondary heat exchanger isno more than 64K, and an air outlet of the secondary heat exchanger is connected with an ejected
airflow inlet of the supersonic ejector; an ejector
airflow inlet of the supersonic ejector is connected to a gas outlet of a
gas generator; the supersonic ejector sequentially includes a mixing section, a super-expansion section and a sub-expansion section which are arranged coaxially in the directionof the
airflow; and the mixing section is a conical isobaric
mixing chamber with a contracted cross section. The large flow liquid
oxygen supercooling method can meet the needs of rapid cooling and filling of large-flow liquid oxygen before launching such as CZ-5. In addition, the pumping capacity of the supersonic ejector can be matched with the load, and more security and reliability are achieved.