发明名称 Ultra-High-Pressure Fluid Injection Dynamic Orbit-Transfer System and Method
摘要 A flying object includes a main body, an engine, a power system and an ultra-high-pressure fluid injection dynamic orbit-transfer system which includes a pressure storage device for storing a predetermined amount of ultrahigh-pressure gas, a central automatic control system, at least one air pipeline connected to the pressure storage device, and a nozzle assembly provided on the main body and connected to the air pipeline. The nozzle assembly includes a plurality of nozzle units. Each of the nozzle units includes a nozzle body having a nozzle hole, and is arranged and aligned adjacent to at least another the nozzle unit. The central automatic control system is configured to selectively activate at least two of the nozzle units for ejection of ultrahigh-pressure gas so as to controllably alter a flying locus of the flying object.
申请公布号 US2017088254(A1) 申请公布日期 2017.03.30
申请号 US201615201319 申请日期 2016.07.01
申请人 Hong RuiQing 发明人 Hong RuiQing
分类号 B64C15/14 主分类号 B64C15/14
代理机构 代理人
主权项 1. A flying object, comprising: a main body; an engine supported in said main body for providing a driving force for said main body to fly in air; a power system supported in said main body and connected to said engine; and an ultra-high-pressure fluid injection dynamic orbit-transfer system, which comprises: a pressure storage device supported in said main body and connected to said engine, and arranged to store a predetermined amount of ultrahigh-pressure gas; a central automatic control system supported in said main body; at least one air pipeline connected to said storage device; and a nozzle assembly provided on said main body and connected to said air pipeline, said nozzle assembly comprising a plurality of nozzle units, each of said nozzle units comprising a nozzle body having a nozzle hole, and being arranged and aligned adjacent to at least another said nozzle unit, said central automatic control system being configured to selectively activate at least two of said nozzle units for ejection of ultrahigh-pressure gas so as to controllably alter a flying locus of said flying object.
地址 San Gabriel CA US
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